EP0950006A1 - Aircraft landing gear arrangement - Google Patents
Aircraft landing gear arrangementInfo
- Publication number
- EP0950006A1 EP0950006A1 EP97947160A EP97947160A EP0950006A1 EP 0950006 A1 EP0950006 A1 EP 0950006A1 EP 97947160 A EP97947160 A EP 97947160A EP 97947160 A EP97947160 A EP 97947160A EP 0950006 A1 EP0950006 A1 EP 0950006A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- gear
- aircraft
- bearing
- mounting
- arrangement
- 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- Withdrawn
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/02—Undercarriages
- B64C25/08—Undercarriages non-fixed, e.g. jettisonable
- B64C25/10—Undercarriages non-fixed, e.g. jettisonable retractable, foldable, or the like
- B64C25/12—Undercarriages non-fixed, e.g. jettisonable retractable, foldable, or the like sideways
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
Definitions
- This invention concerns aircraft landing gear arrangements and in particular an arrangement for an
- aircraft main landing gear mounted at least in part from a
- aircraft comprises a main oleo strut supporting wheels
- the trunnion bearings are arranged to pivot
- aft trunnion bearing is pivotally attached to a gear beam
- an aircraft landing gear arrangement including a main oleo strut having forward and aft trunnion bearings,
- the mounting for the forward trunnion bearing may
- the gear beam may be mounted at one end to the rear spar
- the mounting for the aft trunnion bearing may be
- the mounting for the aft trunnion bearing may
- a supplemental bearing having a pivotal axis
- the supplemental bearing may comprise
- the supplemental bearing may conveniently be
- invention includes an end bearing at either end of the
- gear beam for rotatably mounting the gear beam to the rear
- fusible locating means may be provided. Such fusible
- locating means may be located in the vicinity of one or
- fusible locating means may comprise at least one strut
- the aft trunnion bearing may permit limited
- gear beam about a longitudinal axis of the gear beam.
- the aft trunnion bearing may include an
- Figure 1 is a rear isometric view of a main
- Figure 2 is a sectional view taken on the line
- Figure 3 is a rear isometric view of a main
- Figure 4 is an enlarged part sectional view of the
- Figure 5 is a horizontal section taken through a
- Figure 6 shows the arrangement of Figure 3 with
- Figure 7 shows the arrangement of Figure 6
- Figure 8 is a rear isometric view of a main
- Figure 9 is a part sectional view through a gear
- Figure 10 is a horizontal part sectional view of a
- FIG 11 shows the arrangement of Figure 8 with
- Figure 12 shows the arrangement of Figure 11 with
- Figure 13 is a rear isometric view of a main
- Figure 14 is an enlarged detail view of detail XIV
- main landing gear arrangement 1 according to the prior art
- the arrangement comprises a wing rear spar 2, an aircraft fuselage 3 , a landing gear beam 4 attached at
- a main landing gear oleo strut 7 is shown
- the oleo strut has a forward trunnion
- the forward trunnion bearing housing is secured to the rear
- fuse pins 12 connected between the forward trunnion bearing housing 9 and a forward trunnion fitting 14.
- the rear trunnion bearing housing 11 is rotatable
- Trunnions 16, 17, are rotatable in
- a wall 23 of the recess in the gear beam is of adequate
- End bearing 26 rotatably mounts end 5 of the
- the end bearing 26 has an eyelet 29 for the passage of a
- longitudinal axis 15 is controlled by a control strut 34
- gear beam 4 to rotate about its longitudinal axis with the
- control strut 34 is
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- General Details Of Gearings (AREA)
- Tires In General (AREA)
- Gear Transmission (AREA)
Abstract
Description
Claims
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB9625241A GB2320002A (en) | 1996-12-04 | 1996-12-04 | Aircraft landing gear arrangement |
GB9625241 | 1996-12-04 | ||
PCT/GB1997/003319 WO1998024688A1 (en) | 1996-12-04 | 1997-12-02 | Aircraft landing gear arrangement |
Publications (1)
Publication Number | Publication Date |
---|---|
EP0950006A1 true EP0950006A1 (en) | 1999-10-20 |
Family
ID=10803958
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP97947160A Withdrawn EP0950006A1 (en) | 1996-12-04 | 1997-12-02 | Aircraft landing gear arrangement |
Country Status (4)
Country | Link |
---|---|
EP (1) | EP0950006A1 (en) |
EA (1) | EA000886B1 (en) |
GB (1) | GB2320002A (en) |
WO (1) | WO1998024688A1 (en) |
Families Citing this family (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB9818084D0 (en) * | 1998-08-20 | 1998-10-14 | British Aerospace | An adjustable size annular retaining assembly |
FR2787760B1 (en) * | 1998-12-29 | 2001-03-02 | Aerospatiale | AIRCRAFT LANDING GEAR, EQUIPPED WITH A DEVICE FOR PROTECTING A NEAR FUEL TANK, AND AIRCRAFT COMPRISING SUCH A TRAIN |
FR2867151B1 (en) * | 2004-03-04 | 2007-05-25 | Airbus France | FUSELAGE LONGERON FOR AN AIRCRAFT AND CENTRAL BOX EQUIPPED WITH SUCH A LONGERON |
GB2417933A (en) * | 2004-09-10 | 2006-03-15 | Airbus Uk Ltd | Landing gear support assembly for an aircraft |
FR2901536B1 (en) | 2006-05-23 | 2009-01-30 | Airbus France Sas | BEAM FOR PRESSURIZED FLOOR OF AIRCRAFT |
DE102007011611B4 (en) * | 2007-01-22 | 2010-12-09 | Airbus Deutschland Gmbh | Fixing arrangement for lashing strap in a cargo hold floor of an aircraft |
FR2913412B1 (en) | 2007-03-05 | 2012-12-07 | Airbus France | CONTAINER FOR AERIAL FREIGHT TRANSPORT AND AIRCRAFT FUSELAGE FOR FREIGHT TRANSPORT. |
GB201114437D0 (en) * | 2011-08-22 | 2011-10-05 | Airbus Operations Ltd | Landing gear attachment |
US9315254B2 (en) * | 2013-10-11 | 2016-04-19 | The Boeing Company | Joint assembly and method of assembling same |
BR102013032347B1 (en) * | 2013-12-16 | 2023-03-07 | Yaborã Indústria Aeronáutica S.A. | FIXING AIRCRAFT LANDING GEAR AND AIRCRAFT |
US11260965B2 (en) * | 2019-04-15 | 2022-03-01 | The Boeing Company | Aircraft landing gear forward trunnion support assemblies and related methods |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2061496B1 (en) * | 1969-02-03 | 1974-02-22 | Messier Hispano Sa | |
FR2081135B1 (en) * | 1970-03-09 | 1973-03-16 | Snecma | |
FR2348851A1 (en) * | 1976-04-22 | 1977-11-18 | Messier Hispano Sa | LANDING GEAR CONTAINING A SAFETY DEVICE WITH PREDETERMINED BREAKING LOAD |
US4328939A (en) * | 1979-12-26 | 1982-05-11 | The Boeing Company | Airplane main landing gear assembly |
US4345727A (en) * | 1979-12-26 | 1982-08-24 | The Boeing Company | Body-braced main airplane landing gear |
US4392623A (en) * | 1980-12-22 | 1983-07-12 | The Boeing Company | Fused connection adapted to fail under different overloads acting in different directions |
US4392622A (en) * | 1980-12-22 | 1983-07-12 | The Boeing Company | Combined beam support for landing gear |
-
1996
- 1996-12-04 GB GB9625241A patent/GB2320002A/en not_active Withdrawn
-
1997
- 1997-12-02 WO PCT/GB1997/003319 patent/WO1998024688A1/en not_active Application Discontinuation
- 1997-12-02 EA EA199900586A patent/EA000886B1/en not_active IP Right Cessation
- 1997-12-02 EP EP97947160A patent/EP0950006A1/en not_active Withdrawn
Non-Patent Citations (1)
Title |
---|
See references of WO9824688A1 * |
Also Published As
Publication number | Publication date |
---|---|
GB2320002A (en) | 1998-06-10 |
WO1998024688A1 (en) | 1998-06-11 |
GB9625241D0 (en) | 1997-01-22 |
EA000886B1 (en) | 2000-06-26 |
EA199900586A1 (en) | 2000-02-28 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PUAI | Public reference made under article 153(3) epc to a published international application that has entered the european phase |
Free format text: ORIGINAL CODE: 0009012 |
|
17P | Request for examination filed |
Effective date: 19990723 |
|
AK | Designated contracting states |
Kind code of ref document: A1 Designated state(s): DE ES FR GB IT NL SE |
|
RAP1 | Party data changed (applicant data changed or rights of an application transferred) |
Owner name: BAE SYSTEMS PLC |
|
GRAG | Despatch of communication of intention to grant |
Free format text: ORIGINAL CODE: EPIDOS AGRA |
|
RIN1 | Information on inventor provided before grant (corrected) |
Inventor name: HIGGINS, NIGEL, BRITISH AEROSPACE AIRBUS LIMITED |
|
17Q | First examination report despatched |
Effective date: 20010327 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: THE APPLICATION IS DEEMED TO BE WITHDRAWN |
|
18D | Application deemed to be withdrawn |
Effective date: 20010703 |