GB1456978A - Arrangement for suspension and dropping of loads - Google Patents

Arrangement for suspension and dropping of loads

Info

Publication number
GB1456978A
GB1456978A GB5669073A GB5669073A GB1456978A GB 1456978 A GB1456978 A GB 1456978A GB 5669073 A GB5669073 A GB 5669073A GB 5669073 A GB5669073 A GB 5669073A GB 1456978 A GB1456978 A GB 1456978A
Authority
GB
United Kingdom
Prior art keywords
load
pins
hooks
housing
lever
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
GB5669073A
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.)
Airbus Defence and Space GmbH
Original Assignee
Messerschmitt Bolkow Blohm AG
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 Messerschmitt Bolkow Blohm AG filed Critical Messerschmitt Bolkow Blohm AG
Publication of GB1456978A publication Critical patent/GB1456978A/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
    • B64D1/06Bomb releasing; Bombs doors

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Load-Engaging Elements For Cranes (AREA)
  • Clamps And Clips (AREA)

Abstract

1456978 Suspension and dropping of loads MESSERSCHMITT - BOLKOW - BLOHM GmbH 6 Dec 1973 [14 Dec 1972] 56690/73 Heading F3C An arrangement for the suspension and dropping of a load from an aircraft, wherein the load is suspended from pivoted hooks, steadied by members which are urged towards the load and, is ejected by means which are actuated by a combustible charge. The arrangement has hollow pins 10a, 10B, Fig. 1, which extend into depressions 11, 12 respectively in the load 2 and has hooks 4, 4 which engage lugs 3, 3 respectively, the lugs being mounted on the load 2. The hooks 4, 4 each pivot about a fulcrum 5 on a housing 1 and are each connected with a respective push-rod 6, so that, when cartridges in housings 15 are ignited, pressurized-gas acts on a piston in a cylinder 8 to move a lever 9 which actuates the push-rods 6, via rod 7, to release the hooks 4 from the lugs 3. The pressurizedgas also passes along conduits 16, 16 in the housing 1 to move pistons 14, 14 in the respective pins 10a, 10b, the pistons being urged against portions 13, 13 of the load 2 ejecting the latter. The load is steadied by arms 17, Fig. 3, which are carried by the housing 1 and are provided with bearing plates 18 having screw-thread adjusting means. In another embodiment a load 20, Fig. 5, having four lugs 3 is suspended by four hooks 4 and is guided by four pins 21 in housings 1, 1. The pins 21 serve as cylinders for ejection pistons 14 and are resiliently mounted in the housings by springs 22. A depression 11, Fig. 7, in the load 20 accurately locates one pin 21. Another pin 21 is received in a slot 12 and the other two pins 21 are received with clearance in a respective depression 23. The pins are guided by bushes 24, Fig. 5, which are screwed into the housing 1 and also serve to steady the load 20. Lever 9 is connected with a lever 25 which interconnects the two housings via a lever 26 and an actuating shaft 27, Fig. 6. Thus the hooks can be released even if one of the cartridges fails to ignite. In a further embodiment a load 30, Fig. 8, is provided with suspension fittings 32, Fig. 11, each having two lateral apertures 33 which are engaged by hook parts 34, Fig. 10, of a double hook 31. Each fitting 32 has a bore 35, Fig. 11, and is provided with a collar 36 by which the fitting 32 is received in the load 30 and secured by a screw 37, Fig. 8. The housing 1 has two flanges 38 into which are screwed bolts 39 on which pins 40 are resiliently mounted by springs 41. Ejection pistons 14 are provided and act directly on the load 30. Wedges 42, 42, Fig. 10, for each double hook 31 are inserted between the respective fitting 32 and the respective flange 38 of the housing 1. The load 30 is suspended prior to the insertion of the wedges.
GB5669073A 1972-12-14 1973-12-06 Arrangement for suspension and dropping of loads Expired GB1456978A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19722261173 DE2261173C3 (en) 1972-12-14 1972-12-14 Device for detachable fixing

Publications (1)

Publication Number Publication Date
GB1456978A true GB1456978A (en) 1976-12-01

Family

ID=5864391

Family Applications (1)

Application Number Title Priority Date Filing Date
GB5669073A Expired GB1456978A (en) 1972-12-14 1973-12-06 Arrangement for suspension and dropping of loads

Country Status (4)

Country Link
DE (1) DE2261173C3 (en)
FR (1) FR2210538B1 (en)
GB (1) GB1456978A (en)
IT (1) IT1002224B (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2182125A (en) * 1985-10-25 1987-05-07 British Aerospace Store adaptor

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2316468A1 (en) * 1975-07-01 1977-01-28 Alkan R & Cie DUAL-PURPOSE HOOK FOR CARRYING LOADS ON AIRCRAFT
FR2345346A1 (en) * 1976-03-22 1977-10-21 Alkan R & Cie EJECTOR ALLOWING THE CARGO OF LOADS UNDER PLANE, WHETHER EQUIPPED WITH RINGS OR PARTS CALLED SADDLES
GB1529087A (en) * 1976-04-30 1978-10-18 Westland Aircraft Ltd Store ejector release units
DE2644127C3 (en) * 1976-09-30 1981-09-17 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Carrying and dropping device for loads on carrier vehicles
FR2370948A1 (en) * 1976-11-16 1978-06-09 Alkan R & Cie AZIMUT HARMONIZATION DEVICE FOR A LOAD TAKEN UNDER AIRCRAFT
US4182502A (en) * 1976-11-16 1980-01-08 R. Alkan & Cie Device for the bearing harmonization of an airborne load
FR2376026A1 (en) * 1977-01-03 1978-07-28 Alkan R & Cie AUTOMATIC TIMING DEVICE FOR LOADS TAKEN ON AIRCRAFT
DE3136320C2 (en) * 1981-09-12 1983-10-20 Deutsche Forschungs- und Versuchsanstalt für Luft- und Raumfahrt e.V., 5000 Köln Method and device for suppressing the external load wing flutter of aircraft
FR2563181B1 (en) * 1984-04-20 1986-08-08 Alkan R & Cie DEVICE FOR HARMONIZING AN AZIMUTH OF A PYLON FOR CARRYING LOADS UNDER AIRCRAFT
FR2734785B1 (en) * 1995-05-31 1997-08-22 Aerospatiale DEVICE FOR HANGING CARRIAGES UNDER A CARRIAGE MAT EQUIPPED WITH AN AIRCRAFT
FR2768503B1 (en) 1997-09-16 1999-12-03 Aerospatiale DEVICE FOR AUTOMATICALLY CONTROLLING AT LEAST ONE MOBILE ELEMENT SUCH AS A VENTRAL MISSILE DRIFT
CN107560498B (en) * 2017-10-16 2019-08-30 北京航天发射技术研究所 A kind of rocket body propulsion device

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2182125A (en) * 1985-10-25 1987-05-07 British Aerospace Store adaptor

Also Published As

Publication number Publication date
FR2210538A1 (en) 1974-07-12
DE2261173B2 (en) 1978-09-28
IT1002224B (en) 1976-05-20
FR2210538B1 (en) 1978-10-27
DE2261173A1 (en) 1974-06-20
DE2261173C3 (en) 1979-06-13

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Legal Events

Date Code Title Description
PS Patent sealed
PCNP Patent ceased through non-payment of renewal fee