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Publication numberUS3496519 A
Publication typeGrant
Publication dateFeb 17, 1970
Filing dateApr 16, 1968
Priority dateApr 16, 1968
Publication numberUS 3496519 A, US 3496519A, US-A-3496519, US3496519 A, US3496519A
InventorsVetter Ottomar H
Original AssigneeUnited Carr Inc
Export CitationBiBTeX, EndNote, RefMan
External Links: USPTO, USPTO Assignment, Espacenet
Release connector having a swiveled lanyard
US 3496519 A
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Description  (OCR text may contain errors)

Feb. 17, 31970 o. ll-l. VETTER 3,495,519

RELEASE CONNECTOR HAVING A SWIVELED LANYARD Filed April 16, 1968 2 Sheets-Sheet 2 88 INVENTOR. afro/wm? #Enum A :vaan/exs 3,496,519 RELEASE CONNECTOR HAVING A SWIVELED LANYARD Ottomar H. Vetter, Minneapolis, Minn., assignor to United-Carr, Incorporated, Boston, Mass., a corporation of Delaware Filed Apr. 16, 1968, Ser. No. 721,775 Int. Cl. H01r 13/ 62 U.S. Cl. 339-45 7 Claims ABSTRACT OF THE DISCLOSURE The two halves or components of an electrical connector are mated by insertion of one half into the other half. Helical slots or grooves guide one component into proper latching relationship with the other. When the latching engagement has been properly effected, external indicia on the two components is automatically brought into physical alignment to designate that the latching engagement has been fully made. A lanyard has its ends mounted in the inner race of a ball bearing assembly and a coil spring resists the pull exerted on the lanyard to a desired degree, a sufficient pull causing the spring to compress with the result that the bayonet pawls included in the latching mechanism are free to move outwardly and disengage the lugs that have been brought into latching engagement and which latching engaement is normally denoted by the aligned indicia.

BACKGROUND OF THE INVENTION Field of the invention This invention relates generally to electric connectors and pertains more particularly to an electrical connector that will separate when a predetermined amount of force is applied to the two halves or components.

Description of the prior art Release-type connectors have been used in the past. However, such connectors have not clearly indicated when the parts have been properly mated. Also, no provision has been made for the twisting of the connector with respect to the objects between which it is attached.

SUMMARY OF THE INVENTION Aircraft operations, particularly those of a military nature, involve the release of one object with respect to another object. Jettisonable fuel tanks normally held under the wings of an airplane is but one example where electrical signals must be transmitted from the tank itself to the instrument board. Another application requiring a releasable type of electrical connector is in conjunction with the separation of the nose cone from a missile body. Also, rockets are frequently held beneath the wing of a plane and must be appropriately controlled in .order to effect a launching thereof. Other situations involve the flexible suspension of one object from another high-altitude balloon exploration activity being but one example, such a suspension involving a foreshortening of the cable or lanyard that is used if the lanyard cannot rotate or swivel through a complete circle.

Accordingly, the present invention has for an object the provision of a connector that will release when a predetermined load is applied thereto, yet which will per- States i. e atent mit the component parts to be easily mated together. More specifically, the invention has for an aim the provision of a ball bearing assembly to which the lanyard is attached so that the inner race thereof can be rotated relative to the outer race in order to allow initial connection of the components. Also, the invention enables the person effecting the connection to know when the parts have been properly latched together, appropriate indicia that is easily discernible, both visually and by touch, being employed. Also, the aforementioned ball bearing assembly allows the lanyard to remain in an untwisted and hence unshortened condition during the use when connecting two objects that twist or rotate with respect to each other.

BRI-EF DESCRIPTION OF THE DRAWING FIGURE l is a perspective view illustrating my connector in actual use, the upper component of which is connected to one fragmentarily depicted object and the lower component connected to another object which is also only fragmentarily depicted;

FIGURE 2'is a sectional view taken in the direction of line 2-2 of FIGURE l for the purpose of showing the internal construction of the connector;

FIGURE 3 is a sectional view taken in the direction of line 3-3 of FIGURE 2 which illustrates the latching arrangement and also certain keys and keyways that are embodied in the connector;

FIGURE 4 is a sectional view of the lower portion of the upper connector component, the view being Similar to that pictured in FIGURE 2 but with the plug body removed so as to show the helical groove arrangement that is utilized in latching the two components together;

FIGURE 5 is an exploded perspective view of the plug body for the purpose of showing a keyway inthe threaded portion thereof which receives an internal key on the spring retainer shell, a section of the shell Wall being removed in order to expose said key, and

FIGURE 6 is a perspective view of the lower component for the purpose of showing still more clearly the means by way of which the latching engagement of the two components is accomplished but with its contacts removed.

DESCRIPTION OF THE PREFERRED EMBODIMENT Referring first to FIGURE l, the connector exemplifying my invention has been generally denoted by the reference numeral 10. The connector comprises a first half or component 12 and a second half or component 14 which are separable or releasable with respect to each other. To illustrate the utility of the invention, a portion 16 of an airplane wing has been shown which has a U- bolt 18 mounted therein and for the sake of a simplified illustration held by nuts 20. It is the U-bolt 18 that serves as a mechanical connection for a lanyard 22 which is connected to the first component 12 in a manner presently to be described. It can be seen from FIGURE 1, though, that a plurality .of conductors constituting a cable 24 lead upwardly through a grommet 26 in the wing 16 and continue on to the instrument board in the cockpit of the plane. A portion 28 of a fuel tank has been pictured, this being the object that is to be jettisoned in the present instance. As can be readily discerned from FIGURE 1, the second component 14 includes a flange 30 and mounting screws 32 extend through this flange into the tank 28.

The first component 12 in addition to the lanyard 22 comprises a coupling ring or outer sleeve 34 forming an outer race portion 36. The outer sleeve 34 further includes an internal flange 38 intermediate the race portion 36 and a skirt portion 40. From FIGURE 3 it will be seen that the skirt portion 40 is formed with three keyways 42 for a purpose hereinafter explained. Actually, the internal flange 38 is formed by counterboring the sleeve 34 and the counterbored portion of the skirt 40 accommodates the latching mechanism referred to later herein. At this time, attention is directed to an inner sleeve or inner race 44 that is contained within the outer race 36. By means of a plurality of balls 46 the inner race 44 is made rotatable with respect to the outer race 36. Also, the inner race 44 is formed with diametrically located, radially directed apertures 48 which have in communication therewith axial passages 50, one of which appears in FIGURE 2.

It is through the agency of the diametrically located apertures 48 that a pair of beads or enlarged members 52 are held or accommodated, these beads 52 being fixedly attached to the ends of the lanyard 22. Thus, the bight of the lanyard 22 passes over the U-shaped bolt 18 and the beads 52 are anchored in the inner race 44 to attach the lanyard to the ball bearing assembly formed by the inner race 44 and the outer race 36. Inasmuch as the outer race 36 is integral with the outer sleeve 34, the lanyard 22 is connected via the inner race 44 and the balls 46 to the sleeve 34 which functions as a coupling ring as hereinbefore briefly mentioned and which hereinafter will become better understood. It will be perceived, though, that the bore labeled 54 of the outer sleeve 34 has a diameter equal to the diameter of the bore labeled 56 of the inner race 44.

A spring retainer shell 58, best seen in FIGURES 2 and 5 but visible at one end in FIGURE 1, is contained within the bores 54 and 56, the shell 58 having an outturned flange 59 and a cylindrical body 60 integral with the flange 59 and an inturned flange 61 integral with the other end of the body 60 remote from the flange 59. Although the keyway therefor will be mentioned later, attention is drawn to the presence of a key or lug 62 on the flange 61, the key 62 extending inwardly from the inturned flange 61, a portion of the body 60 in FIGURE 5 being broken away to expose the key 62. There is also a compression washer or ring 64 (FIGURE 2) that bears against the inturned flange 61.

The cylindrical body 60 has a diameter considerably less than the diameter of the previously mentionedv bores 54 and 56, thereby forming an annular space 66 for the reception of a coil spring 68. It is this particular spring 68 that determines the force needed to effect the release or separation of the first component 12 with respect to the second component 14. The particular spring constant for the coil spring 68 can be selected so as to determine the amount of separation force that will be necessary.

The component 12 includes a plug body 70 having a barrel 72 provided with a threaded portion at 74. The previously mentioned key 62 is designed to fit within a keyway 75 formed in the threaded portion 74. A retaining nut 76 when placed on the threaded portion 74, and tightened sufiiciently will engage the compression washer or ring 64. It will be appreciated that the washer 64 will in this way be forced against the inturned flange 61 of the shell 58 to thereby mechanically anchor the plug body 70 to the shell 58, the key 62 and keyway 75 assuring a desired angular orientation of these parts.

The plug body 70 further includes a dielectric disc 78, a first rubber insert 80 and a second rubber insert 82. It will be appreciated that the disc 78 is of rigid dielectric material and serves as a mounting means for a plurality of plug contacts 84. The plug contacts extend from opposite sides of the disc 78 and are embedded in the rubber inserts 80, 82. The barrel 72 includes an integral shroud 86 thereon having four axially disposed and angularly spaced keys 88 plus a wider key 88a as can be seen Vin FIGURE 5. The barrel 72 also has an outer peripheral flange 90.

The means for coupling together the components 12 and 14 in a mated relationship includes a latch ring 92 provided in the illustrated instance with three slots 94 (all three appearing in FIGURE 3), each-having an external indentation 96 (FIGURE 4) and communicating at one end with an external circumferential groove 98.

The coupling means further comprises three bayonet pawls 100 which are carried by the latch ring 92. More specifically, the pawls 100 are pivotally mounted on pins 102 that reside in the circumferential groove 98. Additional pins 104 function as limits or stops for the pawls 100, the pins 104 bearing against the bottom of the external indentations 96 when the pawls are pivoted inwardly toward each other. From FIGURE 2 it will be discerned that each pawl 100 is formed with a latch tooth at 106 and has a limit edge 108 which engages the interior of the coupling ring or outer sleeve 34. Thus, the pivotal movement of the pawls 100 is limited in one direction by its particular pin 104 and in the opposite direction by the sleeve 34 when said sleeve 34 circumscribes the pawls 100 so that the edges 108 can bear thereagainst.

From FIGURE 4 it will be seen that a lip 110 has a thickness approximately one-half of the thickness of the latch ring 92. This forms a bore 112 having a reduced diameter compared with the internal diameter of the lip 110, thereby forming a shoulder at 114. By reason of the reduced diameter bore 112 and the resulting shoulder 114 a sufficient thickness exists for the provision of helical slots or grooves 116 that form guide ramps or tracks leading to centrally disposed ends of the previously mentioned slots 94 in which the bayonet pawls 100 reside. Also, there is an internal annular groove 118 communicating with the same ends of the slots 94 into which the helical slots 116 terminate, the slots 116 also terminat.

ing in this same groove 118. A wave washer 120 (FIG- URE 2) functions as a spring for a purpose presently to be referred to, the washer 120 being disposed in the internal groove 118.

Close inspection of FIGURE 2 will demonstrate that an internal shoulder at 122 abuts the barrel flange 90 at one side thereof, whereas a groove 124 disposed circumferentially around the interior of the latch ring 92 accommodates a spring washer 126 having two revolutions in the illustrated situation; this washer may be a Spiralox washer but any locking washer having the requisite spring action can be utilized.

At this time reference will be made to the construction of the other component 14 which when mated with the component 12 constitutes the connector 10. The component 14 includes a receptacle body 128. Part of the body 128 is a sleeve 130 that is integral with the earlier-mentioned mounting flange 30, the sleeve 130 functioning to effect the mating of the component 14 with the component 12. The sleeve 130 has four internal longitudinal keyways 132 that are angularly spaced so as to receive therein the previously mentioned keys 88 and a wider keyway 13211 for accommodating the key 88a.

Of importance in effecting the mating of the two components 12 and 14 are radially projecting lugs 134 which are of a size so as to be received readily in the helical slots or grooves 116. In this way, when the sleeve 130 is twisted with respect to the latch ring 92, the lugs 134 will be helically advanced toward the internal groove 118 and will bear against the wave washer 120.

While the specific number of individual contacts is unimportant to a practicing of the invention, nonetheless the number of receptacle or socket contacts labeled 136 will correspond lwith the number of plug contacts 84 contained in the first connector component 12. A rigid dielectric disc 13S which corresponds to the disc 78 is employed and carries the various receptacle contacts 136. The disc 138 is disposed -between a rst rubber insert 140 and a second r-ubber insert 142. It is important, quite obviously, that these receptacle contacts 136 be properly oriented s`o as to receive therein the various plug contacts 84 when the two components 12, 14 are fully mated with each other. The keys 88 or 88u,ntogether with the keyways 132 and 132a, assure the correct orientation and hence the proper engagement of the contacts 84 and 134.

The receptacle body 128 in addition to having the ange 30 has a projecting threaded end 144 which allows a conductor orfcable clamp 146 to be attached thereto. The clamp 146 has a split ring end at 148 which can be tightened against the bundle of conductors or cable that will be electrically connected to the various receptacle contacts 136 and which function s0 as to provide a continuation of the electrical paths provided by the Vpreviously mentioned vconductors 24.

Inasmuch as it is planned that the connector components 12 'and 14 will separate when a predetermined amount offorce is applied to the lanyard 22, such as by the releaseof the fuel tank 28 by a mechanical release. mechanism' not shown, it is extremely critical that the various contacts 84 be engaged properly Iwith the contacts 136. This can only be done when the two components 12 and 14 are angularly oriented with each other. Hence, if the radially projecting lugs 134 are not fully advanced so that they reside in axial alignment with the bayonet pawls 100, morespecifically the latching teeth 106 thereof, the desired electrical connections will not be made.

With the 'foregoing in mind, the present invention incorporates therein visible notches 150 on the outer sleeve 34. These notches can not only be felt but can also be readily seen, especially where a brightly colored paint is applied thereto. Additional notches 152, there being three such notches 152 because three notches 150 have been illustrated, are disposed on the outturned flange 59 of the spring retainer shell 58. The alignment or reg-istry of these notches 150 and 152 with each other can be seen in FIG- URE. l. Additionally, lines or shallow grooves 154 on the outer sleeve 34 are employed and these lines become registered with further lines or grooves 156 on the sleeve 34 of the second component 14. Consequently, the person coupling the components 12 and 14 together will be apprised of the fully latched or mated relationship of these components when the end notches 150, 152 are aligned and also when the l-ines or grooves 154, 156 are in registry with each other.

It should be obvious from the information given herein that antifouling properties or characteristics are imparted to the lanyard 22. More specifically, if the objects 16 and 28 are such that they would rotate relative to each other (not in a situation where one is an airplane -wing and one is a fuel tank but likely in balloon explorations) the lanyard 22 would become shorter by virtue of the twisting action. However, this objectionable result is obviated when practicing the instant invention because the inner race 44 can readily rotate relative to the outer race 36 owing to the ball bearings 46 disposed therebetween. A considerable amount of thrust or load can be carried without the balls binding which would prevent further rotative movement. Hence, a full circle can be achieved as far as the swiveling action is concerned in this instance.

Not only is the swivel action provided during actual use of the connector but the swivel action facilitates the mating of the two components 12, 14. Assuming now that the objects16 and 28 are xedly oriented with respect to each other,.:such as when one constitutes an airplane wing and the other a fuel tank, then the person connecting the two components cannot adjust or orient the objects themselves. All that he need do, though, is to twist one component with respect to the other and thereby effect the alignment. It will be recognized that a pylon usually houses the connector 10 when it serves as a connecting means between the electrical circuitry that extends into the wing of the plane and the subjacent fuel tank that is to be released or jettisoned when it becomes empty. Very little space is available for eifecting the mating of the two cornponents 12, 14 in such a situation and the present invention has particular value in such an environment.

What is claimed is:

1. A release connector having a swiveled lanyard comprising a first connector component including an outer sleeve member forming an outer race adjacent one end and an inwardly directed shoulder between said one end and the other end thereof, a shoulder inner sleeve mem ber forming an inner race, a plurality of ball bearings disposed between said races so that said inner sleeve member is rotatable within said outer sleeve member, a lanyard having an intermediate bight portion for attaching said rst component to one object, said lanyard having its ends anchored to said inner sleeve member at diametrically opposite locations which lie axially between said ball bearings and said one end of said outer sleeve to thereby mount said lanyard for swivel movement with respect to said outer sleeve, a shell within said sleeve members having anoutwardly directed shoulder at the end thereof lying adjacent the said one end of said outer sleeve member and a cylindrical body portion of a size to form an annular space between said body portion and said sleeve members, a coil spring contained in said annular space having its ends abutting said shoulders, contact means xedly carried within said shell member, and coupling means mounted in a fixed relation with the contact means and normally residing within said outer shell member near the other end thereof; a second connector component including a shell member, a Contact means iixedly carried within said second shell member, coupling means on said second shell member releasably engageable with the coupling means of said rst component, means on said second shell for attaching said second component to a second object, whereby said outer sleeve member, said shell member and first contact means can be rotatively oriented to effectuate proper mating of sa'id respective contact means.

2. A connector in accordance with claim 1 including enlarged elements on said lanyard ends, said inner sleeve member having radially directed apertures at said diametrically opposite locations of a size to receive therein said enlarged elements and said inner sleeve further having axial passages leading into said radially directed apertures from the end of said inner sleeve member that is adjacent said one end of the outer sleeve member, said passages being of a size large enough to accommodate said lanyard and small enough to prevent escape of said enlarged elements to thereby anchor said lanyard ends.

3. A connector :in accordance with claim 2 in which said rst coupling lmeans includes a ring member retained in a xed relationship with said first shell member and said first contact means, a plurality of bayonet pawls pivotally mounted to said ring member, said ring member having an axially directed slot for each of said pawls so that said pawls normally pivot outwardly against the interior of said outer sleeve and are thus limited thereby, and a plurality of radially projecting lugs on the shell member of said second component engageable with said pawls, there being a lug for each of said pawls.

4. A connector in accordance with claim 3 in which said outer sleeve member has indicia thereon and said rst shell member also has indicia theron, said respective indicia being in registry when said lugs are in latched engagement with said pawls.

5. A connector in accordance with claim 4 in which the indicia on said outer sleeve member constitutes at least one notch formed in the end thereof adjacent said lanyard and the indicia on said first shell member constitutes a corresponding number of notches formed in the shoulder of said shell member.

7 v 8 6. A connector in accordance with claim 3 in which References Cited said outer sleeve member has indicia thereon adjacent the UNITED STATES PATENTS end thereof opposite said lanyard and said second shell 2 710 384 6/1955 Dupre et al member also has indicia thereon near the end thereof 3043925 7/1962 Wilson having said lugs, said respective indicia being in registry 5 3138423 6/1964 Samuelson et al i 339273 when said lugs are in latched engagement with said pawls. 3,1 561513 11/1964 Peterson et al.

7. A connector in accordance with claim 6 in which the indicia on the outer sleeve member constitutes at least RICHARD E. MOORE, Primary Examiner one longitudinal line and in which the indicia on said second shell member constitutes a corresponding number 10 U-S- Cl- X-R- of lines. 891.811; 339-113, 186

UNITED STATES PATENT OFFICE Po-wso (5/69) CERTIFICATE OF CORRECTION Par-.ent No. 3,496,519 Dated February 17, 1970 Invenror) Ottomar H. Vetter It :la certified that error appears in the shave-identified patent and that said Lettera Patent are hereby corrected as shown below:

Column 6 line 12 "s boulder" should be shorter line 33 delete "a (second occurrence) SIGNED AND SEALED JUL141970 4SEAL) Attest:

EdwardMFletcherJr.

.At-testing Officer WILLIAM E. SGI-FINDER, JR. onlnissionea` of Patents

Patent Citations
Cited PatentFiling datePublication dateApplicantTitle
US2710384 *Jul 8, 1949Jun 7, 1955Burndy Engineering Co IncSpring loaded disconnecting panel
US3043925 *Sep 25, 1958Jul 10, 1962Cannon Electric CoElectrical connector with multiple release mechanism
US3138423 *Dec 13, 1962Jun 23, 1964Dale Products IncUpper end airplane antenna mast
US3156513 *Jan 26, 1962Nov 10, 1964IttPeripheral tang lock for quick disconnect umbilical connector
Referenced by
Citing PatentFiling datePublication dateApplicantTitle
US4330166 *Aug 16, 1979May 18, 1982Automation Industries, Inc.Electrical connector substantially shielded against EMP and EMI energy
US4490002 *Dec 1, 1982Dec 25, 1984The United States Of America As Represented By The Secretary Of The Air ForceReleasable cable connector assembly for use between a mobile and stationary object
US4930209 *Jul 14, 1989Jun 5, 1990Amp IncorporatedMethod for assembly of lanyard and connector
US7097490 *Dec 11, 2003Aug 29, 2006Edo Mbm Technology LimitedElectrical connector
US8052444 *Sep 2, 2010Nov 8, 2011Raytheon CompanyLatching release system for a connector assembly
Classifications
U.S. Classification439/258, 439/315, 89/1.811, 439/680
International ClassificationH01R13/633, H01R13/635
Cooperative ClassificationH01R13/635
European ClassificationH01R13/635