[go: up one dir, main page]
More Web Proxy on the site http://driver.im/

US2331990A - Chair construction - Google Patents

Chair construction Download PDF

Info

Publication number
US2331990A
US2331990A US342929A US34292940A US2331990A US 2331990 A US2331990 A US 2331990A US 342929 A US342929 A US 342929A US 34292940 A US34292940 A US 34292940A US 2331990 A US2331990 A US 2331990A
Authority
US
United States
Prior art keywords
stanchions
frame
seat
supporting
sleeves
Prior art date
Legal status (The legal status 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 status listed.)
Expired - Lifetime
Application number
US342929A
Inventor
Mcarthur Warren
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
WARREN MCARTHUR Corp
Original Assignee
WARREN MCARTHUR CORP
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 WARREN MCARTHUR CORP filed Critical WARREN MCARTHUR CORP
Priority to US342929A priority Critical patent/US2331990A/en
Application granted granted Critical
Publication of US2331990A publication Critical patent/US2331990A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D11/00Passenger or crew accommodation; Flight-deck installations not otherwise provided for
    • B64D11/06Arrangements of seats, or adaptations or details specially adapted for aircraft seats
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B60VEHICLES IN GENERAL
    • B60NSEATS SPECIALLY ADAPTED FOR VEHICLES; VEHICLE PASSENGER ACCOMMODATION NOT OTHERWISE PROVIDED FOR
    • B60N2/00Seats specially adapted for vehicles; Arrangement or mounting of seats in vehicles
    • B60N2/68Seat frames
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D11/00Passenger or crew accommodation; Flight-deck installations not otherwise provided for
    • B64D11/06Arrangements of seats, or adaptations or details specially adapted for aircraft seats
    • B64D11/0639Arrangements of seats, or adaptations or details specially adapted for aircraft seats with features for adjustment or converting of seats

Definitions

  • This invention relates to chairs or seats and an object is to provide a chair particularly adapted for airplane use.
  • a further object is to provide a chair of this type constructed and arranged to resist the unusual stresses and stains to which an airplane chair is subjected while at the ame time permitting the use of very light weight material in its manufacture.
  • the invention comprises a base frame member including a pair of spaced stanchions, and a seat carrying frame or carriage which is supported and vertically adjustable on the spaced stanchions.
  • the seat supporting carriage includes a pair of elongated sleeves rigidly secured tothe carriage and slidably mounted on the stanchions which are in turn securely anchored to the floor or the like.
  • the sleeve connection between the rigid seat frame and the securely anchored stanchions prevents any distortion of the parts due to side stresses resulting, for example, from tilting or banking of a plane in flight.
  • stanchions l 0 are secured to spaced elongated supports ll adapted to be mounted on tracks for horizontal adjustment in any desired manner.
  • the stanchions are preferably tubular and may be separate members or may, as illustrated, be formed from a single tube of U-shape bent to form a horizontal base portion [2. If separate members, each stanchion is independently secured to one of the supports 1 l. v
  • the seat supporting frame or carriag 13 IS preferably formed from a single tube bent to provide side members ll, an upper rear transverse frame member I 5, and a lower rear transverse frame member IS.
  • the upper and lower cross members are connected by and rigidly secured to spaced sleeves I'I slidably mounted on the supporting stanchion l0.
  • Each end of each sleeve is rigidly secured in a bore formed in a tube-securing block 18 which has a groove to receive the adjacent cross frame member or tube IE or I 6 secured therein by a strap l9 bolted to the block, see Figure 5.
  • a pin 20 extends through the strap and cross member to prevent rotation of the tubular member relative to the clamping block.
  • the seat carriage and connected sleeve members form a structural unit which is movable vertically on the stanchions.
  • Any suitable device for locking the carriage at different heights can be employed. That shown consists of a pin 2
  • the pin is mounted in a bracket 23 secured to the block l8 and pressed inwardly by spring 24. It can be retracted to permit movement of the carriage bya hand lever,
  • a fork 29 or the like engages a collar 30 on the locking pin 2
  • lifting the handle 25 retracts pin 21 to permit the seat carriage to be raised or lowered on the stanchions, while release of the handle permits the spring 24 to impel the pin into locking position in a perforation in the stanchion.
  • a lock is provided on each sleeve.
  • the rocker shaft 28 extends across the carriage to actuate both pins and is similarly supported at each end.
  • FIG. 1 shows a back frame 31 and a seat frame 32, the detailed constructed of which forms no part of this invention.
  • means such as elastic cords 33 between a cross member 34, which connects the upper ends of the stanchions l0, and the cross member I6 of the seat carriage can be employed to lift the carriage upon release of the locking pins. When occupied the weight of the occupant will move the carriage downwardly when the pins are released.
  • the construction is such as will provide a strong, rigid construction even with light weight structural members of tubular form. It will be apparent from Figure 4 that the rectangular formation provided by the seat carriage and supporting sleeves provides a positive lock against any distortion by side strains resulting,'for example, from banking of a plane in flight. The stanchions being securely anchored to the base no deformation of the frame structure is possible short of actual collapse of a structural member.
  • a chair construction comprising a pair of supporting stanchions, a seat carrying frame formed by a single tubular member bent to provide spaced side members connected by upper and lower transverse frame members all formed by said tubular member, frame supporting sleeves slidably mounted on said stanchions, means for rigidly securing' said transverse frame members to said sleeves, and means for supporting said sleeves at any one of a plurality of points on said stanchions.
  • a chair construction comprising a tubular base frame including a pair of tubular supporting stanchions, a seat carrying frame formed by a single tubular member bent to provide spaced side members connected by upper and lower transverse frame members all formed by said tubular member, a frame supporting sleeve slidably mounted on each stanchion, means for rigidly securing said transverse frame members to said sleeves, and means for supporting said sleeves on said stanchions.
  • a chair construction comprising a base frame formed by a lJ-shaped member bent to form a horizontal base portion and spaced upwardly ber, seat frame supporting sleeves slidably mounted on said stancbions, means rigidly securing said upper and lower transverse frame members to spaced points on said sleeves, and means for supporting said sleeves on said stanchions.
  • a chair construction comprising a base frame formed by a tubular member of U-shape bent to form a horizontal base portion and spaced upwardly extending stanchions, a seat carrying frame formed by a second tubular member bent to provide spaced side members and vertically spaced upper and lower transverse frame members connecting said side members and all formed by said second tubular member, seat frame supporting sleeves slidably mounted on said stanchions, means rigidly securing said upper and lower transverse frame members to vertically spaced points on said sleeves, and means for supporting said sleeves on said stanchions.

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Transportation (AREA)
  • Mechanical Engineering (AREA)
  • Chair Legs, Seat Parts, And Backrests (AREA)

Description

Oct. 19, 1943. w. McARTHUR CHAIR CONSTRUCTION 3 Sheets-Sheet 1 Filed June 28, 1940 NHMH Oct. 19, 1943. w. McARTHUR 2,331,990
CHAIR CONSTRUCTION Filed June 28, 1940 3 Sheets-Sheet 2 Oct. '19, 1943. WMCARTHUR 2,331,990
CHAIR CONSTRUCTION Filed June 28, 1940 5 Sheets-Sheet 5 ha INVENTOR ATTO EY Patented Oct; 19, 1943 CHAIR CONSTRUCTION Warren McArthur, New York, N. Y., assignor to Warren McArthur Corporation, a corporation or New York Application June 28, 1940, Serial No. 342,929
4 Claims. (01. 155-88) This invention relates to chairs or seats and an object is to provide a chair particularly adapted for airplane use.
A further object is to provide a chair of this type constructed and arranged to resist the unusual stresses and stains to which an airplane chair is subjected while at the ame time permitting the use of very light weight material in its manufacture.
These and other objects which will be apparent to those skilled in the art are accomplished by this invention, one embodiment of which is The illustrated embodiment of my invention is shown in the drawings as formed'of hollow tubes for light weight, and this is the preferred construction although it will be apparent that various features of the invention are equally adapted to other forms of structural members.
The invention comprises a base frame member including a pair of spaced stanchions, and a seat carrying frame or carriage which is supported and vertically adjustable on the spaced stanchions. The seat supporting carriage includes a pair of elongated sleeves rigidly secured tothe carriage and slidably mounted on the stanchions which are in turn securely anchored to the floor or the like. The sleeve connection between the rigid seat frame and the securely anchored stanchions prevents any distortion of the parts due to side stresses resulting, for example, from tilting or banking of a plane in flight.
As illustrated, spaced supporting stanchions l 0 are secured to spaced elongated supports ll adapted to be mounted on tracks for horizontal adjustment in any desired manner. The stanchions are preferably tubular and may be separate members or may, as illustrated, be formed from a single tube of U-shape bent to form a horizontal base portion [2. If separate members, each stanchion is independently secured to one of the supports 1 l. v
The seat supporting frame or carriag 13 IS preferably formed from a single tube bent to provide side members ll, an upper rear transverse frame member I 5, and a lower rear transverse frame member IS. The upper and lower cross members are connected by and rigidly secured to spaced sleeves I'I slidably mounted on the supporting stanchion l0. Each end of each sleeve is rigidly secured in a bore formed in a tube-securing block 18 which has a groove to receive the adjacent cross frame member or tube IE or I 6 secured therein by a strap l9 bolted to the block, see Figure 5. For additional rig dity a pin 20 extends through the strap and cross member to prevent rotation of the tubular member relative to the clamping block.
It will be apparent that the seat carriage and connected sleeve members form a structural unit which is movable vertically on the stanchions. Any suitable device for locking the carriage at different heights can be employed. That shown consists of a pin 2| extending through an opening in a lower block 18 and adapted to enter perforations 22 in the adjacent face of the associated stanchion. The pin is mounted in a bracket 23 secured to the block l8 and pressed inwardly by spring 24. It can be retracted to permit movement of the carriage bya hand lever,
25 connected by link 26 to crank arm 21 on rocker shaft 28 supported in a bracket 28' at each end.
A fork 29 or the like engages a collar 30 on the locking pin 2|. Obviously, lifting the handle 25 retracts pin 21 to permit the seat carriage to be raised or lowered on the stanchions, while release of the handle permits the spring 24 to impel the pin into locking position in a perforation in the stanchion. Preferably a lock is provided on each sleeve. As shown the rocker shaft 28 extends across the carriage to actuate both pins and is similarly supported at each end.
Any type of seat and back frame or frames can be mounted on the seat carriage I3. The drawings show a back frame 31 and a seat frame 32, the detailed constructed of which forms no part of this invention.
If desired, means such as elastic cords 33 between a cross member 34, which connects the upper ends of the stanchions l0, and the cross member I6 of the seat carriage can be employed to lift the carriage upon release of the locking pins. When occupied the weight of the occupant will move the carriage downwardly when the pins are released.
The construction is such as will provide a strong, rigid construction even with light weight structural members of tubular form. It will be apparent from Figure 4 that the rectangular formation provided by the seat carriage and supporting sleeves provides a positive lock against any distortion by side strains resulting,'for example, from banking of a plane in flight. The stanchions being securely anchored to the base no deformation of the frame structure is possible short of actual collapse of a structural member.
It will be apparent that the invention can be variously modified and adapted within the scope of the appended claims.
I claim:
1. A chair construction comprising a pair of supporting stanchions, a seat carrying frame formed by a single tubular member bent to provide spaced side members connected by upper and lower transverse frame members all formed by said tubular member, frame supporting sleeves slidably mounted on said stanchions, means for rigidly securing' said transverse frame members to said sleeves, and means for supporting said sleeves at any one of a plurality of points on said stanchions.
2. A chair construction comprising a tubular base frame including a pair of tubular supporting stanchions, a seat carrying frame formed by a single tubular member bent to provide spaced side members connected by upper and lower transverse frame members all formed by said tubular member, a frame supporting sleeve slidably mounted on each stanchion, means for rigidly securing said transverse frame members to said sleeves, and means for supporting said sleeves on said stanchions.
3. A chair construction comprising a base frame formed by a lJ-shaped member bent to form a horizontal base portion and spaced upwardly ber, seat frame supporting sleeves slidably mounted on said stancbions, means rigidly securing said upper and lower transverse frame members to spaced points on said sleeves, and means for supporting said sleeves on said stanchions.
4. A chair construction comprising a base frame formed by a tubular member of U-shape bent to form a horizontal base portion and spaced upwardly extending stanchions, a seat carrying frame formed by a second tubular member bent to provide spaced side members and vertically spaced upper and lower transverse frame members connecting said side members and all formed by said second tubular member, seat frame supporting sleeves slidably mounted on said stanchions, means rigidly securing said upper and lower transverse frame members to vertically spaced points on said sleeves, and means for supporting said sleeves on said stanchions.
WARREN McARTI-IUR.
US342929A 1940-06-28 1940-06-28 Chair construction Expired - Lifetime US2331990A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US342929A US2331990A (en) 1940-06-28 1940-06-28 Chair construction

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US342929A US2331990A (en) 1940-06-28 1940-06-28 Chair construction

Publications (1)

Publication Number Publication Date
US2331990A true US2331990A (en) 1943-10-19

Family

ID=23343895

Family Applications (1)

Application Number Title Priority Date Filing Date
US342929A Expired - Lifetime US2331990A (en) 1940-06-28 1940-06-28 Chair construction

Country Status (1)

Country Link
US (1) US2331990A (en)

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2457242A (en) * 1944-11-30 1948-12-28 United Shoe Machinery Corp Gun turret
US2481382A (en) * 1947-08-07 1949-09-06 Myrtle Lee Ruppert Three-way baby chair
US2570687A (en) * 1946-07-24 1951-10-09 Edward J Boss Chair having vertically adjustable seat
US2637371A (en) * 1950-07-13 1953-05-05 Harold S Boutin Chair having resilient frame
US2664141A (en) * 1950-03-15 1953-12-29 Elvin M Musselman Baby walker with removable sling
US3285656A (en) * 1965-07-26 1966-11-15 System Communica Aktiebolag Height adjusting devices for chairs, tables, and the like
US3305264A (en) * 1966-01-17 1967-02-21 M H Spinks Sr Entpr Inc Adjustable aircraft seat
US3954298A (en) * 1973-05-22 1976-05-04 Universal Oil Products Company Height adjustment mechanism for suspension seat
US7008015B2 (en) 2003-12-16 2006-03-07 Eric Bischoff Seat suspension assembly
US10682933B2 (en) 2018-05-16 2020-06-16 Eric Bischoff Adjustable seat suspension assembly

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2457242A (en) * 1944-11-30 1948-12-28 United Shoe Machinery Corp Gun turret
US2570687A (en) * 1946-07-24 1951-10-09 Edward J Boss Chair having vertically adjustable seat
US2481382A (en) * 1947-08-07 1949-09-06 Myrtle Lee Ruppert Three-way baby chair
US2664141A (en) * 1950-03-15 1953-12-29 Elvin M Musselman Baby walker with removable sling
US2637371A (en) * 1950-07-13 1953-05-05 Harold S Boutin Chair having resilient frame
US3285656A (en) * 1965-07-26 1966-11-15 System Communica Aktiebolag Height adjusting devices for chairs, tables, and the like
US3305264A (en) * 1966-01-17 1967-02-21 M H Spinks Sr Entpr Inc Adjustable aircraft seat
US3954298A (en) * 1973-05-22 1976-05-04 Universal Oil Products Company Height adjustment mechanism for suspension seat
US7008015B2 (en) 2003-12-16 2006-03-07 Eric Bischoff Seat suspension assembly
US10682933B2 (en) 2018-05-16 2020-06-16 Eric Bischoff Adjustable seat suspension assembly

Similar Documents

Publication Publication Date Title
US2746520A (en) Reclining chair
US2331990A (en) Chair construction
US2439163A (en) Invalid transfer device
US3779600A (en) Foldable arm rest assembly
US3316014A (en) Telescoping chair
US2182598A (en) Reclining chair
US3203732A (en) Chair having adjustable back and seat
US2675059A (en) Rockable and springable chair of the reclining deck or lawn type
US2689600A (en) Portable armrest for automobile seats
US1262216A (en) Adjustable foot-rest for chairs.
US3039119A (en) Stretcher having recessed bed
US2015138A (en) Chair
US2776704A (en) Reclining chaise longue
US1842208A (en) Adjustable arm sofa
US2203610A (en) Folding chair
US1937056A (en) Combination cot and reclining chair
US2638151A (en) Seat for vehicles such as aircraft
GB1037972A (en) Improvements in reclining seats
US1701417A (en) Motor-vehicle seat
US2614612A (en) Convertible chaise lounge
US2767778A (en) Adjustable dual-purpose chair
US2079767A (en) Glider swing
US2783824A (en) Lounging chair with adjustable back rest
US2814333A (en) Child's chair for use either within or outside of an automobile
US2799326A (en) Reclining seat back construction