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Publication numberUS2227717 A
Publication typeGrant
Publication dateJan 7, 1941
Filing dateSep 26, 1938
Priority dateSep 26, 1938
Publication numberUS 2227717 A, US 2227717A, US-A-2227717, US2227717 A, US2227717A
InventorsJones Adam W
Original AssigneeJones Adam W
Export CitationBiBTeX, EndNote, RefMan
External Links: USPTO, USPTO Assignment, Espacenet
Chair mounting for airplanes
US 2227717 A
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Description  (OCR text may contain errors)

Jan. 7, 1941. A. w. JONES CHAIR MOUNTING FOR AIRPLANES Filed Sept. 26, 1938 ATTORNEYS Cir Patented Jan. 7, 1941 cnsnt MOUNTING FOR AmrLANss Adam W. Jones, Montoursville, Pa. I Application September 26, 1938, Serial No. 231,749

3 Claims. (01. -99 e e lugs which are mounted on the body of an airplane This invention relates to means for mounting a chair on the body of an airplane.

It has been found by experience that when an airplane comes to a sudden stop, as for example when striking an obstruction, that the aviator or passenger occupyinga chair or seat fixed on the body is often injured by reason of this person being subjected to a. violent forward throw notwithstanding that this person is fastened to the chair by straps or otherwise.

One of the objects of this invention is, to provide simple and reliable means for mounstingthe chair of an airplane on the body of the same so as to permit the chair and its occupant to move forwardly independently of the body in the event of the latter striking an obstruction and thus save the occupant from the full force of the a shock which would otherwise be experienced.

Another object of this invention is to combine with a chair mounting of this character cushioning means which yieldingly resist the forward movement of the chair relative to the body and thus aid in reducing the shocking effect on the person. l

A further object of this invention is to provide means for preventing the chair after being thrown forwardly violently, from recoiling backwardly quickly and thereby preventing injury which otherwise might occur to the person occupying the seat.

With this end in view this invention consists generally of means for mounting thechair on the body of an airplane so that this chair when moved forwardly relative to the body will travel a path which extends forwardly and upwardly instead of merely forwardly, whereby the person occupying the chair will be tossed in a curved forward and upward direction and thus relieved substantially from the shock to which the person i is subjected, also by associating with this chair mounting spring means which yieldingly resist the forward movement of the chair and thus cushion the shock when the body stops suddenly 7 and the chair is thrown forwardly, and also by embodying in this chair mounting detent means whereby the chair after being thrown forwardly is prevented from again moving rearwardly until manually released.

In the accompanying drawing:7 7 a Fig. 1 is a side elevation of means for mounting a chair on the body of an airplane in ac cordance with this invention. 7

Fig. 21s a bottom plan view thereof.

Fig. 3 is a cross section, on an enlarged scale, taken on line 3-4, Fig. 1.

In the following description similar characters of reference indicate like parts in the several figures of the drawing: a

The numerals III, II and I2 represent, respectively, front, intermediate and rear brackets or so as to practically form an integral part thereof, said body, whichfis representedinFig. ,1 by dottedlines 13, being of any suitable construction.

Over the front part of this bodyis arranged the chair which is to. be occupied by the person riding in the airplane such as the aviator or passenger. Although this chair maybe variously constructed, that form which is shown in the drawing comprises a lower horizontal bottom frame 14 which carries aseat IS, a rear frame l6 projectingupwardly from the bottom frame l4 and carrying the back l1, and side frames 18 connecting the bottom frame and back frame and carrying the arm rests 19. In order to prevent the person occupyingthexchair from falling out of the some while the airplane, is in operation,

fasteningmeans are provided which preferably consist of a strap20"adapted to pass forwardly around the body of this person and connected at opposite ends by any suitable means with eyes it which project upwardly from the lower rear parts of the chair frame. 7 7 l l l 7 Means are provided for connectingthe chair withrthe body of'the airplane in such a manner that the chair is capable of moving in a dlrection horizontally lengthwise offthe body and also vertically in theforward part of this movement. The means for this purpose which are shown in the drawingare preferably constructed asfoliows: ,7 ,7

The numerals 22 represent two rear upright comparatively short: links which are arranged on opposite sides of the rear part of the chair and each of which is pivoted at its upper endfby means of a horizontal transverse bolt 23, or the like, to c a lug 24 projecting downwardly from the rear sideapart of the chair frame ll while the lower end of this link is pivotally connected by means of 7a horiZOntaltranSverse bolt 25, or the like, with the adjacent intermediate lug II on the body of the airplane. Thenumeral 2B represents atwo upright front ,comparatively long linkswhich are arrangedon opposite sides of the \flOIilG part of the chair and each of which is pivotally connected'at its: upperend by means of 7a .horizontalptransverse bolt 21, orthe like, with a lug 28 projectingdownwardly from the adjacent front side portion of the chair bottom while the lower end ofthislink is pivotally connected by meansofa horizontal transverse bolt 29, or the 7 like, with the adjacent bracket l0 ofthe airplane body. 4

In the preferredconstruction the lowerrpivots 25 and 29 of rtherear andfront links are arranged f horizontally in line, as shown in Fig. 1, or substantially so, and the upper pivots-23 andll of these links are arranged on a plane which rises forwardly relative ito the planeon which the lower pivots 25 and of these linksare arranged.

In the normal operative position of this chair, in which it is rearmost and lowermost relative to the body, both the rear and front links 22 and 23 are inclined rearwardly and these links stand at an angle of approximately 30, relative to the bottom frame of the chair, as shown by full lines in Fig. 1. When, however, the forward movement of the airplane is suddenly checked or stopped altogether, such as would occur, for example when the airplane strikes an obstruction, then the momentum of the chair together with the load of the person occupyin the same will cause this chair and the person to be thrown violently forwardly. During such movement of the chair both the rear and front links Hand 28 n will also move forwardly into a posiltion in which they are substantially'upright and perpendicular to the bottom frame of the chair and the body of the airplane, as shown by dotted lines in Fig. 1.

front end relative toits rear end duejto'th chair follows at this time, whereby ,th pc occupying the seat will be move?! forwardly also elevated during the latter part-o this for rely 'movedward movement, instead of beingjjrn forwardly in a direction substantially-flparallel with the body of the airplane, thereby causing this person to be tossed'forwardly and upwardly" and relieving this person-from the full effects of the shock which otherwise wouldbe experienced.

The shock to which the occupant of the seat is subjected is further. reduced byso, organizing the front links of the "chairsupporting means that they absorb a considerable amount of this shock. Although various absorbing means. may be employed for this purpose-those whichnare shown in Fig. l are suitable for this purpose and as there shown 'thesame consist in making each of the front links 2i-offupper and lower sections 30, 3| which have their outer ends pivoted respectively to the chair antibody of the airplane while their' inner ends-are guided upon each other and are yieldinglyheldin a distended or elongated position byfmeansfof aspring 32. In the construction shown in Fig- 1 thef'llpper section 30 of each front link is made inJthe form of a tube and the lower sectlo'n'3l hasthe form ofa hollow rod and thespring =32 is-srranged in the tubular upper section '30 of this link and bears with its upper'end'against: a shoulder 33 at the upper end of'the link section 30 while its lower end bears against the upper end of the tubular rod 3|. The extension orelongation of the two sections of each link 23' under the action of the spring 32 maybe-limited in various ways, for example,by means of cooperating shoulders formed on these parts as shown at 34 in Fig. l.


Means are provided which operate to yieldingly hold the chair in its rearmost normal position but permit the chair and its occupant to move forwardly under their momentum independently of the body of the airplane in the event that the latter is stopped by engagement with an obstruction. The preferred means provided for this purpose which are shown in the drawing are constructed as follows:

The numeral 35 represents two cylinders arranged in rear of the side parts of the chair and each provided at its lower end with a head 38 which is pivoted by means of a horizontal transverse bolt 31 to the adjacent bracket I! on the body of the airplane. At its upper end each of these cylinders is provided with a head 33 having a central guide opening 39. Within the lower part of each of the cylinders 36 is arranged a piston or plunger 40 which is provided with an upwardly, extendingoonnecting rod 4| passing through the guide opening 38 in the upper end of the-respective cylinder and pivotally connected byrmeans'pf a horizontal transverse bolt 42 with an attaching lug 43 projecting downwardly from the adjacent part of the chair frame. Within each cylinder is arranged a spring system which [is so, constructed that during the first part of *the upward movement ofthe plunger 40 in this cylinder this spring system will offer only a -moderate resistanceto the plunger and thereafter this spring resistance increases and is most pronounced during the last part'of the upward stroke of the plunger in the cylinder, thereby causing the forward movement of the chair when thrown forwardly by momentum, independently of the body of the airplane, to be checked gradually by encountering progressively increasing re-' sistance, thereby further relieving the person occupying the chair from the shock incident to the collision of the body of the airplane with some obstruction. In the preferred form of these spring resistance means, the same comprise helical spring sections 44, 45 and 48 which are arranged in the cylinder 35 around the connecting rod 4|, the lowermost one of these spring sections 44 being interposed between the plunger 44 and a lower separating disk 41 mounted on the rod 4|, and being made of comparatively light wire so that the-same is only of light tension and offers a moderate resistance, the intermediate section 43 of this spring being interposed between the lower separating disk 41 and an upper separating disk, 43 mounted on the rod 4| and made of heavier wire than the lower spring a section- 44 so as. to be of stronger tension and offer agreater resistance, and'the upper spring .section- 48 being arranged between the upper separating disk 43 and the upper head 33 of the cylinder and made of heavier wire than the intermediate' spring section so as to be of high strength or tension and offer the greatest resistance to the upward movement'of the plunger The combined effect of the several spring'sections of the spring system in each of these cylinders 33 operates to hold thechair in its rearmost normal position which islimited by engagement of the lower ends of the connectingdrods 4| with the lower heads 36 of the cylinders 35, as shown in Fig. 1. If the chair is thrown forwardly only to a moderate extent relative to the body of the airplane due to a comparatively mild impact of thebody with an obstruction, then this partial forward movement of the chair will only compress the lowermost or light springs ll, but when the momentum with which the chair is thrown forward relative to the body of the airplane is greater, then the plungers ill will move upwardly in the cylinders to a greater extent and not only compress the lowermost light springs but also compress the intermediate heavier springs. If, however, the chair is thrown forwardly under a momenum of maximum force, then each piston 40 will not only compress the lower light tension spring 44 and the intermediate spring 45 of greater tension but also compress the upper heaviest spring the tension of which offers the greatest resistance thereby combining the cushioning effect of the several springs in each group and causing the shock upon the person occupying the chair to be reduced accordingly.

In the absence of any other provision, the chair after being thrown forwardly by momentum relative to the airplane body will be again returned automatically to its rearmost normal position by resilience of the several sections of the spring system. This return or recoil movement of these springs is, however, checked by making each of the cylinders 35 practically airtight and providing each of the plungers III with an annular packing 49 so that when each plunger moves upwardly air is free to move from the upper end of each cylinder past its plunger and into the lower end of the. respective cylinder, but when this plunger moves downwardly the air in the lower end of this cylinder will be trapped therein. and escapes slowly therefrom into the upper part of the respective cylinder due to the leakage of the air past the joint between the respective plunger and cylinder. By this construction each cylinder 35 and its plunger 40, in' effect, form a dash-pot which operates to prevent the recoil of the spring system from returning the chair suddenly to its rearmost position and possibly injuring the occupant of the chair if this occupant were jerked back suddenly after being thrown forwardly.

. Means are provided whereby the chair after being moved forwardly by momentum independently of the airplane body is prevented from immediately recoiling backwardly and possibly injuring the occupant of the chair, such as snapping back the head and breaking the neck of the occupant. The means suitable for this purpose shown in thedrawing comprise two detent pawls 50 arranged in an inclined position on opposite sides of the connecting rod ll and above the upper head 38 of each cylinder 35 and pawl pivoted at its outer end by a pin 5| on said head and engaging its inner end with the adjacent part of said rod, and a spring 52 which holds said pawl yieldingly in engagement with said rod and which is interposed between the respective pawl and an abutment 53 on the upper head 38 of the cylinder. By these means the plunger and connecting rod II are free to move upwardly in the cylinder and compress the cluster of spring sections therein for cushioning the forward movement of the chair and its occupant but retrograde movement of these parts is prevented by the clutch action of the detent pawls 50 on the connecting rod thereby avoiding the sudden return of the chair upon reaching the limit of its forward movement and eliminating the possibility of harmful effects which might follow such quick return of the chair.

Restoration of the chair to its normalrearward position can be readily effected by first releasing the. pawls 50 manually from the connecting rod 4| so that the resilience of the springs 44, 45, 46 can operate to move the chair and thereupon reengaging these pawls with said rod ready for repeating this detent function.

These means for mounting the chair of an airplane on the body positively absorb most, ifnot' all, the objectionable shock which theoccupant of the chair would suffer in the absence of such provision and therefore reduce to a minimumthe i liability of injuring the occupant of the chair in case the airplane collides with an obstruction or effects a nose dive. I


1. An airplane comprising a body, a chair, a linkage movably connecting said chair and body and spring means which yieldingly resist the forward movement of said chair andis con structed to offer successively greaterresistanoe to the forward movement of the chair and which includes a lower cylinder pivoted to the body, a plunger arranged in the cylinder and connected with the chair, a lower light tensioned spring engaging with said plunger, an upper heavy tensioned spring engaging with the upper end of said cylinde and an intermediate tensioned spring. interposed between said lower andupper springs.

2. An airplane-comprising a body, a chair, a linkage connecting said chair and body, and means for controlling the movement of saidchair relative to said-body including a cylinder connected with the body, a plunger movable lengthwise in the cylinder and having and connected with said chair, spring means interposed between i said plunger and the cylinder and operating to yieldingly resist the forward movement of said chair, and detent means which permit forward movement of the chair butprevent. backward movement of the same including pawls pivoted on I the cylinder and engaging opposite sides of said said pawls and abutments on said cylinder and a operating to hold the pawls in engagement with rod, and retaining springs interposed between 8. A chair mounting for airplanes comprisinga comparatively long front link pivotally connected at its lower and upper ends with the body of the airplane and the front part of the chair, respec-' tively; a comparatively short rear link spaced from said front link and pivotally connected at its lower and upper ends with said body and the rear part of the chair, said chair and links being movable forwardly and backwardly in a vertical plane, the pivotal connections between the lower ends of said links and the airplane body being stationary and arranged horizontally inline and the pivotal connectionsbetween the upper ends of said links and said chair being arranged on an inclined line which risesforwardly relative tothe line on which the lower ends of said links are pivotally connected with said airplane body, so that in the'rearward position of said links the chair will be tipped upwardly at its front end to a moderate extent while in the forward position of the links the chair will be tipped upwardly at its front end'to a greater extent, and yielding 7 means whereby said chair is yieldingly held in its rearmost position and permits the same to move forwardly under its momentum when the forward movement of the airplane is arrested. 1

Referenced by
Citing PatentFiling datePublication dateApplicantTitle
US2433950 *May 25, 1945Jan 6, 1948Donald HendersonCrash seat for high-speed conveyances
US2568930 *Dec 22, 1945Sep 25, 1951Parsons John BSeat adjuster
US2606727 *Jul 30, 1947Aug 12, 1952De Haven La Vern HSafety chair for vehicles
US2639913 *Apr 10, 1950May 26, 1953Reynolds Decelerator CompanyCrash decelerator
US2660222 *May 29, 1952Nov 24, 1953Woodsworth Leland ASafety seat for vehicles
US2680476 *Mar 7, 1952Jun 8, 1954Saffell James LHydraulic snubber for shoulder harness
US2682931 *Mar 3, 1950Jul 6, 1954Young Victor MMeans for absorbing energy due to sudden impact
US2726831 *Jan 12, 1953Dec 13, 1955Stanley Aviation CorpAircraft seat
US2789650 *Jul 3, 1953Apr 23, 1957Roger RacineSafety vehcilse seat
US2877825 *Jul 2, 1954Mar 17, 1959Olson Herbert OTractor seat
US2880815 *May 5, 1955Apr 7, 1959Fred ApfelbaumVehicle brake operation responsive safety seat device
US2933127 *Apr 11, 1958Apr 19, 1960Aerotec Ind IncSeats for conveyances
US2953189 *Oct 1, 1956Sep 20, 1960Ira M BarashShock absorber
US2959207 *Apr 10, 1958Nov 8, 1960Aerotec Ind IncSeat mountings for aircraft and other conveyances
US2966200 *Sep 4, 1959Dec 27, 1960Aeroquip CorpShock absorbent fitting
US3126072 *Jun 11, 1962Mar 24, 1964 Energy
US3291525 *Oct 18, 1965Dec 13, 1966Fritzmeier RupertVehicle seats
US3429613 *May 19, 1967Feb 25, 1969Rice Herbert CSafety seat belt anchorage
US3531154 *Apr 21, 1969Sep 29, 1970Howell Ind IncEnergy absorbing seat mounting device
US3711153 *Feb 12, 1971Jan 16, 1973Wingard LtdSeats for motor vehicles
US3792896 *Sep 20, 1971Feb 19, 1974Budd CoCrash attenuation apparatus for a seat in a vehicle
US3947058 *Jul 30, 1974Mar 30, 1976Jean Andre LaporteSeat-belt restrainer
US3972561 *Oct 3, 1974Aug 3, 1976Daimler-Benz AktiengesellschaftRetaining mechanism for the passengers of vehicles
US4613101 *Sep 27, 1984Sep 23, 1986The Boeing CompanyApparatus for repositioning aircraft ejection seat during the ejection sequence and method
US4720139 *Oct 6, 1981Jan 19, 1988The United States Of America As Represented By The Administrator Of The National Aeronautics And Space AdministrationVariable response load limiting device
US5022707 *Oct 25, 1988Jun 11, 1991Life Force Associates, L.P.Seat tilting
US5110182 *Oct 21, 1988May 5, 1992Life Force Associates, L.P.Portable seat
US5366269 *Aug 20, 1992Nov 22, 1994Life Force Associates, L.P.Apparatus for restraining a passenger in a vehicle
US5449218 *May 23, 1991Sep 12, 1995Life Force, Inc.Vehicle safety device
US5605372 *Oct 14, 1994Feb 25, 1997Al-Abdullateef; AbdulghafourSafety seat system
US5738409 *Jan 8, 1997Apr 14, 1998Bursik; Thomas A.Rocking chair construction
US6257663 *Apr 25, 2000Jul 10, 2001Richard SwierczewskiVehicle seat for absorbing impact
US6435591 *Mar 11, 1998Aug 20, 2002Autoliv Development AbDevice for avoiding whiplash injuries
US6435592Mar 15, 2001Aug 20, 2002Autoliv Development AbDevice for avoiding whiplash injuries
US6554356Nov 16, 2000Apr 29, 2003The C.E. White Co.Shock absorbing vehicle seat frame
US7393167 *May 17, 2005Jul 1, 2008Be Aerospace, Inc.Load-limiting and energy-dissipating mount for vehicle seating
US7520555 *Dec 8, 2006Apr 21, 2009Ford Global Technologies, LlcEnergy absorbing seat anchor restraint system for child safety seats
US7604293Jun 5, 2007Oct 20, 2009Mazda Motor CorporationVehicle seat structure
US7753442Jun 6, 2006Jul 13, 2010Anecia LlcSpherically guided safety seating system
US8297698Mar 17, 2010Oct 30, 2012Richard SwierczewskiMechatronic vehicle safety seat
EP1864851A1 *Jun 6, 2007Dec 12, 2007Mazda Motor CorporationVehicle seat structure
WO1994004390A1 *Aug 20, 1993Mar 3, 1994Life Force IncApparatus for restraining a passenger in a vehicle
U.S. Classification297/302.4, 296/68.1, 297/216.2, 297/470
International ClassificationG09B9/12, B64D25/04, B64D25/00, G09B9/02
Cooperative ClassificationB64D25/04, G09B9/12
European ClassificationB64D25/04, G09B9/12