IT8020481A0 - Supporto per gruppo motopropulsore a turbina a gas. - Google Patents

Supporto per gruppo motopropulsore a turbina a gas.

Info

Publication number
IT8020481A0
IT8020481A0 IT8020481A IT2048180A IT8020481A0 IT 8020481 A0 IT8020481 A0 IT 8020481A0 IT 8020481 A IT8020481 A IT 8020481A IT 2048180 A IT2048180 A IT 2048180A IT 8020481 A0 IT8020481 A0 IT 8020481A0
Authority
IT
Italy
Prior art keywords
gas turbine
turbine drivetrain
support
drivetrain support
gas
Prior art date
Application number
IT8020481A
Other languages
English (en)
Other versions
IT1130018B (it
Inventor
Nightingale Douglas John
Original Assignee
Rolls Royce
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 Rolls Royce filed Critical Rolls Royce
Publication of IT8020481A0 publication Critical patent/IT8020481A0/it
Application granted granted Critical
Publication of IT1130018B publication Critical patent/IT1130018B/it

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
    • F02K1/56—Reversing jet main flow
    • F02K1/60—Reversing jet main flow by blocking the rearward discharge by means of pivoted eyelids or clamshells, e.g. target-type reversers
    • 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
    • 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
    • B64D27/404—Suspension arrangements specially adapted for supporting vertical loads
    • 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
    • F02C7/20—Mounting or supporting of plant; Accommodating heat expansion or creep
    • 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
    • F02K1/74—Reversing at least one flow in relation to at least one other flow in a plural- flow engine

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Control Of Turbines (AREA)
IT20481/80A 1979-03-10 1980-03-10 Supporto per gruppo motopropulsore a turbina a gas IT1130018B (it)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB7908516A GB2044358B (en) 1979-03-10 1979-03-10 Gas turbine jet engine mounting

Publications (2)

Publication Number Publication Date
IT8020481A0 true IT8020481A0 (it) 1980-03-10
IT1130018B IT1130018B (it) 1986-06-11

Family

ID=10503796

Family Applications (1)

Application Number Title Priority Date Filing Date
IT20481/80A IT1130018B (it) 1979-03-10 1980-03-10 Supporto per gruppo motopropulsore a turbina a gas

Country Status (6)

Country Link
US (1) US4326682A (it)
JP (1) JPS55123318A (it)
DE (1) DE3008690A1 (it)
FR (1) FR2451461A1 (it)
GB (1) GB2044358B (it)
IT (1) IT1130018B (it)

Families Citing this family (76)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4658579A (en) * 1983-07-14 1987-04-21 United Technologies Corporation Load sharing for engine nacelle
US4821980A (en) * 1987-09-29 1989-04-18 The Boeing Company Vibration isolating engine mount
US4922711A (en) * 1988-06-10 1990-05-08 The Boeing Company Thrust reversing system for high bypass fan engines
WO1991005150A1 (en) * 1989-09-29 1991-04-18 Sundstrand Corporation, Inc. Geodesic engine mount structure
US5127606A (en) * 1990-11-16 1992-07-07 Allied-Signal Inc. Aircraft engine mount adapter and method
US5174525A (en) * 1991-09-26 1992-12-29 General Electric Company Structure for eliminating lift load bending in engine core of turbofan
US5275357A (en) * 1992-01-16 1994-01-04 General Electric Company Aircraft engine mount
US5320307A (en) * 1992-03-25 1994-06-14 General Electric Company Aircraft engine thrust mount
US5524847A (en) * 1993-09-07 1996-06-11 United Technologies Corporation Nacelle and mounting arrangement for an aircraft engine
US5452575A (en) * 1993-09-07 1995-09-26 General Electric Company Aircraft gas turbine engine thrust mount
US5443229A (en) * 1993-12-13 1995-08-22 General Electric Company Aircraft gas turbine engine sideways mount
US5467941A (en) * 1993-12-30 1995-11-21 The Boeing Company Pylon and engine installation for ultra-high by-pass turbo-fan engines
WO1996018538A1 (en) * 1994-12-12 1996-06-20 United Technologies Corporation A mounting arrangement for a gas turbine engine
EP0796198B1 (en) * 1994-12-23 1998-08-19 United Technologies Corporation A mounting arrangement for a gas turbine engine
FR2867156B1 (fr) * 2004-03-04 2006-06-02 Airbus France Systeme de montage interpose entre un moteur d'aeronef et une structure rigide d'un mat d'accrochage fixe sous une voilure de cet aeronef.
FR2867157B1 (fr) * 2004-03-04 2006-06-02 Airbus France Systeme de montage interpose entre un moteur d'aeronef et une structure rigide d'un mat d'accrochage fixe sous une voilure de cet aeronef.
FR2869874B1 (fr) * 2004-05-04 2006-06-23 Snecma Moteurs Sa Moteur d'avion avec des moyens de suspension a la structure d'un avion
EP1819907A2 (en) * 2004-12-01 2007-08-22 United Technologies Corporation Fan blade with integral diffuser section and tip turbine blade section for a tip turbine engine
EP1828591B1 (en) * 2004-12-01 2010-07-21 United Technologies Corporation Peripheral combustor for tip turbine engine
WO2006059971A2 (en) * 2004-12-01 2006-06-08 United Technologies Corporation Tip turbine engine integral fan, combustor, and turbine case
WO2006060010A1 (en) * 2004-12-01 2006-06-08 United Technologies Corporation Compressor inlet guide vane for tip turbine engine and corresponding control method
WO2006059970A2 (en) * 2004-12-01 2006-06-08 United Technologies Corporation Turbine engine with differential gear driven fan and compressor
US9003759B2 (en) 2004-12-01 2015-04-14 United Technologies Corporation Particle separator for tip turbine engine
US7878762B2 (en) * 2004-12-01 2011-02-01 United Technologies Corporation Tip turbine engine comprising turbine clusters and radial attachment lock arrangement therefor
WO2006110125A2 (en) * 2004-12-01 2006-10-19 United Technologies Corporation Stacked annular components for turbine engines
WO2006059979A1 (en) * 2004-12-01 2006-06-08 United Technologies Corporation Tip turbine engine integral case, vane, mount, and mixer
US7976272B2 (en) 2004-12-01 2011-07-12 United Technologies Corporation Inflatable bleed valve for a turbine engine
US7883314B2 (en) * 2004-12-01 2011-02-08 United Technologies Corporation Seal assembly for a fan-turbine rotor of a tip turbine engine
EP1825114B1 (en) * 2004-12-01 2008-08-20 United Technologies Corporation Tip turbine engine with a heat exchanger
US8757959B2 (en) * 2004-12-01 2014-06-24 United Technologies Corporation Tip turbine engine comprising a nonrotable compartment
DE602004020125D1 (de) * 2004-12-01 2009-04-30 United Technologies Corp Schmiermittel-versorgungssystem für das getriebe eines tip-turbinen-triebwerks
WO2006059969A1 (en) * 2004-12-01 2006-06-08 United Technologies Corporation Counter-rotating compressor case and assembly method for tip turbine engine
EP1825113B1 (en) * 2004-12-01 2012-10-24 United Technologies Corporation Counter-rotating gearbox for tip turbine engine
EP1825116A2 (en) * 2004-12-01 2007-08-29 United Technologies Corporation Ejector cooling of outer case for tip turbine engine
WO2006060013A1 (en) * 2004-12-01 2006-06-08 United Technologies Corporation Seal assembly for a fan rotor of a tip turbine engine
US7934902B2 (en) * 2004-12-01 2011-05-03 United Technologies Corporation Compressor variable stage remote actuation for turbine engine
US8096753B2 (en) * 2004-12-01 2012-01-17 United Technologies Corporation Tip turbine engine and operating method with reverse core airflow
EP1825112B1 (en) * 2004-12-01 2013-10-23 United Technologies Corporation Cantilevered tip turbine engine
WO2006059996A1 (en) * 2004-12-01 2006-06-08 United Technologies Corporation Balanced turbine rotor fan blade for a tip turbine engine
DE602004029950D1 (de) * 2004-12-01 2010-12-16 United Technologies Corp Enggekoppelte getriebeanordnung für einen spitzenturbinenmotor
US7882695B2 (en) 2004-12-01 2011-02-08 United Technologies Corporation Turbine blow down starter for turbine engine
DE602004027766D1 (de) * 2004-12-01 2010-07-29 United Technologies Corp Hydraulische dichtung für ein getriebe eines spitzenturbinenmotors
WO2006059997A2 (en) 2004-12-01 2006-06-08 United Technologies Corporation Annular turbine ring rotor
EP1828567B1 (en) 2004-12-01 2011-10-12 United Technologies Corporation Diffuser aspiration for a tip turbine engine
WO2006059988A1 (en) * 2004-12-01 2006-06-08 United Technologies Corporation Modular tip turbine engine
US7845157B2 (en) 2004-12-01 2010-12-07 United Technologies Corporation Axial compressor for tip turbine engine
EP1834071B1 (en) * 2004-12-01 2013-03-13 United Technologies Corporation Inducer for a fan blade of a tip turbine engine
EP1828568B1 (en) * 2004-12-01 2011-03-23 United Technologies Corporation Fan-turbine rotor assembly for a tip turbine engine
WO2006060006A1 (en) 2004-12-01 2006-06-08 United Technologies Corporation Tip turbine engine non-metallic tailcone
US7976273B2 (en) * 2004-12-01 2011-07-12 United Technologies Corporation Tip turbine engine support structure
EP1828683B1 (en) 2004-12-01 2013-04-10 United Technologies Corporation Combustor for turbine engine
US7874802B2 (en) * 2004-12-01 2011-01-25 United Technologies Corporation Tip turbine engine comprising turbine blade clusters and method of assembly
US20090169385A1 (en) * 2004-12-01 2009-07-02 Suciu Gabriel L Fan-turbine rotor assembly with integral inducer section for a tip turbine engine
DE602004031679D1 (de) * 2004-12-01 2011-04-14 United Technologies Corp Regenerative Kühlung einer Leit- und Laufschaufel für ein Tipturbinentriebwerk
US7921636B2 (en) * 2004-12-01 2011-04-12 United Technologies Corporation Tip turbine engine and corresponding operating method
EP2333287A1 (en) * 2004-12-01 2011-06-15 United Technologies Corporation Vectoring transition duct for turbine engine
US8641367B2 (en) 2004-12-01 2014-02-04 United Technologies Corporation Plurality of individually controlled inlet guide vanes in a turbofan engine and corresponding controlling method
WO2006060000A1 (en) * 2004-12-01 2006-06-08 United Technologies Corporation Variable fan inlet guide vane assembly, turbine engine with such an assembly and corresponding controlling method
EP1831519B1 (en) * 2004-12-01 2010-08-04 United Technologies Corporation Tip turbine engine with multiple fan and turbine stages
US7874163B2 (en) * 2004-12-01 2011-01-25 United Technologies Corporation Starter generator system for a tip turbine engine
WO2006062497A1 (en) * 2004-12-04 2006-06-15 United Technologies Corporation Tip turbine engine mount
GB2422874A (en) * 2005-02-05 2006-08-09 Alstom Technology Ltd Gas turbine burner expansion bar structure
US8967945B2 (en) 2007-05-22 2015-03-03 United Technologies Corporation Individual inlet guide vane control for tip turbine engine
US8262050B2 (en) * 2008-12-24 2012-09-11 General Electric Company Method and apparatus for mounting and dismounting an aircraft engine
US8469309B2 (en) * 2008-12-24 2013-06-25 General Electric Company Monolithic structure for mounting aircraft engine
US8979491B2 (en) 2009-05-15 2015-03-17 Pratt & Whitney Canada Corp. Turbofan mounting arrangement
US8567202B2 (en) * 2009-05-15 2013-10-29 Pratt & Whitney Canada Corp. Support links with lockable adjustment feature
US8313293B2 (en) * 2009-05-15 2012-11-20 Pratt & Whitney Canada Corp. Turbofan mounting system
US8621874B2 (en) * 2009-08-25 2014-01-07 Honeywell International Inc. Turbomachine core coupling assembly
US9114882B2 (en) * 2010-10-26 2015-08-25 United Technologies Corporation Fan case and mount ring snap fit assembly
DE102010001059A1 (de) * 2010-01-20 2011-07-21 Rolls-Royce Deutschland Ltd & Co KG, 15827 Zwischengehäuse für ein Gasturbinentriebwerk
EP3184433B1 (en) * 2010-06-14 2018-07-25 LORD Corporation A helicopter engine mounting system and methods
US8348191B2 (en) 2010-07-14 2013-01-08 Spirit Aerosystems, Inc. Fail-safe aircraft engine mounting apparatus
US9194296B2 (en) 2012-05-18 2015-11-24 Pratt & Whitney Canada Corp. Inner bypass duct wall attachment
US9212607B2 (en) 2012-07-18 2015-12-15 Spirit Aerosystems, Inc. Intermediate structure for independently de-mountable propulsion components
GB201906164D0 (en) * 2019-05-02 2019-06-19 Rolls Royce Plc Gas turbine engine

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BE466778A (it) * 1945-07-21 1900-01-01
US2539960A (en) * 1946-05-22 1951-01-30 Bristol Aeroplane Co Ltd Mounting structure for gas-turbine power plants for aircraft
US2720370A (en) * 1950-12-04 1955-10-11 Hasbrouck Augustus Resilient engine mounting system, including flexible self-compensating joints
GB777803A (en) * 1953-01-15 1957-06-26 Pye Ltd Improvements in or relating to television receivers
FR1275966A (fr) * 1959-12-18 1961-11-10 Gen Electric Inverseur de poussée
DE1506083A1 (de) * 1965-03-16 1969-10-23 Rolls Royce Triebwerkseinbau in Flugzeugen
US3352114A (en) * 1965-07-17 1967-11-14 Rolls Royce Mounting means for separately supporting a gas turbine engine and a jet pipe in an engine pod
US3601340A (en) * 1969-05-28 1971-08-24 Rohr Corp Method and apparatus for augmenting and reversing thrust and reducing nozzle base drag and noise of an aircraft jet engine
GB1318748A (en) * 1970-08-11 1973-05-31 Secr Defence Gas turgine ducted fan engines for aircraft
US3675418A (en) * 1970-11-19 1972-07-11 United Aircraft Corp Jet engine force frame
DE2241817C3 (de) * 1972-08-25 1975-04-03 Motoren- Und Turbinen-Union Muenchen Gmbh, 8000 Muenchen Schubumkehrvorrichtung für ein mit einer Nachverbrennungsanlage ausgerüstetes Turbinenstrahltriebwerk eines Flugzeugs
GB1504290A (en) * 1975-08-01 1978-03-15 Rolls Royce Gas turbine engine mounting systems
US4044973A (en) * 1975-12-29 1977-08-30 The Boeing Company Nacelle assembly and mounting structures for a turbofan jet propulsion engine
GB2010969A (en) * 1977-12-22 1979-07-04 Rolls Royce Mounting for Gas Turbine Jet Propulsion Engine
US4185798A (en) * 1978-03-13 1980-01-29 Rohr Industries, Inc. Thrust reverser-cascade two door pre-exit

Also Published As

Publication number Publication date
FR2451461B1 (it) 1983-06-17
FR2451461A1 (fr) 1980-10-10
DE3008690A1 (de) 1980-09-11
US4326682A (en) 1982-04-27
GB2044358B (en) 1983-01-19
JPS55123318A (en) 1980-09-22
GB2044358A (en) 1980-10-15
IT1130018B (it) 1986-06-11

Similar Documents

Publication Publication Date Title
IT8020481A0 (it) Supporto per gruppo motopropulsore a turbina a gas.
IT1125821B (it) Supporto per caschi in genere,provvisto di gruppo microtelefono
IT8020479A0 (it) Gruppo motopropulsore a turbina agas.
GB2050592B (en) Gas turbine
JPS5364113A (en) Gas turbine
GB2043868B (en) Gas turbine
IT7919025A0 (it) Impianto a turbina a gas.
IT8025643A0 (it) Accendino a gas.
IT7822594A0 (it) Supporto a snodo.
NL7702207A (nl) Heetgaszuigermachine.
GB2046843B (en) Gas turbine engines-de-icing-icing
JPS55160127A (en) Gas turbine
IT7829660A0 (it) Gruppo motopropulsore a turbina agas.
GB2044431B (en) Gas turbine
IT7926561A0 (it) Procedimento per preparare un copolimero.
IT7928478A0 (it) Intercalati organometallici.
IT7926370A0 (it) Procedimento per preparare un copolimero.
IT8024056A0 (it) Macchina alternativa a gas caldi.
IT8026592A0 (it) Supporto per un mandrino.
IT8021234A0 (it) Bruciatore a gas.
IT8024303A0 (it) Impianto integrato di turbina a gas a combustione di carbone.
AU504726B1 (en) Solar. collector-refrigerant gas generator
IT8019886A0 (it) Accendisigari a gas.
IT8024055A0 (it) Macchina alternativa a gas caldi.
IT7920238A0 (it) Supporto a rotolamento.