GB956020A - Improvements in or relating to apparatus for supporting loads on board aircraft - Google Patents

Improvements in or relating to apparatus for supporting loads on board aircraft

Info

Publication number
GB956020A
GB956020A GB3790361A GB3790361A GB956020A GB 956020 A GB956020 A GB 956020A GB 3790361 A GB3790361 A GB 3790361A GB 3790361 A GB3790361 A GB 3790361A GB 956020 A GB956020 A GB 956020A
Authority
GB
United Kingdom
Prior art keywords
frame
aircraft
rails
loads
secured
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
Application number
GB3790361A
Inventor
Armand Georges Ricard
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.)
Ateliers dAviation Louis Breguet SA
Original Assignee
Ateliers dAviation Louis Breguet SA
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 Ateliers dAviation Louis Breguet SA filed Critical Ateliers dAviation Louis Breguet SA
Publication of GB956020A publication Critical patent/GB956020A/en
Expired legal-status Critical Current

Links

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
    • B64D1/00Dropping, ejecting, releasing, or receiving articles, liquids, or the like, in flight
    • B64D1/02Dropping, ejecting, or releasing articles
    • B64D1/04Dropping, ejecting, or releasing articles the articles being explosive, e.g. bombs
    • 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
    • B64D1/00Dropping, ejecting, releasing, or receiving articles, liquids, or the like, in flight
    • B64D1/02Dropping, ejecting, or releasing articles
    • B64D1/04Dropping, ejecting, or releasing articles the articles being explosive, e.g. bombs
    • B64D1/06Bomb releasing; Bomb doors

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Magnetic Bearings And Hydrostatic Bearings (AREA)

Abstract

956,020. Aircraft. SOC. ANON. DES ATELIERS D'AVIATION LOUIS BREQUET. Oct. 23, 1961 [Nov. 17, 1960], No. 37903/61. Headings B7G and B7W. [Also in Division F3] A structure for releasably supporting loads in aircraft comprises one or more frames 4 having means 18 for releasably attaching one or more loads 19, means being provided to displace the frame relatively to the aircraft on longitudinally extending tracks and so shift the load relatively to the centre of gravity of the aircraft, further means being provided to secure the frame in a selected position. Each frame 4 comprises a pair of box girders 5 interconnected by stays and carrying trunnions 6 at each end. On each trunnion is mounted a spider 7 having three radial legs in which rollers 8 are journalled to co-operate with the flanges of channel shaped rails 3 secured to the walls 2 of the stowage compartment in the aircraft. In addition at each end of the frame 4 is mounted a roller 10, which abuts the edge of flange 3a and so prevents lateral displacement of the frame. To lock the frame at a selected position along the rails, at least one trunnion carries a pin 11, Fig. 3, which can be moved by means of a handle 13, sliding in a U-shaped slot 14, into and out of engagement with holes 12 spaced along the rail 3. Preferably additional support means are provided and comprise overhead rails 15 parallel to rails 3 but of smaller section. U-shaped attaching means 16 carried by the girders 5 are secured to the rails 15 by inserting pins 17 into co-operating holes in the members 16 and 15. Loads 19, such as bombs or containers, are suspended from the frame and may be released by remote control. Arcuate arms 18 pivoted on the frame 4 bear against opposing sides of the loads and are simultaneously rotated into and out of position by linkage 21, 23 connected to bevel gearing which is rotated by means of a crank 25. To load the frame 4, a winch 26 is used in conjunction with a pulley 29 on the frame 4.
GB3790361A 1960-11-17 1961-10-23 Improvements in or relating to apparatus for supporting loads on board aircraft Expired GB956020A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR844215A FR1280071A (en) 1960-11-17 1960-11-17 Device for securing loads, which may or may not be dropped, in an aircraft hold

Publications (1)

Publication Number Publication Date
GB956020A true GB956020A (en) 1964-04-22

Family

ID=8742885

Family Applications (1)

Application Number Title Priority Date Filing Date
GB3790361A Expired GB956020A (en) 1960-11-17 1961-10-23 Improvements in or relating to apparatus for supporting loads on board aircraft

Country Status (2)

Country Link
FR (1) FR1280071A (en)
GB (1) GB956020A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4168047A (en) * 1975-07-03 1979-09-18 R. Alkan & Cie Automatic load carrier and jettisoning system with built-in hoisting means

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108820212B (en) * 2018-06-11 2023-12-22 天津航天中为数据系统科技有限公司 Aircraft with load-transmitting function

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4168047A (en) * 1975-07-03 1979-09-18 R. Alkan & Cie Automatic load carrier and jettisoning system with built-in hoisting means

Also Published As

Publication number Publication date
FR1280071A (en) 1961-12-29

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