FR2898866B1 - Distributeur hydraulique pour train d'atterrissage d'avion - Google Patents
Distributeur hydraulique pour train d'atterrissage d'avionInfo
- Publication number
- FR2898866B1 FR2898866B1 FR0650993A FR0650993A FR2898866B1 FR 2898866 B1 FR2898866 B1 FR 2898866B1 FR 0650993 A FR0650993 A FR 0650993A FR 0650993 A FR0650993 A FR 0650993A FR 2898866 B1 FR2898866 B1 FR 2898866B1
- Authority
- FR
- France
- Prior art keywords
- aircraft landing
- hydraulic distributor
- landing train
- train
- distributor
- 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
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
- B64C25/18—Operating mechanisms
- B64C25/22—Operating mechanisms fluid
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
- F15B—SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
- F15B13/00—Details of servomotor systems ; Valves for servomotor systems
- F15B13/02—Fluid distribution or supply devices characterised by their adaptation to the control of servomotors
- F15B13/04—Fluid distribution or supply devices characterised by their adaptation to the control of servomotors for use with a single servomotor
- F15B13/042—Fluid distribution or supply devices characterised by their adaptation to the control of servomotors for use with a single servomotor operated by fluid pressure
- F15B13/043—Fluid distribution or supply devices characterised by their adaptation to the control of servomotors for use with a single servomotor operated by fluid pressure with electrically-controlled pilot valves
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
- F15B—SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
- F15B13/00—Details of servomotor systems ; Valves for servomotor systems
- F15B13/02—Fluid distribution or supply devices characterised by their adaptation to the control of servomotors
- F15B13/06—Fluid distribution or supply devices characterised by their adaptation to the control of servomotors for use with two or more servomotors
- F15B13/08—Assemblies of units, each for the control of a single servomotor only
- F15B13/0803—Modular units
- F15B13/0807—Manifolds
- F15B13/0814—Monoblock manifolds
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
- F15B—SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
- F15B13/00—Details of servomotor systems ; Valves for servomotor systems
- F15B13/02—Fluid distribution or supply devices characterised by their adaptation to the control of servomotors
- F15B13/06—Fluid distribution or supply devices characterised by their adaptation to the control of servomotors for use with two or more servomotors
- F15B13/08—Assemblies of units, each for the control of a single servomotor only
- F15B13/0803—Modular units
- F15B13/0832—Modular valves
- F15B13/0842—Monoblock type valves, e.g. with multiple valve spools in a common housing
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49229—Prime mover or fluid pump making
- Y10T29/49236—Fluid pump or compressor making
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- General Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Fluid-Pressure Circuits (AREA)
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0650993A FR2898866B1 (fr) | 2006-03-22 | 2006-03-22 | Distributeur hydraulique pour train d'atterrissage d'avion |
US11/689,715 US7810755B2 (en) | 2006-03-22 | 2007-03-22 | Hydraulic distributor for airplane landing gear |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0650993A FR2898866B1 (fr) | 2006-03-22 | 2006-03-22 | Distributeur hydraulique pour train d'atterrissage d'avion |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2898866A1 FR2898866A1 (fr) | 2007-09-28 |
FR2898866B1 true FR2898866B1 (fr) | 2008-11-21 |
Family
ID=37492375
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR0650993A Expired - Fee Related FR2898866B1 (fr) | 2006-03-22 | 2006-03-22 | Distributeur hydraulique pour train d'atterrissage d'avion |
Country Status (2)
Country | Link |
---|---|
US (1) | US7810755B2 (fr) |
FR (1) | FR2898866B1 (fr) |
Families Citing this family (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB0717903D0 (en) * | 2007-09-14 | 2007-10-31 | Airbus Uk Ltd | Method and apparatus for providing power in an aircraft to one or more aircraft systems |
FR2933670B1 (fr) * | 2008-07-08 | 2011-04-08 | Airbus France | Systeme d'ouverture et de fermeture de trappe pour case de train d'atterrissage d'un aeronef |
GB2469484B (en) * | 2009-04-15 | 2013-09-18 | Ge Aviat Systems Ltd | Landing gear actuation control system |
USD638342S1 (en) * | 2010-04-21 | 2011-05-24 | Messier-Dowty Sa | Connecting rod |
USD638776S1 (en) * | 2010-04-21 | 2011-05-31 | Messier-Dowty Sa | Connecting rod |
USD638775S1 (en) * | 2010-04-21 | 2011-05-31 | Messier-Dowty Sa | Connecting rod |
USD632633S1 (en) * | 2010-09-04 | 2011-02-15 | Messier-Dowty Sa | Part of landing gear |
FR2966428B1 (fr) * | 2010-10-20 | 2013-08-02 | Messier Bugatti | Circuit hydraulique d'actionnement d'un atterrisseur et procedes de deploiement et de relevage d'un atterrisseur utilisant un tel circuit. |
GB201113030D0 (en) * | 2011-07-28 | 2011-09-14 | Airbus Operations Ltd | Aircraft landing gear |
JP6170755B2 (ja) * | 2013-06-18 | 2017-07-26 | 住友精密工業株式会社 | 電動油圧アクチュエータ |
GB2563437A (en) * | 2017-06-16 | 2018-12-19 | Airbus Operations Ltd | Landing gear controller |
FR3088898B1 (fr) * | 2018-11-23 | 2020-12-18 | Safran Landing Systems | Circuit hydraulique de manœuvre de train d’atterrissage d’aéronef |
US11124293B2 (en) * | 2019-04-23 | 2021-09-21 | Goodrich Corporation | Integral bracket manifold for landing gear assemblies |
US11619311B2 (en) * | 2020-06-08 | 2023-04-04 | The Boeing Company | Flow control valve, a method of assembly, and a hydraulic system |
FR3111620B1 (fr) * | 2020-06-23 | 2022-07-01 | Safran Landing Systems | Dispositif de verrouillage d’atterrisseur |
FR3148575B1 (fr) * | 2023-05-11 | 2025-04-18 | Safran Landing Systems | Système d’actionnement hydraulique d’atterrisseur et aéronef en comportant. |
FR3156754A1 (fr) * | 2023-12-14 | 2025-06-20 | Safran Landing Systems | Bloc modulaire de distribution hydraulique pour système d’actionnement d’atterrisseurs d’aéronef |
Family Cites Families (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2701695A (en) * | 1949-08-18 | 1955-02-08 | Mcdonnell Aircraft Corp | Hydraulic interlock for retractable landing gear and closure operators for the chambers therefor |
US3107886A (en) * | 1961-11-09 | 1963-10-22 | Kaman Aircraft Corp | Hydraulic system for aircraft landing gear and hydraulic actuator therefor |
FR2061559B2 (fr) * | 1969-06-27 | 1974-06-14 | Messier Hispano Sa | |
FR2529859A1 (fr) * | 1982-07-12 | 1984-01-13 | Messier Hispano Sa | Bloc integre de commande des atterrisseurs pour aeronef |
US4573649A (en) * | 1983-08-01 | 1986-03-04 | The Boeing Company | Integrated alternate gear extension and ground-crew door opening/closing system for an aircraft |
GB0214119D0 (en) * | 2002-06-19 | 2002-07-31 | Airbus Uk Ltd | Landing gear door assembly |
DE10330805B4 (de) * | 2003-07-08 | 2015-07-30 | Liebherr-Aerospace Lindenberg Gmbh | Luftfahrzeug-Fahrwerksbetätigung |
US6854689B1 (en) * | 2004-02-09 | 2005-02-15 | The Boeing Company | Methods and systems for operating aircraft landing gears |
FR2875475B1 (fr) * | 2004-09-21 | 2008-02-08 | Airbus France Sas | Systeme de manoeuvre d'un train d'atterrissage pour aeronef et aeronef comportant un tel systeme |
-
2006
- 2006-03-22 FR FR0650993A patent/FR2898866B1/fr not_active Expired - Fee Related
-
2007
- 2007-03-22 US US11/689,715 patent/US7810755B2/en not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
FR2898866A1 (fr) | 2007-09-28 |
US7810755B2 (en) | 2010-10-12 |
US20080277525A1 (en) | 2008-11-13 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
CA | Change of address |
Effective date: 20110916 |
|
CD | Change of name or company name |
Owner name: AIRBUS HOLDING, FR Effective date: 20110916 |
|
CJ | Change in legal form |
Effective date: 20110916 |
|
TP | Transmission of property |
Owner name: AIRBUS HOLDING, FR Effective date: 20110913 |
|
PLFP | Fee payment |
Year of fee payment: 11 |
|
PLFP | Fee payment |
Year of fee payment: 12 |
|
PLFP | Fee payment |
Year of fee payment: 13 |
|
PLFP | Fee payment |
Year of fee payment: 15 |
|
ST | Notification of lapse |
Effective date: 20211105 |