FR2357419A1 - Release mechanism for aeroplane load - is for low level operations and has guide fixed to aircraft floor attached to parachute canopy - Google Patents

Release mechanism for aeroplane load - is for low level operations and has guide fixed to aircraft floor attached to parachute canopy

Info

Publication number
FR2357419A1
FR2357419A1 FR7621057A FR7621057A FR2357419A1 FR 2357419 A1 FR2357419 A1 FR 2357419A1 FR 7621057 A FR7621057 A FR 7621057A FR 7621057 A FR7621057 A FR 7621057A FR 2357419 A1 FR2357419 A1 FR 2357419A1
Authority
FR
France
Prior art keywords
load
parachute canopy
release mechanism
sledge
aeroplane
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.)
Withdrawn
Application number
FR7621057A
Other languages
French (fr)
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.)
Etudes et Fabrications Aeronautiques SA
Original Assignee
Etudes et Fabrications Aeronautiques 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 Etudes et Fabrications Aeronautiques SA filed Critical Etudes et Fabrications Aeronautiques SA
Priority to FR7621057A priority Critical patent/FR2357419A1/en
Publication of FR2357419A1 publication Critical patent/FR2357419A1/en
Withdrawn legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D1/00—Dropping, ejecting, releasing, or receiving articles, liquids, or the like, in flight
    • B64D1/02—Dropping, ejecting, or releasing articles
    • B64D1/08—Dropping, ejecting, or releasing articles the articles being load-carrying devices
    • B64D1/12—Releasing

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Types And Forms Of Lifts (AREA)

Abstract

The load release mechanism consists of a detachable sledge (10) which locates in a guide fixed to the floor of the aircraft's hold and is attached to the parachute canopy. The interior of the aircraft's hold, which has rear doors, is provided with rollers which allow the load, mounted on a pallete (1), to be manoeuvred. The rear edge of the palette is fitted with bearings (11) which locate in a groove in the sledge. As the load is pushed forward towards the open aircraft hatch the sledge follows the guide and is twisted round, this action releasing the load and deploying the parachute canopy. The sledge finally leaves the guide and descends with the load.
FR7621057A 1976-07-09 1976-07-09 Release mechanism for aeroplane load - is for low level operations and has guide fixed to aircraft floor attached to parachute canopy Withdrawn FR2357419A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR7621057A FR2357419A1 (en) 1976-07-09 1976-07-09 Release mechanism for aeroplane load - is for low level operations and has guide fixed to aircraft floor attached to parachute canopy

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR7621057A FR2357419A1 (en) 1976-07-09 1976-07-09 Release mechanism for aeroplane load - is for low level operations and has guide fixed to aircraft floor attached to parachute canopy

Publications (1)

Publication Number Publication Date
FR2357419A1 true FR2357419A1 (en) 1978-02-03

Family

ID=9175498

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7621057A Withdrawn FR2357419A1 (en) 1976-07-09 1976-07-09 Release mechanism for aeroplane load - is for low level operations and has guide fixed to aircraft floor attached to parachute canopy

Country Status (1)

Country Link
FR (1) FR2357419A1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4303213A (en) * 1979-02-21 1981-12-01 The Boeing Company Tow plate

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4303213A (en) * 1979-02-21 1981-12-01 The Boeing Company Tow plate

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Legal Events

Date Code Title Description
CL Concession to grant licences
ST Notification of lapse