AU589180B2 - An improved apparatus - Google Patents

An improved apparatus

Info

Publication number
AU589180B2
AU589180B2 AU57093/86A AU5709386A AU589180B2 AU 589180 B2 AU589180 B2 AU 589180B2 AU 57093/86 A AU57093/86 A AU 57093/86A AU 5709386 A AU5709386 A AU 5709386A AU 589180 B2 AU589180 B2 AU 589180B2
Authority
AU
Australia
Prior art keywords
improved apparatus
improved
Prior art date
Legal status (The legal status 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 status listed.)
Ceased
Application number
AU57093/86A
Other versions
AU5709386A (en
Inventor
Kenneth Odell Johnson
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
General Electric Co
Original Assignee
General Electric Co
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 General Electric Co filed Critical General Electric Co
Publication of AU5709386A publication Critical patent/AU5709386A/en
Application granted granted Critical
Publication of AU589180B2 publication Critical patent/AU589180B2/en
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
    • B64C11/46—Arrangements of, or constructional features peculiar to, multiple propellers
    • B64C11/48—Units of two or more coaxial propellers
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
    • B64C11/30—Blade pitch-changing mechanisms
    • B64C11/306—Blade pitch-changing mechanisms specially adapted for contrarotating propellers
    • B64C11/308—Blade pitch-changing mechanisms specially adapted for contrarotating propellers automatic
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
    • F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
    • F02K3/072—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type with counter-rotating, e.g. fan rotors
    • 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
    • B64D27/00—Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby
    • B64D2027/005—Aircraft with an unducted turbofan comprising contra-rotating rotors, e.g. contra-rotating open rotors [CROR]
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
AU57093/86A 1985-05-01 1986-05-01 An improved apparatus Ceased AU589180B2 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US72846685A 1985-05-01 1985-05-01
US728466 1985-05-01

Publications (2)

Publication Number Publication Date
AU5709386A AU5709386A (en) 1986-11-06
AU589180B2 true AU589180B2 (en) 1989-10-05

Family

ID=24926972

Family Applications (1)

Application Number Title Priority Date Filing Date
AU57093/86A Ceased AU589180B2 (en) 1985-05-01 1986-05-01 An improved apparatus

Country Status (9)

Country Link
JP (1) JPH0681883B2 (en)
AU (1) AU589180B2 (en)
CA (1) CA1262409A (en)
DE (1) DE3614157C2 (en)
FR (1) FR2581423B1 (en)
GB (1) GB2174762B (en)
IT (1) IT1208606B (en)
NL (1) NL8601055A (en)
SE (1) SE462660B (en)

Families Citing this family (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3734624A1 (en) * 1987-10-13 1989-05-03 Kastens Karl Propeller fan
DE3812027A1 (en) * 1988-04-11 1989-10-26 Mtu Muenchen Gmbh PROPFAN TURBO ENGINE
US4916892A (en) * 1988-05-06 1990-04-17 General Electric Company High pressure seal
US4976102A (en) * 1988-05-09 1990-12-11 General Electric Company Unducted, counterrotating gearless front fan engine
GB2218747B (en) * 1988-05-20 1993-01-27 Gen Electric Propeller/fan pitch feathering apparatus
DE3818466C1 (en) * 1988-05-31 1989-12-21 Mtu Muenchen Gmbh
DE3837994A1 (en) * 1988-11-09 1990-05-10 Mtu Muenchen Gmbh DEVICE FOR ADJUSTING THE ROTOR BLADES OF A PROPFAN / TURBO PROPOWER PLANT
US5263898A (en) * 1988-12-14 1993-11-23 General Electric Company Propeller blade retention system
US4951461A (en) * 1989-03-20 1990-08-28 General Electric Company Power turbine support arrangement
US5112191A (en) * 1989-04-11 1992-05-12 General Electric Company Rotating cowling
US5082424A (en) * 1989-06-05 1992-01-21 General Electric Company Connection system for aircraft propeller blades
DE3933776A1 (en) * 1989-10-10 1991-04-18 Mtu Muenchen Gmbh Prop-fan aircraft engine with contra-rotating fan rotors - has epicyclic gear train to connect turbines to fan rotors
FR2761412B1 (en) * 1997-03-27 1999-04-30 Snecma DOUBLE-BODY TURBOPROPULSOR GROUP WITH ISODROME REGULATION
US6711887B2 (en) * 2002-08-19 2004-03-30 General Electric Co. Aircraft gas turbine engine with tandem non-interdigitated counter rotating low pressure turbines
FR2864997B1 (en) * 2004-01-08 2006-04-28 Snecma Moteurs SEMI-LIEURED TURBINE TURBINE ENGINE HANDLING A PILOT RECEIVER TO KEEP A SUBSTANTIALLY CONSTANT ROTATION SPEED
DE102008005163B4 (en) 2008-01-19 2009-12-03 Deutsches Zentrum für Luft- und Raumfahrt e.V. Aircraft engine
FR2941493B1 (en) * 2009-01-23 2011-08-26 Snecma FREE TURBINE TURBINE ENGINE THAT ENABLES AN ELECTRIC POWER GENERATOR
US8182222B2 (en) 2009-02-12 2012-05-22 Hamilton Sundstrand Corporation Thermal protection of rotor blades
GB201102987D0 (en) * 2011-02-22 2011-04-06 Rolls Royce Plc A propfan engine
RU2482311C1 (en) * 2011-12-14 2013-05-20 Открытое акционерное общество "Авиадвигатель" Gas turbine engine with aft location of open propeller fan
FR3004494B1 (en) * 2013-04-15 2018-01-19 Safran Nacelles TUYERE FOR AIRCRAFT TURBOPROPULSER WITH NON-CARBONATED BLOWER
FR3016662B1 (en) * 2014-01-23 2016-02-12 Snecma NON-CARNETIC PROPELLER TURBOMOTEUR HAVING A REINFORCING ENVELOPE INCORPORATING PIPES OF PIPES
FR3050431B1 (en) * 2016-04-20 2018-04-27 Safran Aircraft Engines SIMPLIFIED STEP ACTUATION SYSTEM FOR A TURBOMACHINE PROPELLER

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2129502A (en) * 1982-11-01 1984-05-16 Gen Electric Counter rotation power turbine

Family Cites Families (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB238343A (en) * 1924-07-03 1925-08-20 English Electric Co Ltd Improvements in the construction of elastic fluid turbines
FR776676A (en) * 1933-10-23 1935-01-31 Helical turbine
FR910103A (en) * 1942-01-02 1946-05-28 Rateau Soc Gas turbine engine combined with a fan or propellant
BE462340A (en) * 1944-04-15
GB1004641A (en) * 1963-05-16 1965-09-15 Vickers Armstrong Aircraft Ltd Improvements in jet-propulsion power-plants for aircraft
GB978041A (en) * 1963-08-21 1964-12-16 Rolls Royce Aerofoil-section member having relatively movable parts
DE1426835A1 (en) * 1964-06-27 1969-04-03 Maschf Augsburg Nuernberg Ag Process and arrangement for generating energy or for power consumption in counter-rotating turbines or machines
GB1097632A (en) * 1965-11-19 1968-01-03 Bristol Siddeley Engines Ltd Gas turbine power plant
FR1483743A (en) * 1965-12-02 1967-06-09 Snecma Turbomachine with contra-rotating compressor
GB1212593A (en) * 1968-01-25 1970-11-18 British Aircraft Corp Ltd Improvements relating to rotary large diameter gas seals
GB1203712A (en) * 1968-02-07 1970-09-03 Rolls Royce Improvements in or relating to gas turbine engine
SU411214A1 (en) * 1968-05-12 1974-01-15
US3861139A (en) * 1973-02-12 1975-01-21 Gen Electric Turbofan engine having counterrotating compressor and turbine elements and unique fan disposition
US4446696A (en) * 1981-06-29 1984-05-08 General Electric Company Compound propulsor
US4519746A (en) * 1981-07-24 1985-05-28 United Technologies Corporation Airfoil blade
GB2138507B (en) * 1983-04-22 1987-07-29 Rolls Royce Mounting and exhausting in turbo-propellor aircraft engines
DE3507035A1 (en) * 1984-03-02 1985-09-12 General Electric Co., Schenectady, N.Y. GAS TURBINE ENGINE

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2129502A (en) * 1982-11-01 1984-05-16 Gen Electric Counter rotation power turbine

Also Published As

Publication number Publication date
FR2581423B1 (en) 1993-10-22
AU5709386A (en) 1986-11-06
GB2174762B (en) 1990-04-04
JPH0681883B2 (en) 1994-10-19
CA1262409A (en) 1989-10-24
IT8620279A0 (en) 1986-04-30
SE8601928D0 (en) 1986-04-25
DE3614157C2 (en) 1997-06-26
GB8610566D0 (en) 1986-06-04
DE3614157A1 (en) 1986-11-06
JPS6217301A (en) 1987-01-26
SE8601928L (en) 1986-11-02
FR2581423A1 (en) 1986-11-07
GB2174762A (en) 1986-11-12
IT1208606B (en) 1989-07-10
SE462660B (en) 1990-08-06
NL8601055A (en) 1986-12-01

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