BRPI0816826A2 - Acionamento hidráulico, dispositivo de abastecimento hidráulico, avião com um dispositivo de abastecimento hidráulico, bem como, processo para a configuração de um dispositivo de abastecimento hidráulico - Google Patents

Acionamento hidráulico, dispositivo de abastecimento hidráulico, avião com um dispositivo de abastecimento hidráulico, bem como, processo para a configuração de um dispositivo de abastecimento hidráulico

Info

Publication number
BRPI0816826A2
BRPI0816826A2 BRPI0816826-1A2A BRPI0816826A BRPI0816826A2 BR PI0816826 A2 BRPI0816826 A2 BR PI0816826A2 BR PI0816826 A BRPI0816826 A BR PI0816826A BR PI0816826 A2 BRPI0816826 A2 BR PI0816826A2
Authority
BR
Brazil
Prior art keywords
supply device
hydraulic supply
hydraulic
plane
setting
Prior art date
Application number
BRPI0816826-1A2A
Other languages
English (en)
Inventor
Juergen Laude
Original Assignee
Airbus Operations Gmbh
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 Gmbh filed Critical Airbus Operations Gmbh
Publication of BRPI0816826A2 publication Critical patent/BRPI0816826A2/pt

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02—Aircraft characterised by the type or position of power plants
    • B64D27/16—Aircraft characterised by the type or position of power plants of jet type
    • B64D27/18—Aircraft characterised by the type or position of power plants of jet type within, or attached to, wings
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/40—Arrangements for mounting power plants in aircraft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
    • 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
    • F01D15/00—Adaptations of machines or engines for special use; Combinations of engines with devices driven thereby
    • F01D15/08—Adaptations for driving, or combinations with, pumps
    • 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
    • F01D21/00—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/22—Fuel supply systems
    • F02C7/236—Fuel delivery systems comprising two or more pumps
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/32—Arrangement, mounting, or driving, of auxiliaries
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
    • F02C9/26—Control of fuel supply
    • F02C9/46—Emergency fuel control
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2240/00—Components
    • F05D2240/40—Use of a multiplicity of similar components
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00—Function
    • F05D2260/40—Transmission of power
    • F05D2260/402—Transmission of power through friction drives
    • F05D2260/4023—Transmission of power through friction drives through a friction clutch
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00—Function
    • F05D2260/80—Diagnostics
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00—Function
    • F05D2260/84—Redundancy
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00—Function
    • F05D2260/85—Starting
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2270/00—Control
    • F05D2270/50—Control logic embodiments
    • F05D2270/56—Control logic embodiments by hydraulic means, e.g. hydraulic valves within a hydraulic circuit
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2270/00—Control
    • F05D2270/60—Control system actuates means
    • F05D2270/64—Hydraulic actuators

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Fluid-Pressure Circuits (AREA)
  • Control Of Fluid Gearings (AREA)
  • General Details Of Gearings (AREA)
  • Control Of Positive-Displacement Pumps (AREA)
  • Rotary Pumps (AREA)
BRPI0816826-1A2A 2007-09-17 2008-09-17 Acionamento hidráulico, dispositivo de abastecimento hidráulico, avião com um dispositivo de abastecimento hidráulico, bem como, processo para a configuração de um dispositivo de abastecimento hidráulico BRPI0816826A2 (pt)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US97283807P 2007-09-17 2007-09-17
DE102007044229A DE102007044229A1 (de) 2007-09-17 2007-09-17 Luftfahrzeug, Triebwerksanordnung und Triebwerksträger
PCT/EP2008/007778 WO2009036970A2 (de) 2007-09-17 2008-09-17 Hydraulikantrieb, hydraulikversorgungs-vorrichtung, flugzeug mit einer hydraulikversorgungs-vorrichtung sowie verfahren zur konfiguration einer hydraulikversorgungs-vorrichtung

Publications (1)

Publication Number Publication Date
BRPI0816826A2 true BRPI0816826A2 (pt) 2015-03-10

Family

ID=40348610

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0816826-1A2A BRPI0816826A2 (pt) 2007-09-17 2008-09-17 Acionamento hidráulico, dispositivo de abastecimento hidráulico, avião com um dispositivo de abastecimento hidráulico, bem como, processo para a configuração de um dispositivo de abastecimento hidráulico

Country Status (9)

Country Link
US (1) US9022318B2 (pt)
EP (1) EP2201234A2 (pt)
JP (1) JP2010538888A (pt)
CN (1) CN101802368B (pt)
BR (1) BRPI0816826A2 (pt)
CA (1) CA2699693A1 (pt)
DE (1) DE102007044229A1 (pt)
RU (1) RU2010115183A (pt)
WO (1) WO2009036970A2 (pt)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9719428B2 (en) * 2007-11-30 2017-08-01 United Technologies Corporation Gas turbine engine with pylon mounted accessory drive
FR2944261B1 (fr) * 2009-04-14 2013-01-04 Airbus France Systeme de generation de puissance electrique pour aeronef a propulsion arriere
FR2977637B1 (fr) * 2011-07-04 2015-07-24 Hispano Suiza Sa Boitier de relais d'accessoires d'une turbine a gaz integrant des moyens de desaccouplement
FR2979957B1 (fr) * 2011-09-13 2014-02-14 Snecma Procede de suivi du rendement volumetrique d'une pompe hp d'un systeme de regulation hydraulique de turbomachine
EP3099917B1 (en) * 2014-01-29 2023-10-11 Nuovo Pignone Tecnologie - S.r.l. A compressor train with a stirling engine
US9759094B2 (en) 2015-06-24 2017-09-12 General Electric Company Pump for a turbine engine
DE102017124049B4 (de) 2017-10-16 2023-02-23 Rolls-Royce Deutschland Ltd & Co Kg Flugzeug mit einem Strahltriebwerk
DE102017124043A1 (de) * 2017-10-16 2019-04-18 Rolls-Royce Deutschland Ltd & Co Kg Strahltriebwerk mit einer Anbindungsvorrichtung
FR3123377B1 (fr) 2021-05-27 2023-05-19 Safran Aircraft Engines Ensemble de supportage d’une boite d’accessoires d’une turbomachine d'aéronef

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US2296006A (en) * 1938-11-28 1942-09-15 Wagner Herbert Driving means for mechanism for multimotored airplanes
US2409159A (en) * 1944-08-26 1946-10-08 Allis Chalmers Mfg Co Elastic fluid conditioning apparatus
DE854893C (de) * 1944-11-05 1952-11-06 Daimler Benz Ag Anlasseinrichtung an Flugzeugen mit mehr als zwei an den Tragfluegeln angeordneten Triebwerken
GB626036A (en) * 1947-08-08 1949-07-07 Bristol Aeroplane Co Ltd Improvements in or relating to gas-turbine engines
US2509813A (en) * 1947-09-29 1950-05-30 Stratos Corp Emergency disconnect means for auxiliaries
US2978869A (en) * 1956-11-01 1961-04-11 Bristol Siddeley Engines Ltd Engine accessory mounting arrangements
US2978209A (en) * 1957-09-02 1961-04-04 Rolls Royce Aircraft gas-turbine power plant installation
US3220218A (en) * 1963-12-30 1965-11-30 Gen Electric Device for disconnecting engine driven aircraft accessories
FR2152362B1 (pt) * 1971-09-07 1974-05-10 Snecma
US3965673A (en) * 1973-05-19 1976-06-29 Vereinigte Flugtechnische Werke-Fokker Gesellschaft Mit Beschrankter Haftung Apparatus for starting aircraft engines and for operating auxiliary on-board power generating equipment
US4068470A (en) * 1974-11-08 1978-01-17 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Gas turbine engine with convertible accessories
DE2519152C2 (de) * 1975-04-30 1982-11-25 Vereinigte Flugtechnische Werke Gmbh, 2800 Bremen Vorrichtung zum Anlassen von Flugzeugtriebwerken und zum Betreiben von Flugzeughilfsgeräten
US4456425A (en) * 1980-11-20 1984-06-26 General Electric Company Modular inlet gearbox for a gas turbine engine
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FR2662756B1 (fr) * 1990-06-05 1992-08-14 Snecma Dispositif de transmission etanche entre deux arbres coaxiaux montes dans des boitiers fixes l'un a l'autre, autorisant une intervention rapide notamment en cas de fuite.
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Also Published As

Publication number Publication date
US9022318B2 (en) 2015-05-05
DE102007044229A1 (de) 2009-03-19
WO2009036970A2 (de) 2009-03-26
CN101802368A (zh) 2010-08-11
JP2010538888A (ja) 2010-12-16
EP2201234A2 (de) 2010-06-30
CA2699693A1 (en) 2009-03-26
US20100193631A1 (en) 2010-08-05
RU2010115183A (ru) 2011-10-27
WO2009036970A3 (de) 2009-12-03
CN101802368B (zh) 2015-06-17

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Legal Events

Date Code Title Description
B11A Dismissal acc. art.33 of ipl - examination not requested within 36 months of filing
B11Y Definitive dismissal - extension of time limit for request of examination expired [chapter 11.1.1 patent gazette]