DE4203168C1 - - Google Patents

Info

Publication number
DE4203168C1
DE4203168C1 DE4203168A DE4203168A DE4203168C1 DE 4203168 C1 DE4203168 C1 DE 4203168C1 DE 4203168 A DE4203168 A DE 4203168A DE 4203168 A DE4203168 A DE 4203168A DE 4203168 C1 DE4203168 C1 DE 4203168C1
Authority
DE
Germany
Prior art keywords
cone
housing
longitudinal axis
connecting element
supporting structure
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 - Fee Related
Application number
DE4203168A
Other languages
German (de)
English (en)
Inventor
Guenther 2800 Bremen De Vogg
Wilfried 2805 Stuhr De Eilenstein Wiegmann
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 Operations GmbH
Original Assignee
Airbus Operations GmbH
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 Airbus Operations GmbH filed Critical Airbus Operations GmbH
Priority to DE4203168A priority Critical patent/DE4203168C1/de
Priority to EP93100109A priority patent/EP0554658B1/de
Priority to US08/014,332 priority patent/US5397078A/en
Application granted granted Critical
Publication of DE4203168C1 publication Critical patent/DE4203168C1/de
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/18—Floors
    • B64C1/20—Floors specially adapted for freight
    • 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
    • B64D9/00—Equipment for handling freight; Equipment for facilitating passenger embarkation or the like
    • B64D9/003—Devices for retaining pallets or freight containers

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Jigs For Machine Tools (AREA)
  • Connection Of Plates (AREA)
  • Furniture Connections (AREA)
DE4203168A 1992-02-05 1992-02-05 Expired - Fee Related DE4203168C1 (enExample)

Priority Applications (3)

Application Number Priority Date Filing Date Title
DE4203168A DE4203168C1 (enExample) 1992-02-05 1992-02-05
EP93100109A EP0554658B1 (de) 1992-02-05 1993-01-07 Vorrichtung zur Ausrichtung und Befestigung von Paletten in Flugzeugen
US08/014,332 US5397078A (en) 1992-02-05 1993-02-05 Apparatus for aligning and securing pallets in an aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE4203168A DE4203168C1 (enExample) 1992-02-05 1992-02-05

Publications (1)

Publication Number Publication Date
DE4203168C1 true DE4203168C1 (enExample) 1993-02-25

Family

ID=6450949

Family Applications (1)

Application Number Title Priority Date Filing Date
DE4203168A Expired - Fee Related DE4203168C1 (enExample) 1992-02-05 1992-02-05

Country Status (3)

Country Link
US (1) US5397078A (enExample)
EP (1) EP0554658B1 (enExample)
DE (1) DE4203168C1 (enExample)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE19634791C1 (de) * 1996-08-29 1997-12-04 Daimler Benz Aerospace Airbus X-Riegelelement für ein System zum Verriegeln von Luftfrachtladeeinheiten in einem Frachtladeraum eines Flugzeuges
US5730540A (en) * 1996-09-03 1998-03-24 Lockheed Martin Corporation Hole filling receptacle assembly
US6039519A (en) * 1998-06-25 2000-03-21 Mcdonnell Douglas Corporation Impact-resistant restraint for cargo
US7980796B1 (en) * 2009-05-01 2011-07-19 The Boeing Company Mechanical lock stop system and method
US8221038B1 (en) 2010-02-26 2012-07-17 Angra International, LLC. Overridable side lock (stabber) pallet type load restraint
US8496205B2 (en) 2010-05-03 2013-07-30 Ancra International, Llc Dual pivot pallet type cargo load restraint
US20120061518A1 (en) * 2010-09-10 2012-03-15 Winegard Company Apparatus and method for quickly releasing a dome in a domed satellite antenna
US8337127B2 (en) 2011-04-26 2012-12-25 Ancra International, Llc Latch arrangement for cargo restraint

Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2614871A (en) * 1951-06-30 1952-10-21 Adams Rite Mfg Company Anchor for cargo tie-down devices
DE3122366A1 (de) * 1981-06-05 1982-12-23 Messerschmitt-Bölkow-Blohm GmbH, 8000 München "verbindungseinrichtung zur befestigung von einbauelementen"
DE3206331A1 (de) * 1982-02-22 1983-09-01 Vereinigte Flugtechnische Werke Gmbh, 2800 Bremen Vorrichtung zum schnellen verbinden und loesen von riegeln
US4771969A (en) * 1987-07-27 1988-09-20 Sabre Industries, Inc. Leg set track fitting
US4796873A (en) * 1985-03-26 1989-01-10 Barry Wright Corporation Active vibration isolation system
US4856738A (en) * 1987-03-07 1989-08-15 British Aerospace Public Limited Company Adjustable seating arrangement for aircraft
US5058829A (en) * 1990-01-12 1991-10-22 Weber Aircraft Seat track fitting
US5083726A (en) * 1989-05-10 1992-01-28 Sabre Industries, Inc. Seat track bearing for an airplane
DE4115815C1 (en) * 1991-04-27 1992-06-17 Walter Dipl.-Ing. Michler (Fh), 8088 Eching, De Quick-action component fastener with bolt(s) - which is fitted to body slidable longitudinally w.r.t. fastener
DE4102273A1 (de) * 1991-01-26 1992-07-30 Airbus Gmbh Anschlusselement

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2339130A (en) * 1941-04-17 1944-01-11 Jeremiah W Albin Threaded attachment
US3912206A (en) * 1974-03-01 1975-10-14 Mc Donnell Douglas Corp Load lift and skid pad assembly
US4000870A (en) * 1975-09-08 1977-01-04 Western Gear Corporation Modular system for quick conversion of aircraft passenger compartments to cargo baggage/compartments
US4232497A (en) * 1979-02-21 1980-11-11 Albin Meschnig Device for securing platelike elements to a carrying structure at a distance therefrom
US4341496A (en) * 1979-11-23 1982-07-27 Western Gear Corporation Seat pallet lock
US4830557A (en) * 1988-01-26 1989-05-16 General Electric Company Self-aligning floating nut fastener
GB2223554B (en) * 1988-08-26 1992-07-22 Titus Tool Co Ltd Adjustable fixing device
US4929136A (en) * 1989-03-17 1990-05-29 Spar Aerospace Limited Floating Matable element
US5104070A (en) * 1989-06-01 1992-04-14 Space Industries, Inc. Structural latch for vehicle coupling mechanisms

Patent Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2614871A (en) * 1951-06-30 1952-10-21 Adams Rite Mfg Company Anchor for cargo tie-down devices
DE3122366A1 (de) * 1981-06-05 1982-12-23 Messerschmitt-Bölkow-Blohm GmbH, 8000 München "verbindungseinrichtung zur befestigung von einbauelementen"
DE3206331A1 (de) * 1982-02-22 1983-09-01 Vereinigte Flugtechnische Werke Gmbh, 2800 Bremen Vorrichtung zum schnellen verbinden und loesen von riegeln
US4796873A (en) * 1985-03-26 1989-01-10 Barry Wright Corporation Active vibration isolation system
US4856738A (en) * 1987-03-07 1989-08-15 British Aerospace Public Limited Company Adjustable seating arrangement for aircraft
US4771969A (en) * 1987-07-27 1988-09-20 Sabre Industries, Inc. Leg set track fitting
US5083726A (en) * 1989-05-10 1992-01-28 Sabre Industries, Inc. Seat track bearing for an airplane
US5058829A (en) * 1990-01-12 1991-10-22 Weber Aircraft Seat track fitting
DE4102273A1 (de) * 1991-01-26 1992-07-30 Airbus Gmbh Anschlusselement
DE4115815C1 (en) * 1991-04-27 1992-06-17 Walter Dipl.-Ing. Michler (Fh), 8088 Eching, De Quick-action component fastener with bolt(s) - which is fitted to body slidable longitudinally w.r.t. fastener

Also Published As

Publication number Publication date
US5397078A (en) 1995-03-14
EP0554658A1 (de) 1993-08-11
EP0554658B1 (de) 1995-11-22

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Legal Events

Date Code Title Description
8100 Publication of patent without earlier publication of application
D1 Grant (no unexamined application published) patent law 81
8327 Change in the person/name/address of the patent owner

Owner name: DEUTSCHE AEROSPACE AIRBUS GMBH, 2000 HAMBURG, DE

8364 No opposition during term of opposition
8327 Change in the person/name/address of the patent owner

Owner name: DAIMLER-BENZ AEROSPACE AIRBUS GMBH, 21129 HAMBURG,

8327 Change in the person/name/address of the patent owner

Owner name: DAIMLERCHRYSLER AEROSPACE AIRBUS GMBH, 21129 HAMBU

8327 Change in the person/name/address of the patent owner

Owner name: EADS AIRBUS GMBH, 21129 HAMBURG, DE

8327 Change in the person/name/address of the patent owner

Owner name: AIRBUS DEUTSCHLAND GMBH, 21129 HAMBURG, DE

8327 Change in the person/name/address of the patent owner

Owner name: AIRBUS OPERATIONS GMBH, 21129 HAMBURG, DE

R119 Application deemed withdrawn, or ip right lapsed, due to non-payment of renewal fee

Effective date: 20110901