WO1982002821A1 - Overhead stowage bin mechanism - Google Patents

Overhead stowage bin mechanism Download PDF

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Publication number
WO1982002821A1
WO1982002821A1 PCT/US1981/001473 US8101473W WO8202821A1 WO 1982002821 A1 WO1982002821 A1 WO 1982002821A1 US 8101473 W US8101473 W US 8101473W WO 8202821 A1 WO8202821 A1 WO 8202821A1
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WO
WIPO (PCT)
Prior art keywords
bin
arms
bolt
bearing means
housing
Prior art date
Application number
PCT/US1981/001473
Other languages
French (fr)
Inventor
Co Boeing
Mark Allen Palombo
Arthur Walkden
Original Assignee
Co Boeing
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Co Boeing filed Critical Co Boeing
Priority to DE8181903050T priority Critical patent/DE3172546D1/en
Publication of WO1982002821A1 publication Critical patent/WO1982002821A1/en

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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D11/00Passenger or crew accommodation; Flight-deck installations not otherwise provided for
    • B64D11/003Stowage devices for passengers' personal luggage

Definitions

  • This invention relates to an overhead stowage bin mechanism, and more particularly to its self-aligning bearing with improved installation and repair features.
  • the present invention is an improved mechanism to the basic mechanism disclosed in U.S. Application Serial No. 973,424.
  • the present overhead stowage bin mechanism is particularly adapted for use in passenger airplanes.
  • Each end of the bin is supported by a pair of pivoted arms of unequal length so proportioned that the bin moves from its stowed position downward and slightly forward, at the same time tilting slightly for ease of access.
  • the arms interengage in the down position to increase rigidity.
  • a spring cartridge is connected to each of the upper arms to counterbalance the weight of the bin, and also is arranged to hold the bin in the down position.
  • the upper arms are interconnected by a torque tube, and a snubbing device is also included in the mechanism.
  • the most important parts of the mechanism are the self-aligning bearings which are employed between the bin walls and the arms.
  • the present invention has a specific bearing design which requires only one repairman for bin installation, dismantling, or repair.
  • the bearing design incorporates three main parts: a) a bearing axle retainer, mounted in the arm; b) an internal bin self-aligning needle housing with automatic axle retention means; and c) an external bin flat nut which holds the housing as one unit onto the bin wall.
  • a bearing axle retainer mounted in the arm
  • an internal bin self-aligning needle housing with automatic axle retention means and c) an external bin flat nut which holds the housing as one unit onto the bin wall.
  • the referenced patent shows some identical features with the bearing axle retainer of the present invention, but fails to disclose the axle retention means, the mounting of the self-aligning needle housing and other specific features designed for the bin mechanism.
  • the present invention provides for the following advantages and improvements over the prior art:
  • the stowage bin can be replaced by one man, thus allowing a great savings in maintenance and installation costs.
  • the stowage bin has self-aligning needle bearings which are so designed as to prevent rocking of the bin; thus, perfect linear control is obtained when the bin is moved from stowage to loading position.
  • the bin material, as well as the clamping boss material, does not require a flush surface as required in the prior art to enhance alignment.
  • the bearing unit can be installed on bin materials of different thicknesses without losing any of its properties and advantages. 5. The bin can be removed or installed without disturbing adjacent bins. 6. The internal bin bearing mountings have no hard edges for luggage to be caught on.
  • the present invention is an improvement to an overhead stowage bin mechanism which utilizes a pair of arms at each side of the bin and allows the bin to be moved from a stowed to a loading position, as is well known in the art.
  • the present improvement resides mainly in the bearing design which results in a self-aligning feature and a one-man installation procedure. It will be realized that this invention is very significant to repair operations. For example, in a Boeing 747 commercial airplane, there may be a row of 50 bins next to each other. Repairing one meant one had to be able to reach inbetween the adjacent bins and thus two bins, one at each side, had to be partly disengaged in order to repair the bin inbetween, because the mounting mechanism is at the outside of the bin.
  • the herein disclosed invention provides improved alignment and removal or installation of one bin from within the bin without removal of adjacent bins by one person.
  • the present self-aligning bearing mechanism has three parts, the first part being a bearing axle retainer. This is an externally threaded part which is threaded into the arm and anchored permanently in place by means of conventional deforming slots which are perpendicular to the threads.
  • the threaded part is concave and carries an internally mounted threaded bolt with a self-locking feature of a ratchet-washer arrangement.
  • This part is a staple item.
  • the second part is a housing having a specifically designed width which contains two sets of needle bearings, approximately 80 total.
  • axle-bolt In the center of the two sets of needle bearings is an axle-bolt which is fully supported over its complete length by the needle bearings.
  • the axle bolt has a hollow internally threaded end which upon installation mates and locks with the external threads of the internally mounted threaded bolt of the axle retainer in the arm.
  • the axle bolt has a circumferentially positioned groove at its end which serves as a stop to a spring w.asher which is positioned around the axle bolt; however, the washer-stop or axle bolt retention will only happen when the axle bolt is removed from the axle retainer.
  • the third part is a nut which is positioned at the outside of the bin and serves to retain the self-aligning needle bearing housing with retention axle bolt onto the bin.
  • FIGURE 1 shows a pair of overhead stowage bins, one in a fully opened loading position.
  • FIGURE 2 is a side elevation of the bin mechanism when the bin is in a stowed or closed position.
  • FIGURE 3 is a side elevation of the bin mechanism when the bin is in an opened or loading position.
  • FIGURE 4 is an exploded view of the bearing arrangement.
  • FIGURE 5 is a cross section through the center of a bearing arrangement in an installed position, as along line 5-5 of FIGURE 1.
  • FIGDRE 6 is a cross section of the bearing arrangement when the axle bolt is disconnected from the arm and becomes retained to the bearing self-aligning needle housing.
  • FIGURE 7 is an elevation taken along line 7-7 of FIGURE 6.
  • the arms 20 and 22 provide for a stowed position of the bin 24 by the locking of mechanisms 10 and 12, the spring 26 and snubber 28 force holding the arms 20-22, mounted at the airplane structure pivot points 36 and 38.
  • the bin 24 Upon pulling the handle 34 downwards, the bin 24 becomes unlocked from the locking mechanism 10-12 as illustrated in FIGURE 1 and stops in a slanted loading position while the arms 20 and 22 grab each other at the center flange 40 and" the fork portion 42, which provides for a sturdy non-rocking position as illustrated in FIGURES 1 and 3.
  • a locking means is provided between the two arms 20 and 22 at each side of the bin 24.
  • Linear control during bin transition from the stowed position to the loading position is obtained by the uniquely designed self-aligning bearings 14 and 18 which are provided with the needle bearings 50 located inside of a housing 52.
  • two sets of needle bearings next to each other, as illustrated in FIGURE 5, are utilized.
  • the width of the housing which is almost equal to the length of the axle bolt 54, provides for proper support of the axle, bolt 54 and thus forms a sturdy linear alignment feature.
  • the complete bearing mechanism 60 has three main parts.
  • the axle retainer 62 which comprises an external threaded part with locking slots 64 which are deformed when the retainer 62 is threaded into the arm so that the retainer is permanently positioned.
  • Inside of retainer 62 is an externally threaded bolt 66 which has a ratchet-washer locking means (not shown) so that when the axle bolt 54, which has an internal threaded portion 55, is screwed onto the retainer bolt 66, the axle bolt 54 becomes mounted and locked. Loosening by vibration or the like is prevented by the ratchet washer locking means.
  • This self locking feature is part of the conventional retainer 62 which is a shelf vendor item.
  • a spring retention washer 68 which fits within the teflon washer 70, becomes an automatic lock or holdingmeans to the axle bolt 54. For instance, when the axle bolt is unfastened from an installed position (see FIGDRES 5 and 6), the washer 68 will slide over the bolt and snap into the groove 72 on the end of the axle bolt 54. Accordingly, the axle bolt 54 will always be retained to the needle bearing housing 52.
  • the unique bearing mechanism and the ability to lock the arms 20 and 22 when the bin 24 is in the loading or folded out position provides one man with the opportunity to install or dismantle a bin 24 when standing at a location near the handle 34. He can replace a damaged bin 24, remove and install the bearing mechanism parts, all within a minimum of time compared to the arrangement of conventional bin installations.
  • a cap 82 can be placed over the axle bolt 54 head, thus a smooth housing surface 80 and cap 82 will prevent sharp interference with luggage.
  • a washer 84 is located under the axle bolt 54 head in the preferred embodiment, as illustrated in the exploded version in FIGDRE 4.
  • the third part of the bearing mechanism is the locking nut 86 which is provided with flat flanges 88 and holes 90 for screwing the locking nut 86 by wrench or spanner wrench to the housing 52 as illustrated in FIGURE 7.
  • a pair of holes 92 similar to holes 90 are provided.

Abstract

The bin mechanism allows the bin (24) to be manually moved without any effort from a stowed position to a loading position. For this purpose, the support arms (20) and (22) are provided with specially designed self-aligning bearings (14) and (18). Each bearing (14) or (18) has three parts: an interior bin mounted needle bearing axle unit or housing (52); an exterior bin mounted nut (86); and an axle retainer unit (62). Installation or repair is accomplished from the interior of the bin (24) by the turning of the bearing axle bolt (54) which is threaded unto either the arm (20) or the arm (22). Disconnection of the bolt (54) from the arms (20) or (22) is accomplished while the bin (24) is in its loading position and momentarily arrested by a pin (44) connecting both arms (20) and (22). However, the bolt does not disconnect from the mechanism but is automatically gripped by a retainer washer (68) for retention thereof inside of the needle housing (52). Self-aligning and linear control is accomplished by the substantially wide needle bearing housing (52) providing full non-rocking support to and about the solidly mounted axle bolt (54).

Description

OVERHEAD STOWAGE BIN MECHANISM
Background of the Invention
A. Field of the Invention. This invention relates to an overhead stowage bin mechanism, and more particularly to its self-aligning bearing with improved installation and repair features.
B. Background of the Invention. The present invention is an improved mechanism to the basic mechanism disclosed in U.S. Application Serial No. 973,424.
The present overhead stowage bin mechanism is particularly adapted for use in passenger airplanes. Each end of the bin is supported by a pair of pivoted arms of unequal length so proportioned that the bin moves from its stowed position downward and slightly forward, at the same time tilting slightly for ease of access. The arms interengage in the down position to increase rigidity. A spring cartridge is connected to each of the upper arms to counterbalance the weight of the bin, and also is arranged to hold the bin in the down position. The upper arms are interconnected by a torque tube, and a snubbing device is also included in the mechanism. However, the most important parts of the mechanism are the self-aligning bearings which are employed between the bin walls and the arms. The mechanism, according to Federal Aviation Administration specifications, must support a 300 pound weight hanging free on the stowage bin without signs of misalignment. Installation or removal of a bin is very cumbersome since a bin is generally mounted in a row of 50 or 60 bins. In the prior art the bins were mounted to the arms outside of the bin since the inside had to remain flush for luggage. Thus, removal of one bin meant disconnection of the bin next to it in order to gain access for removing arms, bearings, etc. Furthermore, such removal required the presence of two to three repairmen.
Accordingly, the present invention has a specific bearing design which requires only one repairman for bin installation, dismantling, or repair.
The bearing design incorporates three main parts: a) a bearing axle retainer, mounted in the arm; b) an internal bin self-aligning needle housing with automatic axle retention means; and c) an external bin flat nut which holds the housing as one unit onto the bin wall. The ontly patent of interest which was observed in the art was U .S. Patent No . 3 , 512 , 328 which discloses a male and a female boss assembly associated with a fastener and wherein the bosses are threadibly interconnected so as to clamp an associated structure as proposed.
The referenced patent shows some identical features with the bearing axle retainer of the present invention, but fails to disclose the axle retention means, the mounting of the self-aligning needle housing and other specific features designed for the bin mechanism.
Accordingly, the present invention provides for the following advantages and improvements over the prior art:
1. The stowage bin can be replaced by one man, thus allowing a great savings in maintenance and installation costs. 2. The stowage bin has self-aligning needle bearings which are so designed as to prevent rocking of the bin; thus, perfect linear control is obtained when the bin is moved from stowage to loading position.
3. The bin material, as well as the clamping boss material, does not require a flush surface as required in the prior art to enhance alignment.
4. The bearing unit can be installed on bin materials of different thicknesses without losing any of its properties and advantages. 5. The bin can be removed or installed without disturbing adjacent bins. 6. The internal bin bearing mountings have no hard edges for luggage to be caught on.
Summary of the Invention The present invention is an improvement to an overhead stowage bin mechanism which utilizes a pair of arms at each side of the bin and allows the bin to be moved from a stowed to a loading position, as is well known in the art. The present improvement resides mainly in the bearing design which results in a self-aligning feature and a one-man installation procedure. It will be realized that this invention is very significant to repair operations. For example, in a Boeing 747 commercial airplane, there may be a row of 50 bins next to each other. Repairing one meant one had to be able to reach inbetween the adjacent bins and thus two bins, one at each side, had to be partly disengaged in order to repair the bin inbetween, because the mounting mechanism is at the outside of the bin.
The herein disclosed invention provides improved alignment and removal or installation of one bin from within the bin without removal of adjacent bins by one person. The present self-aligning bearing mechanism has three parts, the first part being a bearing axle retainer. This is an externally threaded part which is threaded into the arm and anchored permanently in place by means of conventional deforming slots which are perpendicular to the threads. The threaded part is concave and carries an internally mounted threaded bolt with a self-locking feature of a ratchet-washer arrangement. This part is a staple item. The second part is a housing having a specifically designed width which contains two sets of needle bearings, approximately 80 total. In the center of the two sets of needle bearings is an axle-bolt which is fully supported over its complete length by the needle bearings. The axle bolt has a hollow internally threaded end which upon installation mates and locks with the external threads of the internally mounted threaded bolt of the axle retainer in the arm. Furthermore, the axle bolt has a circumferentially positioned groove at its end which serves as a stop to a spring w.asher which is positioned around the axle bolt; however, the washer-stop or axle bolt retention will only happen when the axle bolt is removed from the axle retainer. The third part is a nut which is positioned at the outside of the bin and serves to retain the self-aligning needle bearing housing with retention axle bolt onto the bin. Having thus described the features and advantages of the present invention, other features and advantages of the bin mechanism will become further apparent from the following description presented in conjunction with the accompanying drawings, hereinafter defined in detail. Brief Description of the Drawings FIGURE 1 shows a pair of overhead stowage bins, one in a fully opened loading position.
FIGURE 2 is a side elevation of the bin mechanism when the bin is in a stowed or closed position. FIGURE 3 is a side elevation of the bin mechanism when the bin is in an opened or loading position.
FIGURE 4 is an exploded view of the bearing arrangement. FIGURE 5 is a cross section through the center of a bearing arrangement in an installed position, as along line 5-5 of FIGURE 1.
FIGDRE 6 is a cross section of the bearing arrangement when the axle bolt is disconnected from the arm and becomes retained to the bearing self-aligning needle housing.
FIGURE 7 is an elevation taken along line 7-7 of FIGURE 6.
Detailed Description of the Invention As illustrated in FIGURE 2, the arms 20 and 22 provide for a stowed position of the bin 24 by the locking of mechanisms 10 and 12, the spring 26 and snubber 28 force holding the arms 20-22, mounted at the airplane structure pivot points 36 and 38. Upon pulling the handle 34 downwards, the bin 24 becomes unlocked from the locking mechanism 10-12 as illustrated in FIGURE 1 and stops in a slanted loading position while the arms 20 and 22 grab each other at the center flange 40 and" the fork portion 42, which provides for a sturdy non-rocking position as illustrated in FIGURES 1 and 3. Upon installation, dismantling, or repair by only one man, in accordance to the present invention, it appears essential to retain the arras in a locked position by temporarily connecting the two arms 20 and 22 by the insertion of a locking pin 44 through the holes in fork 42 and flange 40. Accordingly, a locking means is provided between the two arms 20 and 22 at each side of the bin 24. Linear control during bin transition from the stowed position to the loading position is obtained by the uniquely designed self-aligning bearings 14 and 18 which are provided with the needle bearings 50 located inside of a housing 52. Preferably two sets of needle bearings next to each other, as illustrated in FIGURE 5, are utilized. As illustrated further, the width of the housing, which is almost equal to the length of the axle bolt 54, provides for proper support of the axle, bolt 54 and thus forms a sturdy linear alignment feature. The complete bearing mechanism 60 has three main parts. The axle retainer 62, which comprises an external threaded part with locking slots 64 which are deformed when the retainer 62 is threaded into the arm so that the retainer is permanently positioned. Inside of retainer 62 is an externally threaded bolt 66 which has a ratchet-washer locking means (not shown) so that when the axle bolt 54, which has an internal threaded portion 55, is screwed onto the retainer bolt 66, the axle bolt 54 becomes mounted and locked. Loosening by vibration or the like is prevented by the ratchet washer locking means. This self locking feature is part of the conventional retainer 62 which is a shelf vendor item.
A spring retention washer 68, which fits within the teflon washer 70, becomes an automatic lock or holdingmeans to the axle bolt 54. For instance, when the axle bolt is unfastened from an installed position (see FIGDRES 5 and 6), the washer 68 will slide over the bolt and snap into the groove 72 on the end of the axle bolt 54. Accordingly, the axle bolt 54 will always be retained to the needle bearing housing 52. The unique bearing mechanism and the ability to lock the arms 20 and 22 when the bin 24 is in the loading or folded out position provides one man with the opportunity to install or dismantle a bin 24 when standing at a location near the handle 34. He can replace a damaged bin 24, remove and install the bearing mechanism parts, all within a minimum of time compared to the arrangement of conventional bin installations. In order to maintain an overall smoothness in the bin 24, a cap 82 can be placed over the axle bolt 54 head, thus a smooth housing surface 80 and cap 82 will prevent sharp interference with luggage. Furthermore, a washer 84 is located under the axle bolt 54 head in the preferred embodiment, as illustrated in the exploded version in FIGDRE 4. The third part of the bearing mechanism is the locking nut 86 which is provided with flat flanges 88 and holes 90 for screwing the locking nut 86 by wrench or spanner wrench to the housing 52 as illustrated in FIGURE 7. In order to hold the housing 52, which has a smooth surface and thus presents a holding problem, a pair of holes 92 similar to holes 90 are provided. And now, therefore, we claim:

Claims

Claims 1. In a stowage bin assembly comprising a fixed supporting structure and a relatively movable bin; mechanism for supporting and guiding said bin from and with respect to said structure comprising in combination: a) an upper arm pivoted at its extremities to said structure and pivoted by a first bearing means to said bin; b) a lower arm, having an abutment intermediate its extremities, pivoted at its extremities to said structure and pivoted by a second bearing means to said bin; c) said upper arm having a cooperating abutmentengaging element engageable with said abutment of said lower arm and interfitting therewith, for limiting relative motion of said arms about their pivots and resisting relative motion therebetween parallel to said pivots; and d) said abutment and said abutment-engaging element provided with a locking means for temporarily locking said arms together for bin installation and repair purposes.
2. In a stowage bin assembly comprising a fixed supporting structure and a relatively movable bin as claimed in claim 1 wherein said first bearing means comprises: a) a self-locking, threaded bolt mounted at said first arm extremity; b) a housing, carrying needle bearing elements to form an elongated axle hole, mounted to said bin interior area; and c) an axle bolt having an internal threaded portion cooperating with said self-locking, threaded bolt and fastened therewith and positioned through said elongated axle hole to form a self-aligning bearing between said first arm and said bin.
3. In a stowage bin assembly comprising a fixed supporting structure as claimed' in claim 1 or claim 2 wherein said second bearing means comprises: a) a self locking threaded bolt mounted at said second arm extremity; b) a housing carrying needle bearing elements to form an elongated axle hole mounted to said bin interior area; and c) an axle bolt having an internal threaded portion cooperating with said self-locking threaded bolt and fastened therewith and positioned through said elongated axle hole to form a self-aligning bearing between said second arm and said bin.
4. A stowage bin assembly including a supporting structure, a bin movable with respect to the supporting structure, and mechanism carrying said bin for said structure by a first pair of arms pivoted on said structure and pivoted by a first bearing means on said bin and by a second pair of arms vertically spaced from said first pair, pivoted on said structure and pivoted by a second bearing means on said bin, each of said second pair of arms being provided intermediate its length with an abutment, and each of said first pair of arms having a fork adjacent its movable end adapted to engage said abutment in one relative position of said arms, the improvement comprising: a) a first housing mounted on said bin interior side forming part of said first bearing means; b) a set of needle bearing means forming a substantial elongated axle' hole mounted in said first housing; c) a bolt, perpendicularly and integrally connected at each said arms of said first pair of arms for forming part of said first bearing means, and d) an axle bolt mounted through said first housing from said bin interior side, through said elongated axle hole, and fastened to said bolt for self-alignment of said first bearing means so that linear controlled bin transition with respect to said supporting structure is obtained.
5. A stowage bin assembly including a supporting structure, a bin movable with respect to the supporting structure, and mechanism carrying said bin for said structure by a first pair of arms pivoted on said structure and pivoted by a first bearing means on said bin and by a second pair of arms vertically spaced from said first pair, pivoted on said structure and pivoted by a second first bearing means on said bin, each of said second pair of arms being provided intermediate its length with an abutment, and each of said first pair of arms having a fork adjacent its movable end adapted to engage said abutment in one relative position of said arms, as claimed in claim 4, the improvement comprising: a) a second housing mounted on said bin interior side forming part of said second bearing means; b) a set of needle bearing means forming a substantial elongated axle hole mounted in said second housing; c) a bolt, perpendicularly and integrally connected at each said arms of said second pair of arms for forming part of said second bearing means; and d) an axle bolt mounted through said second housing from said bin interior side, through said elongated axle hole and fastened to said bolt for self-alignment of said second bearing means so that linear controlled bin transition with respect to said supporting structure is obtained.
6. A stowage bin assembly as claimed in claim 4 or claim 5' wherein said first and said second bearing axle bolt is provided with a retaining groove at its end portion, and wherein a spring washer is provided about said bolt located between said housing and said arm having an outside diameter larger than said axle hole so that upon removal of said axle bolt, said spring washer will contract about said retaining groove and provide -for retention of said axle bolt in said housing of said first and said second bearing means.
PCT/US1981/001473 1981-02-17 1981-11-02 Overhead stowage bin mechanism WO1982002821A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
DE8181903050T DE3172546D1 (en) 1981-02-17 1981-11-02 OVERHEAD STOWAGE AM MECHANISM

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US06/235,215 US4368937A (en) 1981-02-17 1981-02-17 Overhead stowage bin mechanism
US235215810217 1981-02-17

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WO1982002821A1 true WO1982002821A1 (en) 1982-09-02

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EP (1) EP0076796B1 (en)
WO (1) WO1982002821A1 (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0184620A2 (en) * 1984-12-12 1986-06-18 Ford-Werke Aktiengesellschaft Storing device in the linings of motor vehicles
EP2537752A1 (en) * 2011-06-20 2012-12-26 Airbus Operations GmbH Movable stowage bin
FR2981043A1 (en) * 2011-10-11 2013-04-12 Airbus Operations Sas Retractable luggage rack for passenger cabin in aircraft, has support mounted movable in rotation around axis relative to frame, and compartment mounted movable in rotation around another axis relative to support
WO2018219934A1 (en) 2017-06-01 2018-12-06 Inspire AG für mechatronische Produktionssysteme und Fertigungstechnik Force transmission assembly and insert

Families Citing this family (107)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4720154A (en) * 1986-11-19 1988-01-19 Seiter Stephen R Automatic teller machine having motorized drawer
US4760926A (en) * 1988-01-11 1988-08-02 Peter Iuni Light bulb organizer and storage device
US4941718A (en) * 1988-03-21 1990-07-17 Alexander Machinery, Inc. Concealed retractable housings
JP2628346B2 (en) * 1988-07-01 1997-07-09 株式会社トプコン Memory card storage
US4867498A (en) * 1988-12-02 1989-09-19 Chivas Products Limited Overhead console assembly
US5050922A (en) * 1989-11-30 1991-09-24 United Technologies Automotive Overhead console having a pivotable storage shelf-door
DE4130644A1 (en) * 1991-09-14 1993-03-18 Airbus Gmbh UPPER LUGGAGE RACK WITH A LOWERABLE TRAY, IN PARTICULAR FOR A PASSENGER PLANE
DE4209037C2 (en) * 1992-03-20 1994-06-23 Deutsche Aerospace Airbus Device for carrying luggage in airplanes
DE9214592U1 (en) * 1992-10-28 1993-02-11 Deutsche Aerospace Airbus Gmbh, 2000 Hamburg, De
US5281042A (en) * 1992-11-17 1994-01-25 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Adminstration Saddle clamp assembly
US5466028A (en) * 1993-12-27 1995-11-14 Ford Motor Company Storage compartment for an automotive vehicle
US5456529A (en) * 1993-12-30 1995-10-10 The Boeing Company Powered overhead stowage bin
US5480039A (en) * 1994-04-14 1996-01-02 Merl; Milton J. Two bin inventory/facing construction for similar products with different packaging or different versions of the same sized and shaped product
US5567028A (en) * 1995-02-27 1996-10-22 The Boeing Company Mechanism for translating storage bin
DE29518173U1 (en) * 1995-11-16 1996-01-11 Itw Ateco Gmbh Device for damping the movement of a movably mounted component, in particular a flap in an automobile or the like.
DE19546302C2 (en) * 1995-12-12 1998-08-20 Daimler Benz Aerospace Airbus Luggage rack
USRE44313E1 (en) 1996-10-22 2013-06-25 The Boeing Company Airplane with unswept slotted cruise wing airfoil
US5868353A (en) * 1996-11-21 1999-02-09 Benard; Patricia A. Overhead luggage compartment safety device
US5842668A (en) * 1997-02-27 1998-12-01 Hexcel Corporation Quick fit overhead stowage compartment
US6066399A (en) 1997-03-19 2000-05-23 Sanyo Electric Co., Ltd. Hard carbon thin film and method of forming the same
DE29710918U1 (en) * 1997-06-23 1997-08-14 Itw Ateco Gmbh Fuel filler flap
US5934615A (en) * 1997-08-25 1999-08-10 Hexcel Corporation Luggage bins with articulating mechanism
JP3388161B2 (en) * 1997-12-01 2003-03-17 日野自動車株式会社 Overhead console
DE10001038B4 (en) * 2000-01-13 2004-01-29 Airbus Deutschland Gmbh Luggage rack with a lowerable luggage compartment, especially for an aircraft passenger cabin
DE10063932C2 (en) * 2000-12-20 2002-11-28 Airbus Gmbh Luggage rack with a lowerable luggage compartment, especially for an aircraft passenger cabin
JP4046554B2 (en) * 2002-06-12 2008-02-13 嘉信 香取 Airplane baggage storage
US7258308B2 (en) * 2002-07-02 2007-08-21 The Boeing Company Method and apparatus for controlling airflow with a gapped trailing edge device having a flexible flow surface
US6899299B2 (en) * 2002-07-26 2005-05-31 The Boeing Company Luggage bins and aircraft passenger cabin ceilings
JP4169603B2 (en) * 2003-01-22 2008-10-22 株式会社ニフコ Lock mechanism and movable body opening / closing device
US6991276B2 (en) * 2003-05-20 2006-01-31 Mccauley Alvin D Luggage loft assembly
US7059563B2 (en) * 2003-06-03 2006-06-13 The Boeing Company Systems, apparatuses, and methods for moving aircraft control surfaces
US6799739B1 (en) * 2003-11-24 2004-10-05 The Boeing Company Aircraft control surface drive system and associated methods
US7240945B1 (en) * 2004-01-09 2007-07-10 Alfa Leisure, Inc. Articulating overhead console for recreational vehicles
US7424350B2 (en) * 2004-02-02 2008-09-09 The Boeing Company Vehicle control systems and corresponding sizing methods
US20050264144A1 (en) * 2004-06-01 2005-12-01 Tk Canada Limited Cabinet door support mechanism
US6978971B1 (en) * 2004-06-15 2005-12-27 The Boeing Company Methods and apparatuses for controlling airflow proximate to engine/airfoil systems
US7270305B2 (en) * 2004-06-15 2007-09-18 The Boeing Company Aircraft leading edge apparatuses and corresponding methods
US7494094B2 (en) * 2004-09-08 2009-02-24 The Boeing Company Aircraft wing systems for providing differential motion to deployable lift devices
US7264206B2 (en) * 2004-09-30 2007-09-04 The Boeing Company Leading edge flap apparatuses and associated methods
US20060132007A1 (en) * 2004-12-22 2006-06-22 Beckley Daniel V Storage bin assembly
US7128295B2 (en) * 2005-01-07 2006-10-31 The Boeing Company Pivot mechanism for quick installation of stowage bins or rotating items
US7775966B2 (en) 2005-02-24 2010-08-17 Ethicon Endo-Surgery, Inc. Non-invasive pressure measurement in a fluid adjustable restrictive device
US7322547B2 (en) * 2005-01-31 2008-01-29 The Boeing Company Aerospace vehicle leading edge slat devices and corresponding methods
US7338018B2 (en) * 2005-02-04 2008-03-04 The Boeing Company Systems and methods for controlling aircraft flaps and spoilers
RU2395431C2 (en) * 2005-02-15 2010-07-27 Эйрбас Сас Aircraft luggage rack and method to load it
US20060182513A1 (en) * 2005-02-15 2006-08-17 Dortch John P Fastener and method for using same
US7699770B2 (en) 2005-02-24 2010-04-20 Ethicon Endo-Surgery, Inc. Device for non-invasive measurement of fluid pressure in an adjustable restriction device
US8066629B2 (en) 2005-02-24 2011-11-29 Ethicon Endo-Surgery, Inc. Apparatus for adjustment and sensing of gastric band pressure
US8016744B2 (en) 2005-02-24 2011-09-13 Ethicon Endo-Surgery, Inc. External pressure-based gastric band adjustment system and method
US7927270B2 (en) * 2005-02-24 2011-04-19 Ethicon Endo-Surgery, Inc. External mechanical pressure sensor for gastric band pressure measurements
US7775215B2 (en) 2005-02-24 2010-08-17 Ethicon Endo-Surgery, Inc. System and method for determining implanted device positioning and obtaining pressure data
US7658196B2 (en) 2005-02-24 2010-02-09 Ethicon Endo-Surgery, Inc. System and method for determining implanted device orientation
US7234666B2 (en) * 2005-03-02 2007-06-26 The Boeing Company Pivoting storage bin and method of making
US7309043B2 (en) * 2005-04-27 2007-12-18 The Boeing Company Actuation device positioning systems and associated methods, including aircraft spoiler droop systems
US7300021B2 (en) * 2005-05-20 2007-11-27 The Boeing Company Aerospace vehicle fairing systems and associated methods
US7721999B2 (en) * 2005-05-20 2010-05-25 The Boeing Company Aerospace vehicle fairing systems and associated methods
US7367530B2 (en) * 2005-06-21 2008-05-06 The Boeing Company Aerospace vehicle yaw generating systems and associated methods
US7500641B2 (en) * 2005-08-10 2009-03-10 The Boeing Company Aerospace vehicle flow body systems and associated methods
US7611099B2 (en) * 2005-09-07 2009-11-03 The Boeing Company Seal assemblies for use with drooped spoilers and other control surfaces on aircraft
EP1937126A4 (en) * 2005-09-20 2014-07-23 Sca Hygiene Prod Ab Dispenser
US8047468B2 (en) * 2005-10-14 2011-11-01 The Boeing Company Stowage bin with shear fittings
US20070084966A1 (en) * 2005-10-14 2007-04-19 Haynes Michael S Stowage bin with shear fittings
US8011618B2 (en) * 2005-10-28 2011-09-06 Airbus Storage device for baggage for an aircraft cabin
US7708231B2 (en) * 2005-11-21 2010-05-04 The Boeing Company Aircraft trailing edge devices, including devices having forwardly positioned hinge lines, and associated methods
US8152710B2 (en) * 2006-04-06 2012-04-10 Ethicon Endo-Surgery, Inc. Physiological parameter analysis for an implantable restriction device and a data logger
US20080249806A1 (en) * 2006-04-06 2008-10-09 Ethicon Endo-Surgery, Inc Data Analysis for an Implantable Restriction Device and a Data Logger
US20080250341A1 (en) * 2006-04-06 2008-10-09 Ethicon Endo-Surgery, Inc. Gui With Trend Analysis for an Implantable Restriction Device and a Data Logger
US8870742B2 (en) 2006-04-06 2014-10-28 Ethicon Endo-Surgery, Inc. GUI for an implantable restriction device and a data logger
US7578484B2 (en) * 2006-06-14 2009-08-25 The Boeing Company Link mechanisms for gapped rigid krueger flaps, and associated systems and methods
GB2441989B (en) * 2006-09-21 2011-09-07 Ford Global Tech Llc An overhead storage compartment for a vehicle
US20080252090A1 (en) * 2007-04-16 2008-10-16 Lear Corporation Vehicle overhead console assembly having a drop down occupant mirror assembly
US8187163B2 (en) * 2007-12-10 2012-05-29 Ethicon Endo-Surgery, Inc. Methods for implanting a gastric restriction device
US7954769B2 (en) 2007-12-10 2011-06-07 The Boeing Company Deployable aerodynamic devices with reduced actuator loads, and related systems and methods
US7766282B2 (en) * 2007-12-11 2010-08-03 The Boeing Company Trailing edge device catchers and associated systems and methods
US8100870B2 (en) 2007-12-14 2012-01-24 Ethicon Endo-Surgery, Inc. Adjustable height gastric restriction devices and methods
US20090171379A1 (en) * 2007-12-27 2009-07-02 Ethicon Endo-Surgery, Inc. Fluid logic for regulating restriction devices
US8377079B2 (en) 2007-12-27 2013-02-19 Ethicon Endo-Surgery, Inc. Constant force mechanisms for regulating restriction devices
US8142452B2 (en) * 2007-12-27 2012-03-27 Ethicon Endo-Surgery, Inc. Controlling pressure in adjustable restriction devices
US8192350B2 (en) 2008-01-28 2012-06-05 Ethicon Endo-Surgery, Inc. Methods and devices for measuring impedance in a gastric restriction system
US8337389B2 (en) 2008-01-28 2012-12-25 Ethicon Endo-Surgery, Inc. Methods and devices for diagnosing performance of a gastric restriction system
US8591395B2 (en) 2008-01-28 2013-11-26 Ethicon Endo-Surgery, Inc. Gastric restriction device data handling devices and methods
US20090192534A1 (en) * 2008-01-29 2009-07-30 Ethicon Endo-Surgery, Inc. Sensor trigger
US8221439B2 (en) * 2008-02-07 2012-07-17 Ethicon Endo-Surgery, Inc. Powering implantable restriction systems using kinetic motion
US20090204179A1 (en) * 2008-02-07 2009-08-13 Ethicon Endo-Surgery, Inc. Powering implantable restriction systems using temperature
US7844342B2 (en) 2008-02-07 2010-11-30 Ethicon Endo-Surgery, Inc. Powering implantable restriction systems using light
US8114345B2 (en) * 2008-02-08 2012-02-14 Ethicon Endo-Surgery, Inc. System and method of sterilizing an implantable medical device
US8591532B2 (en) 2008-02-12 2013-11-26 Ethicon Endo-Sugery, Inc. Automatically adjusting band system
US8057492B2 (en) * 2008-02-12 2011-11-15 Ethicon Endo-Surgery, Inc. Automatically adjusting band system with MEMS pump
US8034065B2 (en) * 2008-02-26 2011-10-11 Ethicon Endo-Surgery, Inc. Controlling pressure in adjustable restriction devices
US20090228063A1 (en) * 2008-03-06 2009-09-10 Ethicon Endo-Surgery, Inc. System and method of communicating with an implantable antenna
US8233995B2 (en) 2008-03-06 2012-07-31 Ethicon Endo-Surgery, Inc. System and method of aligning an implantable antenna
US8187162B2 (en) * 2008-03-06 2012-05-29 Ethicon Endo-Surgery, Inc. Reorientation port
DE102008034779A1 (en) * 2008-07-25 2010-01-28 Airbus Deutschland Gmbh Device for the rotatable mounting of an aircraft interior equipment component
DE102008049639A1 (en) * 2008-09-30 2010-04-08 Airbus Deutschland Gmbh Load Path Optimized Swiveling Luggage Rack (Hatrack)
US8382045B2 (en) 2009-07-21 2013-02-26 The Boeing Company Shape-changing control surface
DE102010008622A1 (en) * 2010-02-19 2011-08-25 Airbus Operations GmbH, 21129 Caseless storage compartment
EP2404783A1 (en) * 2010-07-09 2012-01-11 Delphi Technologies, Inc. Roof module with storage assembly
DE102010034025B4 (en) * 2010-08-11 2022-02-24 Diehl Aviation Laupheim Gmbh overhead bin
DE102011108895A1 (en) * 2011-07-29 2013-01-31 Airbus Operations Gmbh Carrying structure for movable storage compartment
US9789963B2 (en) 2012-02-14 2017-10-17 C&D Zodiac, Inc. Pivot bin assembly with minimal force required for closing
US10029794B2 (en) 2012-02-14 2018-07-24 C&D Zodiac, Inc. Outboard rotating pivot bin assembly
CN103887650A (en) * 2012-12-20 2014-06-25 深圳富泰宏精密工业有限公司 Chip holding structure and electronic device having chip holding structure
US9157260B1 (en) * 2013-04-24 2015-10-13 The Boeing Company Hydraulically actuated latch mechanism
AT515849A1 (en) * 2014-05-26 2015-12-15 Facc Ag Overhead luggage compartment
US9630718B2 (en) 2015-02-06 2017-04-25 The Boeing Company Variable opening overhead stowage bins and related methods
WO2017151508A1 (en) * 2016-03-01 2017-09-08 Shanghai Yanfeng Jinqiao Automotive Trim Systems Co. Ltd Storage compartment for vehicle interior
US10604965B2 (en) * 2016-08-31 2020-03-31 The Boeing Company Method and apparatus for clocking stowage bin latches

Citations (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US876159A (en) * 1906-10-04 1908-01-07 Peter Erickson Drawer attachment.
US893081A (en) * 1908-04-09 1908-07-14 Andrew Kunan Nut-lock.
US919170A (en) * 1907-05-10 1909-04-20 Joseph B Holesteine Nut-lock.
US1145264A (en) * 1914-04-15 1915-07-06 Frederick A Pflug Portable wardrobe.
GB124139A (en) * 1918-07-23 1919-03-20 Annie Laura Harrell Improvements in and relating to Bolts and Lock Nuts.
US2037156A (en) * 1935-06-15 1936-04-14 Howard A Taplin Needle bearing spring end mounting means
US2929474A (en) * 1958-08-26 1960-03-22 Boardman Stanley Bolt retainer
US3512328A (en) * 1967-07-07 1970-05-19 Bofors Ab Fastening device
US3790240A (en) * 1972-01-10 1974-02-05 Nadella Rolling bearing assembly with a reduced operational clearance
US4076351A (en) * 1976-04-19 1978-02-28 Hobart Dale Wyant Up-down cabinet
US4102005A (en) * 1977-07-05 1978-07-25 Schlage Lock Company Door closer arm
US4275942A (en) * 1978-12-26 1981-06-30 The Boeing Company Stowage bin mechanism

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US806277A (en) * 1905-05-29 1905-12-05 Watson William Mckee Store-cabinet.
US2590341A (en) * 1946-02-23 1952-03-25 Orvie E Nabholz Filing cabinet
DE821444C (en) * 1949-07-24 1951-11-19 Max Schadewald Screw locking
US2885230A (en) * 1957-10-11 1959-05-05 Trico Products Corp Wiper arm head assembly
US3406999A (en) * 1966-07-05 1968-10-22 Ford Motor Co Vehicle camper galley
FR2159800A5 (en) * 1971-11-12 1973-06-22 Rex Chainbelt Inc
DE3069803D1 (en) * 1980-10-09 1985-01-24 Boeing Co STOWAGE AM MECHANISM

Patent Citations (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US876159A (en) * 1906-10-04 1908-01-07 Peter Erickson Drawer attachment.
US919170A (en) * 1907-05-10 1909-04-20 Joseph B Holesteine Nut-lock.
US893081A (en) * 1908-04-09 1908-07-14 Andrew Kunan Nut-lock.
US1145264A (en) * 1914-04-15 1915-07-06 Frederick A Pflug Portable wardrobe.
GB124139A (en) * 1918-07-23 1919-03-20 Annie Laura Harrell Improvements in and relating to Bolts and Lock Nuts.
US2037156A (en) * 1935-06-15 1936-04-14 Howard A Taplin Needle bearing spring end mounting means
US2929474A (en) * 1958-08-26 1960-03-22 Boardman Stanley Bolt retainer
US3512328A (en) * 1967-07-07 1970-05-19 Bofors Ab Fastening device
US3790240A (en) * 1972-01-10 1974-02-05 Nadella Rolling bearing assembly with a reduced operational clearance
US4076351A (en) * 1976-04-19 1978-02-28 Hobart Dale Wyant Up-down cabinet
US4102005A (en) * 1977-07-05 1978-07-25 Schlage Lock Company Door closer arm
US4275942A (en) * 1978-12-26 1981-06-30 The Boeing Company Stowage bin mechanism

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0184620A2 (en) * 1984-12-12 1986-06-18 Ford-Werke Aktiengesellschaft Storing device in the linings of motor vehicles
EP0184620A3 (en) * 1984-12-12 1987-09-09 Ford-Werke Aktiengesellschaft Storing device in the linings of motor vehicles
EP2537752A1 (en) * 2011-06-20 2012-12-26 Airbus Operations GmbH Movable stowage bin
US8783609B2 (en) 2011-06-20 2014-07-22 Airbus Operations Gmbh Movable bin
FR2981043A1 (en) * 2011-10-11 2013-04-12 Airbus Operations Sas Retractable luggage rack for passenger cabin in aircraft, has support mounted movable in rotation around axis relative to frame, and compartment mounted movable in rotation around another axis relative to support
WO2018219934A1 (en) 2017-06-01 2018-12-06 Inspire AG für mechatronische Produktionssysteme und Fertigungstechnik Force transmission assembly and insert
DE102017112174A1 (en) * 2017-06-01 2018-12-06 Inspire AG für mechatronische Produktionssysteme und Fertigungstechnik Power transmission assembly and insert

Also Published As

Publication number Publication date
EP0076796B1 (en) 1985-10-02
EP0076796A4 (en) 1983-03-17
EP0076796A1 (en) 1983-04-20
US4368937A (en) 1983-01-18

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