IT1190334B - Struttura trasmettitrice di potenza per turbomotori a gas - Google Patents

Struttura trasmettitrice di potenza per turbomotori a gas

Info

Publication number
IT1190334B
IT1190334B IT20223/86A IT2022386A IT1190334B IT 1190334 B IT1190334 B IT 1190334B IT 20223/86 A IT20223/86 A IT 20223/86A IT 2022386 A IT2022386 A IT 2022386A IT 1190334 B IT1190334 B IT 1190334B
Authority
IT
Italy
Prior art keywords
power transmitter
transmitter structure
gas turbo
turbo engines
engines
Prior art date
Application number
IT20223/86A
Other languages
English (en)
Other versions
IT8620223A1 (it
IT8620223A0 (it
Inventor
William James Strock
Ambrose Andreas Hauser
Original Assignee
Gen Electric
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 Gen Electric filed Critical Gen Electric
Publication of IT8620223A0 publication Critical patent/IT8620223A0/it
Publication of IT8620223A1 publication Critical patent/IT8620223A1/it
Application granted granted Critical
Publication of IT1190334B publication Critical patent/IT1190334B/it

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12—Blades
    • F01D5/14—Form or construction
    • F01D5/18—Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/02—Blade-carrying members, e.g. rotors
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D7/00—Rotors with blades adjustable in operation; Control thereof
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D9/00—Stators
    • F01D9/06—Fluid supply conduits to nozzles or the like
    • F01D9/065—Fluid supply or removal conduits traversing the working fluid flow, e.g. for lubrication-, cooling-, or sealing fluids
    • 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
    • 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
    • F05D2260/70—Adjusting of angle of incidence or attack of rotating blades
    • F05D2260/74—Adjusting of angle of incidence or attack of rotating blades by turning around an axis perpendicular the rotor centre line
    • 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
    • F05D2260/70—Adjusting of angle of incidence or attack of rotating blades
    • F05D2260/76—Adjusting of angle of incidence or attack of rotating blades the adjusting mechanism using auxiliary power sources
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
IT20223/86A 1985-05-31 1986-04-24 Struttura trasmettitrice di potenza per turbomotori a gas IT1190334B (it)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US06/739,804 US4758129A (en) 1985-05-31 1985-05-31 Power frame

Publications (3)

Publication Number Publication Date
IT8620223A0 IT8620223A0 (it) 1986-04-24
IT8620223A1 IT8620223A1 (it) 1987-10-24
IT1190334B true IT1190334B (it) 1988-02-16

Family

ID=24973839

Family Applications (1)

Application Number Title Priority Date Filing Date
IT20223/86A IT1190334B (it) 1985-05-31 1986-04-24 Struttura trasmettitrice di potenza per turbomotori a gas

Country Status (7)

Country Link
US (1) US4758129A (it)
JP (1) JPS61283704A (it)
CA (1) CA1260401A (it)
DE (1) DE3612595A1 (it)
FR (1) FR2582719B1 (it)
GB (1) GB2176246B (it)
IT (1) IT1190334B (it)

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5108259A (en) * 1988-12-19 1992-04-28 General Electric Company Flexible connector for use in aircraft
US4951461A (en) * 1989-03-20 1990-08-28 General Electric Company Power turbine support arrangement
US5082424A (en) * 1989-06-05 1992-01-21 General Electric Company Connection system for aircraft propeller blades
US5307622A (en) * 1993-08-02 1994-05-03 General Electric Company Counterrotating turbine support assembly
US5388964A (en) * 1993-09-14 1995-02-14 General Electric Company Hybrid rotor blade
US6732502B2 (en) 2002-03-01 2004-05-11 General Electric Company Counter rotating aircraft gas turbine engine with high overall pressure ratio compressor
US6619030B1 (en) 2002-03-01 2003-09-16 General Electric Company Aircraft engine with inter-turbine engine frame supported counter rotating low pressure turbine rotors
US7094027B2 (en) * 2002-11-27 2006-08-22 General Electric Company Row of long and short chord length and high and low temperature capability turbine airfoils
US7063505B2 (en) 2003-02-07 2006-06-20 General Electric Company Gas turbine engine frame having struts connected to rings with morse pins
FR2911644B1 (fr) 2007-01-23 2012-06-01 Snecma Turbopropulseur comportant une helice formee de pales a orientation reglable.
DE102009007013A1 (de) * 2009-01-31 2010-08-12 Deutsches Zentrum für Luft- und Raumfahrt e.V. Triebwerk, insbesondere CROR-Antrieb, für ein Flugzeug
FR2946010B1 (fr) * 2009-05-29 2011-06-24 Snecma Dispositif a verin fixe pour la commande des pales de soufflante d'un turbopropulseur
US20200017229A1 (en) * 2018-07-13 2020-01-16 Bell Helicopter Textron Inc. Fan clutch for convertible engine
US12466544B1 (en) * 2024-05-10 2025-11-11 Rtx Corporation SRV open rotor with core inlet forward of rotor

Family Cites Families (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB814380A (en) * 1954-11-10 1959-06-03 Power Jets Res & Dev Ltd Power plant incorporating a dynamic compressor
US2314572A (en) * 1938-12-07 1943-03-23 Herman E Chitz Turboengine
US2941781A (en) * 1955-10-13 1960-06-21 Westinghouse Electric Corp Guide vane array for turbines
US3075743A (en) * 1958-10-20 1963-01-29 Gen Dynamics Corp Turbo-machine with slotted blades
GB920887A (en) * 1958-11-24 1963-03-13 Rolls Royce Improvements in or relating to gas-turbine engines
GB1190365A (en) * 1966-05-25 1970-05-06 Dowty Rotol Ltd Gas Turbine Engines
US3468473A (en) * 1966-05-25 1969-09-23 Dowty Rotol Ltd Gas turbine engines
GB1196589A (en) * 1966-11-21 1970-07-01 British Aircraft Corp Ltd Form Improvements relating to Turbo-fan Aircraft Engines
US3467198A (en) * 1966-12-05 1969-09-16 Rolls Royce Gear transmission
FR1553936A (it) * 1966-12-05 1969-01-17
FR1520600A (fr) * 1967-02-27 1968-04-12 Snecma Perfectionnements aux turbo-machines à flux axial, et en particulier aux compresseurs axiaux à deux rotors imbriqués contrarotatifs
GB1265150A (it) * 1968-06-22 1972-03-01
US3703081A (en) * 1970-11-20 1972-11-21 Gen Electric Gas turbine engine
DE2218874C3 (de) * 1972-04-19 1979-05-17 Motoren- Und Turbinen-Union Muenchen Gmbh, 8000 Muenchen Vorrichtung zur Verstellung der Gebläseschaufeln eines Turbinenstrahltriebwerks
US3861139A (en) * 1973-02-12 1975-01-21 Gen Electric Turbofan engine having counterrotating compressor and turbine elements and unique fan disposition
US4264274A (en) * 1977-12-27 1981-04-28 United Technologies Corporation Apparatus maintaining rotor and stator clearance
US4304522A (en) * 1980-01-15 1981-12-08 Pratt & Whitney Aircraft Of Canada Limited Turbine bearing support
US4452566A (en) * 1981-06-15 1984-06-05 Institute Of Gas Technology Reactive impeller for pressurizing hot flue gases
US4478551A (en) * 1981-12-08 1984-10-23 United Technologies Corporation Turbine exhaust case design
GB2115881A (en) * 1982-02-26 1983-09-14 Rolls Royce Gas turbine engine stator vane assembly
NL8303401A (nl) * 1982-11-01 1984-06-01 Gen Electric Aandrijfturbine voor tegengesteld draaiende propellers.
US4483659A (en) * 1983-09-29 1984-11-20 Armstrong Richard J Axial flow impeller
US4621978A (en) * 1984-12-03 1986-11-11 General Electric Company Counterrotating power turbine

Also Published As

Publication number Publication date
IT8620223A1 (it) 1987-10-24
GB8608327D0 (en) 1986-05-08
GB2176246A (en) 1986-12-17
DE3612595A1 (de) 1986-12-04
CA1260401A (en) 1989-09-26
GB2176246B (en) 1989-10-25
IT8620223A0 (it) 1986-04-24
JPS61283704A (ja) 1986-12-13
US4758129A (en) 1988-07-19
FR2582719B1 (fr) 1993-12-24
FR2582719A1 (fr) 1986-12-05

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Legal Events

Date Code Title Description
TA Fee payment date (situation as of event date), data collected since 19931001

Effective date: 19950426