IT1182798B - STRUCTURE FOR THE IMPLEMENTATION OF PUSHING INVERTERS IN A MULTI-ENGINE PLANE - Google Patents

STRUCTURE FOR THE IMPLEMENTATION OF PUSHING INVERTERS IN A MULTI-ENGINE PLANE

Info

Publication number
IT1182798B
IT1182798B IT48423/85A IT4842385A IT1182798B IT 1182798 B IT1182798 B IT 1182798B IT 48423/85 A IT48423/85 A IT 48423/85A IT 4842385 A IT4842385 A IT 4842385A IT 1182798 B IT1182798 B IT 1182798B
Authority
IT
Italy
Prior art keywords
inverters
pushing
implementation
engine plane
engine
Prior art date
Application number
IT48423/85A
Other languages
Italian (it)
Other versions
IT8548423A0 (en
Inventor
Steven J Ebbing
Original Assignee
Sundstrand Corp
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 Sundstrand Corp filed Critical Sundstrand Corp
Publication of IT8548423A0 publication Critical patent/IT8548423A0/en
Application granted granted Critical
Publication of IT1182798B publication Critical patent/IT1182798B/en

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/54—Nozzles having means for reversing jet thrust
    • F02K1/76—Control or regulation of thrust reversers
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C25/00—Alighting gear
    • B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface 
    • B64C25/42—Arrangement or adaptation of brakes
    • B64C25/423—Braking devices acting by reaction of gaseous medium
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS 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
    • B64D33/04—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of exhaust outlets or jet pipes
IT48423/85A 1984-08-01 1985-07-30 STRUCTURE FOR THE IMPLEMENTATION OF PUSHING INVERTERS IN A MULTI-ENGINE PLANE IT1182798B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US63670284A 1984-08-01 1984-08-01

Publications (2)

Publication Number Publication Date
IT8548423A0 IT8548423A0 (en) 1985-07-30
IT1182798B true IT1182798B (en) 1987-10-05

Family

ID=24553001

Family Applications (1)

Application Number Title Priority Date Filing Date
IT48423/85A IT1182798B (en) 1984-08-01 1985-07-30 STRUCTURE FOR THE IMPLEMENTATION OF PUSHING INVERTERS IN A MULTI-ENGINE PLANE

Country Status (4)

Country Link
EP (1) EP0190342A1 (en)
JP (1) JPS61502882A (en)
IT (1) IT1182798B (en)
WO (1) WO1986000862A1 (en)

Families Citing this family (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5029091A (en) * 1989-04-11 1991-07-02 United Technologies Corporation Ground mode control of aircraft propeller speed and pitch
LT3149B (en) 1992-10-16 1995-01-31 Fermentas Biotech Inst Hybridoma which produces murine monoclonal antibodies to human angiogenin
FR2760047B1 (en) * 1997-02-27 1999-05-07 Hispano Suiza Sa TURBOJET DRIVE INVERTER WITH DOORS ASSOCIATED WITH A CONTROL SYNCHRONIZATION DEVICE
US6622474B1 (en) * 2001-08-31 2003-09-23 The Boeing Company Synchronization cross-feed system
US6598386B2 (en) 2001-10-16 2003-07-29 Honeywell International, Inc. Jet engine thrust reverser system having torque limited synchronization
US8015797B2 (en) 2006-09-21 2011-09-13 Jean-Pierre Lair Thrust reverser nozzle for a turbofan gas turbine engine
US7946105B2 (en) 2006-11-02 2011-05-24 Honeywell International Inc. Bi-directional locking ring assembly for aircraft thrust reverser manual drive unit
US8051639B2 (en) 2007-11-16 2011-11-08 The Nordam Group, Inc. Thrust reverser
US8172175B2 (en) 2007-11-16 2012-05-08 The Nordam Group, Inc. Pivoting door thrust reverser for a turbofan gas turbine engine
US7735778B2 (en) 2007-11-16 2010-06-15 Pratt & Whitney Canada Corp. Pivoting fairings for a thrust reverser
US8052086B2 (en) 2007-11-16 2011-11-08 The Nordam Group, Inc. Thrust reverser door
US8052085B2 (en) 2007-11-16 2011-11-08 The Nordam Group, Inc. Thrust reverser for a turbofan gas turbine engine
US8127530B2 (en) 2008-06-19 2012-03-06 The Nordam Group, Inc. Thrust reverser for a turbofan gas turbine engine
FR2976625B1 (en) * 2011-06-20 2013-06-07 Aircelle Sa ACTUATOR ASSEMBLY FOR THRUST INVERTER FOR AN AIRCRAFT ENGINE
FR2983173B1 (en) * 2011-11-24 2014-02-28 Aircelle Sa ACTUATOR FOR AN AIRCRAFT AIRCRAFT TURBO AIRBASE WITH REAR PART, PARTICULARLY ANNULAR MONOBLOC
EP2971728B1 (en) * 2013-03-14 2020-09-02 United Technologies Corporation Twin target thrust reverser module
EP3269971A1 (en) * 2016-07-13 2018-01-17 Goodrich Actuation Systems Limited Hydraulically driven thrust reverser
FR3063585B1 (en) * 2017-03-06 2019-04-05 Safran Electronics & Defense ACTUATING DEVICE WITH TWO ACTUATORS

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2629569A (en) * 1947-06-18 1953-02-24 Rolls Royce Control means for aircraft power plant installations
US3662550A (en) * 1971-01-11 1972-05-16 Sundstrand Corp Actuator system
US3941313A (en) * 1972-03-06 1976-03-02 Societe Nationale D'etude Et De Construction De Moteurs D'aviation Jet engine nacelle with drag augmenter auxiliary for thrust-reverser system
US4256277A (en) * 1978-09-12 1981-03-17 Embree David G Actuator system for aircraft control surfaces

Also Published As

Publication number Publication date
EP0190342A1 (en) 1986-08-13
JPS61502882A (en) 1986-12-11
IT8548423A0 (en) 1985-07-30
WO1986000862A1 (en) 1986-02-13

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