BR112014009351A2 - sistema de válvula de sangramento de ar para um sistema hidráulico de aeronave e método para sangrar excesso de ar a partir de um sistema hidráulico de aeronave - Google Patents
sistema de válvula de sangramento de ar para um sistema hidráulico de aeronave e método para sangrar excesso de ar a partir de um sistema hidráulico de aeronaveInfo
- Publication number
- BR112014009351A2 BR112014009351A2 BR112014009351A BR112014009351A BR112014009351A2 BR 112014009351 A2 BR112014009351 A2 BR 112014009351A2 BR 112014009351 A BR112014009351 A BR 112014009351A BR 112014009351 A BR112014009351 A BR 112014009351A BR 112014009351 A2 BR112014009351 A2 BR 112014009351A2
- Authority
- BR
- Brazil
- Prior art keywords
- aircraft hydraulic
- hydraulic system
- air
- aircraft
- bleed valve
- Prior art date
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16K—VALVES; TAPS; COCKS; ACTUATING-FLOATS; DEVICES FOR VENTING OR AERATING
- F16K24/00—Devices, e.g. valves, for venting or aerating enclosures
- F16K24/04—Devices, e.g. valves, for venting or aerating enclosures for venting only
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D17/00—Regulating or controlling by varying flow
- F01D17/20—Devices dealing with sensing elements or final actuators or transmitting means between them, e.g. power-assisted
- F01D17/22—Devices dealing with sensing elements or final actuators or transmitting means between them, e.g. power-assisted the operation or power assistance being predominantly non-mechanical
- F01D17/26—Devices dealing with sensing elements or final actuators or transmitting means between them, e.g. power-assisted the operation or power assistance being predominantly non-mechanical fluid, e.g. hydraulic
-
- 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
- F15B21/00—Common features of fluid actuator systems; Fluid-pressure actuator systems or details thereof, not covered by any other group of this subclass
- F15B21/04—Special measures taken in connection with the properties of the fluid
- F15B21/044—Removal or measurement of undissolved gas, e.g. de-aeration, venting or bleeding
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16K—VALVES; TAPS; COCKS; ACTUATING-FLOATS; DEVICES FOR VENTING OR AERATING
- F16K24/00—Devices, e.g. valves, for venting or aerating enclosures
-
- 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
- Y10T137/00—Fluid handling
- Y10T137/0318—Processes
-
- 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
- Y10T137/00—Fluid handling
- Y10T137/0318—Processes
- Y10T137/0324—With control of flow by a condition or characteristic of a fluid
- Y10T137/0379—By fluid pressure
-
- 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
- Y10T137/00—Fluid handling
- Y10T137/2931—Diverse fluid containing pressure systems
- Y10T137/3115—Gas pressure storage over or displacement of liquid
- Y10T137/3143—With liquid level responsive gas vent or whistle
-
- 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
- Y10T137/00—Fluid handling
- Y10T137/7722—Line condition change responsive valves
- Y10T137/7758—Pilot or servo controlled
- Y10T137/7759—Responsive to change in rate of fluid flow
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Analytical Chemistry (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Fluid-Pressure Circuits (AREA)
Abstract
resumo sistema de válvula de sangramento de ar para um sistema hidráulico de aeronave e método para sangrar excesso de ar a partir de um sistema hidráulico de aeronave a presente invenção apresenta um sistema de válvula de sangramento de ar hidráulico de aeronave (10) tendo uma válvula de ventilação de ar (32) conectada a um controlador eletrônico (14, 18), onde a abertura da válvula de ventilação de ar é permitida apenas quando a aeronave se encontrar em um pré-determinado modo de vôo, o modo de vôo de aeronave sendo determinado por um giroscópio (16) conectado ao controlador (14, 18). 1/1
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US13/274,384 US8833695B2 (en) | 2011-10-17 | 2011-10-17 | Aircraft hydraulic air bleed valve system |
PCT/IB2012/001993 WO2013057553A1 (en) | 2011-10-17 | 2012-10-09 | Aircraft hydraulic air bleed valve system |
Publications (1)
Publication Number | Publication Date |
---|---|
BR112014009351A2 true BR112014009351A2 (pt) | 2017-04-18 |
Family
ID=47189978
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BR112014009351A BR112014009351A2 (pt) | 2011-10-17 | 2012-10-09 | sistema de válvula de sangramento de ar para um sistema hidráulico de aeronave e método para sangrar excesso de ar a partir de um sistema hidráulico de aeronave |
Country Status (6)
Country | Link |
---|---|
US (2) | US8833695B2 (pt) |
EP (1) | EP2769057A1 (pt) |
CN (1) | CN103890321A (pt) |
BR (1) | BR112014009351A2 (pt) |
CA (1) | CA2850426A1 (pt) |
WO (1) | WO2013057553A1 (pt) |
Families Citing this family (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US8833695B2 (en) * | 2011-10-17 | 2014-09-16 | Eaton Corporation | Aircraft hydraulic air bleed valve system |
US9904296B2 (en) * | 2014-04-01 | 2018-02-27 | Honeywell International Inc. | Controlling flow in a fluid distribution system |
WO2016138309A1 (en) | 2015-02-26 | 2016-09-01 | Eaton Corporation | Bleed valve arrangements; and methods |
US10563784B2 (en) | 2016-02-24 | 2020-02-18 | Eaton Intelligent Power Limited | Pressurized fluid system including an automatic bleed value arrangement; components; and, methods |
BE1026218B1 (fr) * | 2018-04-19 | 2019-11-21 | Safran Aero Boosters S.A. | Dispositif de mesure de niveau pour réservoir d'huile de turbomachine |
Family Cites Families (38)
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US2451575A (en) * | 1946-02-20 | 1948-10-19 | Adel Prec Products Corp | Hydraulic selector valve |
US3708139A (en) * | 1959-01-19 | 1973-01-02 | Us Navy | Missile control system |
US3006580A (en) * | 1959-02-09 | 1961-10-31 | Clarkson Alick | Flight control means for aircraft |
US3027121A (en) * | 1960-12-30 | 1962-03-27 | Ii Roger W Griswold | Aerodynamic autopilot |
US3081788A (en) * | 1962-03-28 | 1963-03-19 | Thomas F Lewis | Air bleeder valve for hydraulic systems |
GB1092997A (en) * | 1965-02-24 | 1967-11-29 | British Aircraft Corp Ltd | Improvements relating to hydraulic servo systems |
GB1213853A (en) * | 1968-02-02 | 1970-11-25 | Muirhead Ltd | Improvements in and relating to ship stabilizers |
US4204457A (en) * | 1976-12-30 | 1980-05-27 | Parker-Hannifin Corporation | Device for controlling hydraulic motors |
DE3205846A1 (de) * | 1982-02-18 | 1983-08-25 | Knorr-Bremse GmbH, 8000 München | Fahrzeugbremsanlage, insbesondere hydraulische fahrzeugbremsanlage fuer schienenfahrzeuge |
US4494841A (en) * | 1983-09-12 | 1985-01-22 | Eastman Kodak Company | Acoustic transducers for acoustic position sensing apparatus |
US4524793A (en) | 1983-10-14 | 1985-06-25 | Pall Corporation | Automatic reservoir bleed valve |
US4813446A (en) | 1987-04-06 | 1989-03-21 | Pall Corporation | Automatic pressurized reservoir bleed valve |
US5033694A (en) * | 1989-09-08 | 1991-07-23 | Daiichi Electric Kabushiki Kaisha | Attitude control device for air or sea transportation craft |
US5220837A (en) * | 1992-03-27 | 1993-06-22 | Pall Corporation | Differential pressure transducer assembly |
US5305793A (en) * | 1992-09-16 | 1994-04-26 | Pall Corporation | Automatic pressurized reservoir bleed valve |
US5948044A (en) * | 1996-05-20 | 1999-09-07 | Harris Corporation | Hybrid GPS/inertially aided platform stabilization system |
US5743292A (en) * | 1996-10-07 | 1998-04-28 | Mcdonnell Douglas Corporation | Pressure actuated check valve |
WO1999018379A1 (en) * | 1997-10-02 | 1999-04-15 | Stant Manufacturing Inc. | Electronic fill limit control |
US7216055B1 (en) * | 1998-06-05 | 2007-05-08 | Crossbow Technology, Inc. | Dynamic attitude measurement method and apparatus |
AT3433U3 (de) * | 1999-12-30 | 2001-04-25 | Avl List Gmbh | System zur leitung von flüssigen medien sowie filtervorrichtung zur verwendung in diesem system |
US6654685B2 (en) * | 2002-01-04 | 2003-11-25 | The Boeing Company | Apparatus and method for navigation of an aircraft |
WO2004101357A2 (en) * | 2002-08-30 | 2004-11-25 | Qaxu Technology Inc. | Homeostatic flying hovercraft |
US7000474B2 (en) * | 2003-02-28 | 2006-02-21 | Elo Touchsystems, Inc. | Acoustic device using higher order harmonic piezoelectric element |
US7343232B2 (en) * | 2003-06-20 | 2008-03-11 | Geneva Aerospace | Vehicle control system including related methods and components |
US6799739B1 (en) * | 2003-11-24 | 2004-10-05 | The Boeing Company | Aircraft control surface drive system and associated methods |
US7000628B2 (en) * | 2004-01-26 | 2006-02-21 | Liquid Controls | Electronic air separation system |
US7637458B2 (en) * | 2005-06-08 | 2009-12-29 | The Boeing Company | Systems and methods for providing back-up hydraulic power for aircraft, including tanker aircraft |
WO2007123537A1 (en) * | 2006-04-20 | 2007-11-01 | Dover Electronics, Inc. (Dba Vectron International) | Electro acoustic sensor for high pressure environments |
US7739909B2 (en) * | 2006-11-08 | 2010-06-22 | Gm Global Technology Operations, Inc. | Acoustic fluid level monitoring |
WO2008063547A2 (en) * | 2006-11-16 | 2008-05-29 | Aai Corporation | Vehicle fuel system |
US8439065B2 (en) * | 2008-03-31 | 2013-05-14 | Parker-Hannifin Corporation | Automotive air bleed valve for a closed hydraulic system |
US8333217B2 (en) * | 2008-05-28 | 2012-12-18 | Eaton Corporation | Fault-tolerant bleed valve assembly |
US8265817B2 (en) * | 2008-07-10 | 2012-09-11 | Lockheed Martin Corporation | Inertial measurement with an imaging sensor and a digitized map |
GB2468345B (en) * | 2009-03-05 | 2014-01-15 | Cranfield Aerospace Ltd | Unmanned air vehicle (uav) control system and method |
US8272398B2 (en) * | 2009-03-18 | 2012-09-25 | Eaton Corporation | Liquid discriminating vent valve |
KR101655302B1 (ko) * | 2009-09-22 | 2016-09-07 | 삼성전자주식회사 | 표면 탄성파 센서 시스템 |
US20110236877A1 (en) * | 2010-03-26 | 2011-09-29 | Da-Jeng Yao | Biosensor and method using the same to perform a biotest |
US8833695B2 (en) * | 2011-10-17 | 2014-09-16 | Eaton Corporation | Aircraft hydraulic air bleed valve system |
-
2011
- 2011-10-17 US US13/274,384 patent/US8833695B2/en active Active
-
2012
- 2012-10-09 EP EP12787497.2A patent/EP2769057A1/en not_active Withdrawn
- 2012-10-09 WO PCT/IB2012/001993 patent/WO2013057553A1/en active Application Filing
- 2012-10-09 CA CA 2850426 patent/CA2850426A1/en not_active Abandoned
- 2012-10-09 CN CN201280050840.8A patent/CN103890321A/zh active Pending
- 2012-10-09 BR BR112014009351A patent/BR112014009351A2/pt not_active IP Right Cessation
-
2014
- 2014-08-19 US US14/462,782 patent/US20140352791A1/en not_active Abandoned
Also Published As
Publication number | Publication date |
---|---|
WO2013057553A1 (en) | 2013-04-25 |
US20130092245A1 (en) | 2013-04-18 |
CA2850426A1 (en) | 2013-04-25 |
CN103890321A (zh) | 2014-06-25 |
US20140352791A1 (en) | 2014-12-04 |
EP2769057A1 (en) | 2014-08-27 |
US8833695B2 (en) | 2014-09-16 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
B08F | Application dismissed because of non-payment of annual fees [chapter 8.6 patent gazette] | ||
B08K | Patent lapsed as no evidence of payment of the annual fee has been furnished to inpi [chapter 8.11 patent gazette] |