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FR3129367B1 - AIRCRAFT LANDING GEAR HOUSING HATCH - Google Patents

AIRCRAFT LANDING GEAR HOUSING HATCH Download PDF

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Publication number
FR3129367B1
FR3129367B1 FR2112531A FR2112531A FR3129367B1 FR 3129367 B1 FR3129367 B1 FR 3129367B1 FR 2112531 A FR2112531 A FR 2112531A FR 2112531 A FR2112531 A FR 2112531A FR 3129367 B1 FR3129367 B1 FR 3129367B1
Authority
FR
France
Prior art keywords
landing gear
gear housing
panel side
aircraft
aircraft landing
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.)
Active
Application number
FR2112531A
Other languages
French (fr)
Other versions
FR3129367A1 (en
Inventor
Aline Scotto
Maxime Itasse
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 SAS
Original Assignee
Airbus Operations 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 Airbus Operations SAS filed Critical Airbus Operations SAS
Priority to FR2112531A priority Critical patent/FR3129367B1/en
Publication of FR3129367A1 publication Critical patent/FR3129367A1/en
Application granted granted Critical
Publication of FR3129367B1 publication Critical patent/FR3129367B1/en
Active 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
    • B64C25/001—Devices not provided for in the groups B64C25/02 - B64C25/68
    • 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
    • B64C2025/003—Means for reducing landing gear noise, or turbulent flow around it, e.g. landing gear doors used as deflectors

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Gear Transmission (AREA)

Abstract

TRAPPE DE LOGEMENT DE TRAIN D’ATTERRISSAGE D’AÉRONEF L’invention concerne une trappe de logement de train d’atterrissage d’aéronef (140) comprenant un premier côté de panneau orienté vers l’intérieur relativement au logement de train d’atterrissage lorsque la trappe est fermée et orienté vers un côté d’une jambe principale (110) d’un train d’atterrissage (100) déployé lorsque la trappe est ouverte, un second côté de panneau (141) opposé et un élément de guidage d’écoulement d’air (150). L’élément de guidage d’écoulement d’air est attaché au premier côté de panneau et s’étend à partir de celui-ci, et est attaché à un emplacement du premier côté de panneau qui est situé derrière la jambe principale. L’écoulement d’air (1001) est guidé par l’élément de guidage d’écoulement d’air de sorte qu’il s’éloigne du premier côté de panneau et passe derrière la jambe principale. L’invention concerne également un système de train d’atterrissage d’aéronef, un aéronef, des procédés de manœuvre d’un aéronef et un procédé de réduction de bruit. Figure accompagnant l’abrégé : Figure 1aAIRCRAFT LANDING GEAR HOUSING DOOR An aircraft landing gear housing door (140) includes a first panel side facing inward relative to the landing gear housing when the hatch is closed and oriented towards one side of a main leg (110) of a landing gear (100) deployed when the hatch is open, a second opposite panel side (141) and a guide member of air flow (150). The airflow guide member is attached to and extends from the first panel side, and is attached to a location on the first panel side that is located behind the main leg. The airflow (1001) is guided by the airflow guide member so that it flows away from the first panel side and passes behind the main leg. The invention also relates to an aircraft landing gear system, an aircraft, methods of maneuvering an aircraft, and a method of noise reduction. Figure accompanying the abstract: Figure 1a

FR2112531A 2021-11-25 2021-11-25 AIRCRAFT LANDING GEAR HOUSING HATCH Active FR3129367B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR2112531A FR3129367B1 (en) 2021-11-25 2021-11-25 AIRCRAFT LANDING GEAR HOUSING HATCH

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR2112531A FR3129367B1 (en) 2021-11-25 2021-11-25 AIRCRAFT LANDING GEAR HOUSING HATCH
FR2112531 2021-11-25

Publications (2)

Publication Number Publication Date
FR3129367A1 FR3129367A1 (en) 2023-05-26
FR3129367B1 true FR3129367B1 (en) 2024-04-12

Family

ID=80122388

Family Applications (1)

Application Number Title Priority Date Filing Date
FR2112531A Active FR3129367B1 (en) 2021-11-25 2021-11-25 AIRCRAFT LANDING GEAR HOUSING HATCH

Country Status (1)

Country Link
FR (1) FR3129367B1 (en)

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2005096721A2 (en) * 2004-03-29 2005-10-20 Rohr, Inc. Landing gear noise attenuation
US8695915B1 (en) 2011-03-11 2014-04-15 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Flap side edge liners for airframe noise reduction
US8944364B2 (en) * 2012-11-30 2015-02-03 The Boeing Company Quiet landing gear door

Also Published As

Publication number Publication date
FR3129367A1 (en) 2023-05-26

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