GB2094875B - Self-release mechanism - Google Patents

Self-release mechanism

Info

Publication number
GB2094875B
GB2094875B GB8107644A GB8107644A GB2094875B GB 2094875 B GB2094875 B GB 2094875B GB 8107644 A GB8107644 A GB 8107644A GB 8107644 A GB8107644 A GB 8107644A GB 2094875 B GB2094875 B GB 2094875B
Authority
GB
United Kingdom
Prior art keywords
self
release mechanism
release
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
GB8107644A
Other versions
GB2094875A (en
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.)
Lockheed Martin UK Ampthill Ltd
Original Assignee
Hunting Engineering Ltd
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 Hunting Engineering Ltd filed Critical Hunting Engineering Ltd
Priority to GB8107644A priority Critical patent/GB2094875B/en
Publication of GB2094875A publication Critical patent/GB2094875A/en
Application granted granted Critical
Publication of GB2094875B publication Critical patent/GB2094875B/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
    • F16B21/00—Means for preventing relative axial movement of a pin, spigot, shaft or the like and a member surrounding it; Stud-and-socket releasable fastenings
    • F16B21/06—Releasable fastening devices with snap-action
    • F16B21/07—Releasable fastening devices with snap-action in which the socket has a resilient part
    • F16B21/071—Releasable fastening devices with snap-action in which the socket has a resilient part the socket being integrally formed with a component to be fasted, e.g. a sheet, plate or strip
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT 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

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Connection Of Plates (AREA)
GB8107644A 1981-03-11 1981-03-11 Self-release mechanism Expired GB2094875B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB8107644A GB2094875B (en) 1981-03-11 1981-03-11 Self-release mechanism

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB8107644A GB2094875B (en) 1981-03-11 1981-03-11 Self-release mechanism

Publications (2)

Publication Number Publication Date
GB2094875A GB2094875A (en) 1982-09-22
GB2094875B true GB2094875B (en) 1985-02-27

Family

ID=10520311

Family Applications (1)

Application Number Title Priority Date Filing Date
GB8107644A Expired GB2094875B (en) 1981-03-11 1981-03-11 Self-release mechanism

Country Status (1)

Country Link
GB (1) GB2094875B (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102010031750B4 (en) * 2010-07-21 2012-07-12 Eads Deutschland Gmbh Detachable connection arrangement for attaching externally droppable loads to an aircraft

Also Published As

Publication number Publication date
GB2094875A (en) 1982-09-22

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Legal Events

Date Code Title Description
PE20 Patent expired after termination of 20 years

Effective date: 20010310