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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
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—Arrangement 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)

Abstract

The invention relates to an accessory drive gearbox for an aircraft turbine engine, said gearbox (140) comprising a box (42), a linkage (115) for controlling flaps of the aircraft, which linkage is designed to slide axially inside said gearbox (140), and an actuator (120) for driving said linkage (115) and mounted on said box (42) , said actuator (120) comprising a hollow body (121) , a piston (123) designed for translational movement inside said body (121) and a piston rod (112) connected to said piston (123) and extending at least partially outside the body (121) of the actuator (120), said rod (122) being connected to the linkage (115) , the gearbox (140) being characterized in that the body (121) of the actuator (120) is positioned between the connection between the rod (112) and the linkage (115), and the box (42) of the gearbox (140).
IN2248DEN2015 2012-09-05 2013-08-27 IN2015DN02248A (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1258289A FR2994939B1 (en) 2012-09-05 2012-09-05 ACCESSORIES HOUSING FOR CONTROLLING SHUTTERS OF AN AIRCRAFT
PCT/FR2013/051978 WO2014037650A1 (en) 2012-09-05 2013-08-27 Accessory drive gearbox for controlling the flaps of an aircraft

Publications (1)

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

Family

ID=47178131

Family Applications (1)

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

Country Status (12)

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

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3045007B1 (en) * 2015-12-14 2017-11-24 Airbus Operations Sas CONTROL OF AN AIRCRAFT COMPRISING A PEDAL FITTED TO A CYLINDER AND CONTROL DEVICE THEREFOR

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SU67060A1 (en) * 1944-06-26 1945-11-30 М.П. Медведев Device to control the rudders of the aircraft
DE2325592C2 (en) * 1973-05-19 1982-08-26 Vereinigte Flugtechnische Werke Gmbh, 2800 Bremen Arrangement for starting up aircraft gas turbine engines and for operating aircraft auxiliary equipment
JPH074902U (en) * 1993-06-28 1995-01-24 帝人製機株式会社 Multiple hydraulic cylinder
US7364116B2 (en) * 2004-09-27 2008-04-29 The Boeing Company Automatic control systems for aircraft auxiliary power units, and associated methods
FR2901315B1 (en) * 2006-05-19 2010-09-10 Hispano Suiza Sa ACCESSORIES HOUSING IN AN AIRCRAFT ENGINE SUCH AS A TURBOREACTOR
DE102006030450A1 (en) * 2006-06-29 2008-01-03 Fte Automotive Gmbh Hydraulic actuating device for the actuation of a shift rod, in particular a manual transmission for motor vehicles
US20110148235A1 (en) * 2009-12-18 2011-06-23 Lemmers Jr Glenn C Generator packaging arrangement
US20110146434A1 (en) * 2009-12-18 2011-06-23 Short Keith E Jack shaft disconnect
FR2968716B1 (en) 2010-12-13 2012-12-28 Turbomeca METHOD FOR CONTROLLING THE ELECTRIC GENERATION APPLIED TO AN AIRCRAFT GAS TURBINE AND TURBOMOTOR IMPLEMENTING SUCH A METHOD
US9994304B2 (en) * 2014-10-01 2018-06-12 Nabtesco Corporation Hydraulic actuator

Also Published As

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

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