FR3018501B1 - DEVICE AND METHOD FOR THE ACTIVE CONTROL OF THE LANDING TRAIN OF AN AIRCRAFT - Google Patents

DEVICE AND METHOD FOR THE ACTIVE CONTROL OF THE LANDING TRAIN OF AN AIRCRAFT

Info

Publication number
FR3018501B1
FR3018501B1 FR1452425A FR1452425A FR3018501B1 FR 3018501 B1 FR3018501 B1 FR 3018501B1 FR 1452425 A FR1452425 A FR 1452425A FR 1452425 A FR1452425 A FR 1452425A FR 3018501 B1 FR3018501 B1 FR 3018501B1
Authority
FR
France
Prior art keywords
aircraft
leg
pillar
active control
pivot
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
FR1452425A
Other languages
French (fr)
Other versions
FR3018501A1 (en
Inventor
Samuel Chevrollier
Pierre Parpaite
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.)
Socata SAS
Original Assignee
Socata SAS
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 Socata SAS filed Critical Socata SAS
Priority to FR1452425A priority Critical patent/FR3018501B1/en
Publication of FR3018501A1 publication Critical patent/FR3018501A1/en
Application granted granted Critical
Publication of FR3018501B1 publication Critical patent/FR3018501B1/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C25/00—Alighting gear
    • B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface 
    • B64C25/58—Arrangements or adaptations of shock-absorbers or springs
    • B64C25/60—Oleo legs
    • 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
    • B64C25/001—Devices not provided for in the groups B64C25/02 - B64C25/68
    • B64C2025/008—Comprising means for modifying their length, e.g. for kneeling, for jumping, or for leveling the aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Tires In General (AREA)
  • Transmission Devices (AREA)

Abstract

L'invention concerne un aéronef comportant un train d'atterrissage dit actif, ledit train comprenant : a. une jambe (131), dite pilier, en liaison pivot avec la structure de l'aéronef ; b. une jambe (132), dite de support, en liaison pivot avec la jambe (131) pilier selon un axe (135) parallèle à l'axe de tangage de l'aéronef et portant un moyen (140) de liaison au sol de l'aéronef ; c. un vérin (150) apte à déplacer la jambe (132) de support relativement à la jambe (131) pilier selon une rotation autour du pivot (135) de liaison entre les deux jambes ; d. des moyens (160) pour déplacer la jambe (131) pilier par rapport à la structure de l'aéronef autour de l'axe (125) de liaison pivot de cette jambe avec ladite structure.The invention relates to an aircraft comprising a so-called active landing gear, said landing gear comprising: a. a leg (131), called a pillar, in pivot connection with the structure of the aircraft; b. a so-called support leg (132) in a pivot connection with the pillar leg (131) along an axis (135) parallel to the pitch axis of the aircraft and carrying a means (140) for connecting the ground to the aircraft; vs. a jack (150) capable of moving the support leg (132) relative to the pillar leg (131) according to a rotation about the pivot (135) connecting the two legs; d. means (160) for moving the pillar leg (131) relative to the structure of the aircraft around the pivot link axis (125) of this leg with said structure.

FR1452425A 2014-03-16 2014-03-23 DEVICE AND METHOD FOR THE ACTIVE CONTROL OF THE LANDING TRAIN OF AN AIRCRAFT Expired - Fee Related FR3018501B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR1452425A FR3018501B1 (en) 2014-03-16 2014-03-23 DEVICE AND METHOD FOR THE ACTIVE CONTROL OF THE LANDING TRAIN OF AN AIRCRAFT

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1452161A FR3018500A1 (en) 2014-03-16 2014-03-16 DEVICE AND METHOD FOR THE ACTIVE CONTROL OF THE LANDING TRAIN OF AN AIRCRAFT
FR1452425A FR3018501B1 (en) 2014-03-16 2014-03-23 DEVICE AND METHOD FOR THE ACTIVE CONTROL OF THE LANDING TRAIN OF AN AIRCRAFT

Publications (2)

Publication Number Publication Date
FR3018501A1 FR3018501A1 (en) 2015-09-18
FR3018501B1 true FR3018501B1 (en) 2017-12-08

Family

ID=51417348

Family Applications (2)

Application Number Title Priority Date Filing Date
FR1452161A Pending FR3018500A1 (en) 2014-03-16 2014-03-16 DEVICE AND METHOD FOR THE ACTIVE CONTROL OF THE LANDING TRAIN OF AN AIRCRAFT
FR1452425A Expired - Fee Related FR3018501B1 (en) 2014-03-16 2014-03-23 DEVICE AND METHOD FOR THE ACTIVE CONTROL OF THE LANDING TRAIN OF AN AIRCRAFT

Family Applications Before (1)

Application Number Title Priority Date Filing Date
FR1452161A Pending FR3018500A1 (en) 2014-03-16 2014-03-16 DEVICE AND METHOD FOR THE ACTIVE CONTROL OF THE LANDING TRAIN OF AN AIRCRAFT

Country Status (1)

Country Link
FR (2) FR3018500A1 (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2020142434A1 (en) * 2018-12-31 2020-07-09 DZYNE Technologies Incorporated Swing-arm pivot piston landing gear systems and methods
WO2020142457A1 (en) * 2018-12-31 2020-07-09 DZYNE Technologies Incorporated Tilting landing gear systems and methods

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10150558B2 (en) * 2016-06-30 2018-12-11 DZYNE Technologies Incorporated Tilting landing gear systems and methods
CN107010204B (en) * 2017-03-02 2019-05-31 江西洪都航空工业集团有限责任公司 A kind of design method of adjustable Quick Release rotating shaft mechanism
US10486798B2 (en) * 2017-04-18 2019-11-26 The Boeing Company Aircraft landing gear assembly and method of assembling the same
GB2602150A (en) * 2020-12-21 2022-06-22 Airbus Operations Ltd An aircraft landing gear
FR3132505A1 (en) * 2022-02-08 2023-08-11 Safran Landing Systems Leg for aircraft undercarriage equipped with an accumulator, undercarriage comprising such a leg and aircraft comprising at least one such undercarriage
US20240025536A1 (en) * 2022-07-21 2024-01-25 Blended Wing Aircraft, Inc. Non-coupled landing gear apparatus and methods of use

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1012604A (en) * 1962-12-03 1965-12-08 Dowty Rotol Ltd Aircraft undercarriages
GB1036934A (en) * 1963-07-29 1966-07-20 Dowty Rotol Ltd Improvements relating to aircraft
US3826450A (en) * 1973-06-04 1974-07-30 Lockheed Aircraft Corp Landing gear for stol airplanes
FR2393726A1 (en) * 1977-06-10 1979-01-05 Messier Hispano Sa IMPROVEMENTS TO LANDING BRAKES OF PULLED AND RETRACTION WHEEL SAILS
US4524929A (en) * 1982-09-30 1985-06-25 Grumman Aerospace Corporation Short take off jump mode for airplane landing gear struts
EP0461981A3 (en) * 1990-06-13 1993-08-04 Messier Bugatti Spring-damper unit with variable stroke for a vehicle
FR2702446B1 (en) * 1993-03-08 1995-06-09 Messier Bugatti LIFTABLE LANDING GEAR FOR LARGE AIRCRAFT.
IL138399A (en) * 1998-03-19 2004-01-04 Goodrich Co B F Dual mode positioner for an aircraft landing gear axle beam
US6120009A (en) * 1998-04-16 2000-09-19 The Boeing Company Shock strut with managed damping and force characteristics
US6575405B2 (en) * 1999-03-30 2003-06-10 The Boeing Company Control system and method for a semi-levered landing gear for an aircraft
US7249736B2 (en) * 2005-06-23 2007-07-31 Northrop Grumman Corporation Process for landing a tailless aircraft

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2020142434A1 (en) * 2018-12-31 2020-07-09 DZYNE Technologies Incorporated Swing-arm pivot piston landing gear systems and methods
WO2020142457A1 (en) * 2018-12-31 2020-07-09 DZYNE Technologies Incorporated Tilting landing gear systems and methods

Also Published As

Publication number Publication date
FR3018501A1 (en) 2015-09-18
FR3018500A1 (en) 2015-09-18

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