IN2015DN02248A - - Google Patents

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Publication number
IN2015DN02248A
IN2015DN02248A IN2248DEN2015A IN2015DN02248A IN 2015DN02248 A IN2015DN02248 A IN 2015DN02248A IN 2248DEN2015 A IN2248DEN2015 A IN 2248DEN2015A IN 2015DN02248 A IN2015DN02248 A IN 2015DN02248A
Authority
IN
India
Prior art keywords
linkage
gearbox
actuator
box
piston
Prior art date
Application number
Other languages
English (en)
Inventor
Borgne Eric; Le
Alexandre; Machin
Original Assignee
Turbomeca
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 Turbomeca filed Critical Turbomeca
Publication of IN2015DN02248A publication Critical patent/IN2015DN02248A/en

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
    • B64C13/24—Transmitting means
    • B64C13/38—Transmitting means with power amplification
    • B64C13/40—Transmitting means with power amplification using fluid pressure
    • 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
    • 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
    • B64D41/00—Power installations for auxiliary purposes
    • 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
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02K—DYNAMO-ELECTRIC MACHINES
    • H02K5/00—Casings; Enclosures; Supports
    • H02K5/04—Casings or enclosures characterised by the shape, form or construction thereof
    • H02K5/10—Casings or enclosures characterised by the shape, form or construction thereof with arrangements for protection from ingress, e.g. water or fingers
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02K—DYNAMO-ELECTRIC MACHINES
    • H02K7/00—Arrangements for handling mechanical energy structurally associated with dynamo-electric machines, e.g. structural association with mechanical driving motors or auxiliary dynamo-electric machines
    • H02K7/06—Means for converting reciprocating motion into rotary motion or vice versa
    • 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
    • F05D2220/00—Application
    • F05D2220/30—Application in turbines
    • F05D2220/32—Application in turbines in gas turbines
    • F05D2220/329—Application in turbines in gas turbines in helicopters
    • 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
    • F05D2260/403—Transmission of power through the shape of the drive components
    • F05D2260/4031—Transmission of power through the shape of the drive components as in toothed gearing

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Power Engineering (AREA)
  • Automation & Control Theory (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Actuator (AREA)
  • Transmission Devices (AREA)
  • Gear-Shifting Mechanisms (AREA)
IN2248DEN2015 2012-09-05 2013-08-27 IN2015DN02248A (zh)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1258289A FR2994939B1 (fr) 2012-09-05 2012-09-05 Boitier a accessoires pour la commande de volets d'un aeronef
PCT/FR2013/051978 WO2014037650A1 (fr) 2012-09-05 2013-08-27 Boitier a accessoires pour la commande de volets d'un aéronef

Publications (1)

Publication Number Publication Date
IN2015DN02248A true IN2015DN02248A (zh) 2015-08-21

Family

ID=47178131

Family Applications (1)

Application Number Title Priority Date Filing Date
IN2248DEN2015 IN2015DN02248A (zh) 2012-09-05 2013-08-27

Country Status (12)

Country Link
US (1) US9758238B2 (zh)
EP (1) EP2892806B1 (zh)
JP (1) JP6321652B2 (zh)
KR (1) KR102103043B1 (zh)
CN (1) CN104903195B (zh)
CA (1) CA2883842C (zh)
ES (1) ES2586489T3 (zh)
FR (1) FR2994939B1 (zh)
IN (1) IN2015DN02248A (zh)
PL (1) PL2892806T3 (zh)
RU (1) RU2629835C2 (zh)
WO (1) WO2014037650A1 (zh)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3045007B1 (fr) * 2015-12-14 2017-11-24 Airbus Operations Sas Commande d'un aeronef comprenant une pedale accouplee a un verin et dispositif de commandes associe

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SU67060A1 (ru) * 1944-06-26 1945-11-30 М.П. Медведев Устройство дл управлени рул ми самолета
DE2325592C2 (de) * 1973-05-19 1982-08-26 Vereinigte Flugtechnische Werke Gmbh, 2800 Bremen Anordnung zum Anfahren von Flugzeuggasturbinentriebwerken und zum Betreiben von Flugzeughilfsgeräten
JPH074902U (ja) * 1993-06-28 1995-01-24 帝人製機株式会社 多重油圧シリンダ
US7364116B2 (en) * 2004-09-27 2008-04-29 The Boeing Company Automatic control systems for aircraft auxiliary power units, and associated methods
FR2901315B1 (fr) 2006-05-19 2010-09-10 Hispano Suiza Sa Boitier d'accessoires dans un moteur d'avion tel qu'un turboreacteur
DE102006030450A1 (de) * 2006-06-29 2008-01-03 Fte Automotive Gmbh Hydraulische Stellvorrichtung für die Betätigung einer Schaltstange insbesondere eines Schaltgetriebes für Kraftfahrzeuge
US20110146434A1 (en) * 2009-12-18 2011-06-23 Short Keith E Jack shaft disconnect
US8796892B2 (en) * 2009-12-18 2014-08-05 Hamilton Sundstrand Corporation Multi-pole generator packaging arrangement having a disconnection system
FR2968716B1 (fr) * 2010-12-13 2012-12-28 Turbomeca Procede de controle de la generation electrique appliquee a une turbine a gaz d'aeronef et turbomoteur mettant en oeuvre un tel procede
US9994304B2 (en) * 2014-10-01 2018-06-12 Nabtesco Corporation Hydraulic actuator

Also Published As

Publication number Publication date
WO2014037650A1 (fr) 2014-03-13
EP2892806B1 (fr) 2016-07-13
CA2883842A1 (fr) 2014-03-13
FR2994939A1 (fr) 2014-03-07
CA2883842C (fr) 2020-06-23
CN104903195A (zh) 2015-09-09
JP2015528412A (ja) 2015-09-28
RU2629835C2 (ru) 2017-09-04
US20150232171A1 (en) 2015-08-20
RU2015109721A (ru) 2016-10-27
KR102103043B1 (ko) 2020-04-21
FR2994939B1 (fr) 2014-08-22
CN104903195B (zh) 2016-11-16
KR20150052096A (ko) 2015-05-13
ES2586489T3 (es) 2016-10-14
PL2892806T3 (pl) 2016-11-30
JP6321652B2 (ja) 2018-05-09
US9758238B2 (en) 2017-09-12
EP2892806A1 (fr) 2015-07-15

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