FR944314A - Perfectionnements aux turbines à gaz ou aux propulseurs à gaz à réaction - Google Patents

Perfectionnements aux turbines à gaz ou aux propulseurs à gaz à réaction

Info

Publication number
FR944314A
FR944314A FR944314DA FR944314A FR 944314 A FR944314 A FR 944314A FR 944314D A FR944314D A FR 944314DA FR 944314 A FR944314 A FR 944314A
Authority
FR
France
Prior art keywords
gas
jet engines
turbines
gas jet
gas turbines
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.)
Expired
Application number
Other languages
English (en)
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.)
Lockheed Martin Corp
Original Assignee
Lockheed Aircraft 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
Priority claimed from US488029A external-priority patent/US2468461A/en
Application filed by Lockheed Aircraft Corp filed Critical Lockheed Aircraft Corp
Application granted granted Critical
Publication of FR944314A publication Critical patent/FR944314A/fr
Expired legal-status Critical Current

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
    • F02K1/36—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto having an ejector
    • 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
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
    • 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
    • F01D5/08—Heating, heat-insulating or cooling means
    • F01D5/085—Heating, heat-insulating or cooling means cooling fluid circulating inside the rotor
    • 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
    • F01D9/00—Stators
    • F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
    • F01D9/042—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector fixing blades to stators
    • 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
    • F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/04—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
    • F02C3/06—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor the compressor comprising only axial stages
    • 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
    • F02K1/06—Varying effective area of jet pipe or nozzle
    • F02K1/08—Varying effective area of jet pipe or nozzle by axially moving or transversely deforming an internal member, e.g. the exhaust cone
    • 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
    • F02K1/06—Varying effective area of jet pipe or nozzle
    • F02K1/09—Varying effective area of jet pipe or nozzle by axially moving an external member, e.g. a shroud
    • 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)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Jet Pumps And Other Pumps (AREA)
FR944314D 1943-05-22 1947-01-10 Perfectionnements aux turbines à gaz ou aux propulseurs à gaz à réaction Expired FR944314A (fr)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US488029A US2468461A (en) 1943-05-22 1943-05-22 Nozzle ring construction for turbopower plants
US580241A US2510606A (en) 1943-05-22 1945-02-28 Turbine construction
US581994A US2487588A (en) 1943-05-22 1945-03-10 Variable area propulsive nozzle means for power plants

Publications (1)

Publication Number Publication Date
FR944314A true FR944314A (fr) 1949-04-01

Family

ID=27413784

Family Applications (1)

Application Number Title Priority Date Filing Date
FR944314D Expired FR944314A (fr) 1943-05-22 1947-01-10 Perfectionnements aux turbines à gaz ou aux propulseurs à gaz à réaction

Country Status (3)

Country Link
US (2) US2510606A (fr)
FR (1) FR944314A (fr)
GB (2) GB618493A (fr)

Families Citing this family (63)

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US2653445A (en) * 1945-05-11 1953-09-29 Dehavilland Aircraft Turbocompressor jet-propulsion apparatus and adjustable nozzle therefor
NL70849C (fr) * 1945-05-14
US2597253A (en) * 1945-11-13 1952-05-20 Effie B Melchior Jet-propulsion nozzle
US2635849A (en) * 1946-08-13 1953-04-21 Buchi Alfred Turbine stage
US2692480A (en) * 1948-05-07 1954-10-26 Onera (Off Nat Aerospatiale) Supersonic internal circulation combustion chamber, in particular combustion chamber for aircraft jet engines
US2653446A (en) * 1948-06-05 1953-09-29 Lockheed Aircraft Corp Compressor and fuel control system for high-pressure gas turbine power plants
US2680948A (en) * 1948-08-30 1954-06-15 Engineering & Res Corp Variable area tail pipe for jet engines
US2635419A (en) * 1948-09-30 1953-04-21 Curtiss Wright Corp Adjustable discharge nozzle for jet engines
US2789417A (en) * 1949-03-22 1957-04-23 Bendix Aviat Corp Tailpipe or afterburning control for turbojet engines
US2654215A (en) * 1949-09-27 1953-10-06 United Aircraft Corp Turbine power plant having auxiliary air inlet and thrust augmenter
US2648192A (en) * 1949-09-27 1953-08-11 United Aircraft Corp Variable capacity jet exhaust augmenter
US2793493A (en) * 1950-04-28 1957-05-28 Snecma Devices for deflecting fluid jets
US2659202A (en) * 1950-06-06 1953-11-17 Fay E Null Augmented thrust pulse jet pump or motor and method of creating augmented thrust or suction
GB750622A (en) * 1950-06-16 1956-06-20 Snecma Improvements in or relating to jet propulsion units for aircraft
US2724238A (en) * 1950-10-25 1955-11-22 Tresham D Gregg Jet propulsive devices
US2793491A (en) * 1950-12-07 1957-05-28 Gen Motors Corp Variable area jet nozzle
FR1030483A (fr) * 1951-01-04 1953-06-15 Snecma Procédé et dispositifs de réglage d'un écoulement et leurs diverses applications
US2658332A (en) * 1951-03-21 1953-11-10 Carborundum Co Fluid cooled, refractory, ceramic lined rocket structure
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US2834534A (en) * 1951-09-27 1958-05-13 Snecma Centrifugal air compressor control device
DE976186C (de) * 1952-01-01 1963-04-18 Snecma Turbomaschine, insbesondere Gasturbine
US2671313A (en) * 1952-03-07 1954-03-09 Emile A Laramee Jet engine vacuum expansion nozzle
US2709337A (en) * 1952-03-28 1955-05-31 United Aircraft Corp Boundary layer control for the diffuser of a gas turbine
US3024602A (en) * 1952-04-22 1962-03-13 Snecma Arrangements for deflecting the jet expelled from a discharge nozzle or from a reaction-propulsion unit
DE1043723B (de) * 1952-05-21 1958-11-13 Snecma Verfahren und Vorrichtung zum Beeinflussen des Querschnittes und/oder der Richtung des durch das Strahlrohr eines Rueckstossantriebes hindurchgehenden Gasstromkernes
DE1164754B (de) * 1952-08-15 1964-03-05 United Aircraft Corp Schubduese fuer ein Flugzeugstrahltriebwerk
US2801518A (en) * 1952-09-17 1957-08-06 Solar Aircraft Co Gas turbine
US3041823A (en) * 1952-09-18 1962-07-03 Snecma Control for varying the cross-sectional area of a nozzle
US2811829A (en) * 1952-12-04 1957-11-05 Alfred A Topinka Ram jet employing carbon layer of insulation for solid carbon propellant
US2866314A (en) * 1953-01-02 1958-12-30 United Aircraft Corp Flame holding device movable between a flameholding position and a streamlined position
US2892583A (en) * 1953-01-19 1959-06-30 Stalker Corp Axial flow compressors
DE1083600B (de) * 1954-02-11 1960-06-15 Snecma Vorrichtung zum Regeln des wirksamen Querschnittes der Duese eines Rueckstossantriebes
US2873909A (en) * 1954-10-26 1959-02-17 Svenska Rotor Maskiner Ab Rotary devices and casing structures therefor
NL103792C (fr) * 1954-12-16
US2843357A (en) * 1955-05-06 1958-07-15 Westinghouse Electric Corp Rotary fluid handling apparatus
GB799896A (en) * 1955-10-21 1958-08-13 Rolls Royce Improvements in or relating to axial-flow compressors
US2914300A (en) * 1955-12-22 1959-11-24 Gen Electric Nozzle vane support for turbines
US3109284A (en) * 1956-06-14 1963-11-05 Power Jets Res & Dev Ltd Discharge nozzles for propulsive jets
GB820059A (en) * 1956-07-30 1959-09-16 Bristol Aero Engines Ltd Improvements in or relating to jet propulsion nozzles
US3000552A (en) * 1957-05-28 1961-09-19 Gen Motors Corp Compressor vane mounting
US3049873A (en) * 1958-02-04 1962-08-21 Westinghouse Electric Corp Exhaust nozzle having a flow area of variable convergency and divergency
US3004700A (en) * 1959-08-18 1961-10-17 Gen Electric Turbine engine casing
US3165888A (en) * 1959-09-18 1965-01-19 Edward F Keon Exhaust nozzle for reaction engines and the like
US3021110A (en) * 1960-03-01 1962-02-13 Gen Electric High temperature turbine nozzle retaining means
US3224194A (en) * 1963-06-26 1965-12-21 Curtiss Wright Corp Gas turbine engine
US3262677A (en) * 1963-11-27 1966-07-26 Gen Electric Stator assembly
US3339833A (en) * 1963-12-04 1967-09-05 Rolls Royce Axial fluid flow machine such as a compressor or turbine
US3302926A (en) * 1965-12-06 1967-02-07 Gen Electric Segmented nozzle diaphragm for high temperature turbine
US3906719A (en) * 1968-08-19 1975-09-23 Aerojet General Co Rocket having movable secondary nozzle
US3575260A (en) * 1969-05-15 1971-04-20 Rohr Corp Method and apparatus for augmenting the thrust of a jet-propelled aircraft and suppressing the noise thereof
US3637042A (en) * 1970-07-27 1972-01-25 Rohr Corp Method and apparatus for suppressing the noise of jet-propelled aircraft
US3581841A (en) * 1970-07-27 1971-06-01 Rohr Corp Thrust reversing and noise suppressing apparatus for a jet engine
US3711013A (en) * 1971-04-26 1973-01-16 Rohr Corp Thrust control and sound apparatus
US3739984A (en) * 1971-08-25 1973-06-19 Rohr Industries Inc Thrust augmenting and south suppressing apparatus and method
US3705688A (en) * 1971-09-07 1972-12-12 Gen Motors Corp Oval jet nozzle
US3921906A (en) * 1974-12-02 1975-11-25 Gen Electric Infrared suppression system for a gas turbine engine
US4214703A (en) * 1979-03-23 1980-07-29 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Aircraft engine nozzle
US5224824A (en) * 1990-09-12 1993-07-06 United Technologies Corporation Compressor case construction
US20060150612A1 (en) * 2005-01-12 2006-07-13 Honeywell International Inc. Thrust vector control
CN101939528B (zh) * 2007-08-08 2013-07-24 罗尔股份有限公司 具有旁通流的面积可调风扇喷嘴
FR2991375A1 (fr) * 2012-06-04 2013-12-06 Alstom Technology Ltd Ecran de protection thermique pour une conduite d'arrivee de vapeur dans une turbine basse pression
US10850822B1 (en) 2019-06-27 2020-12-01 Brunswick Corporation Splined and threaded shaft for marine drive

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US607548A (en) * 1898-07-19 Johann georg pinkert
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DE483888C (de) * 1929-10-07 Duell R Diffusor fuer Strahlapparate
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US658586A (en) * 1899-08-17 1900-09-25 Meinhard Reiling Fire-hose.
US779910A (en) * 1902-08-01 1905-01-10 Charles G Curtis Elastic-fluid turbine.
US735054A (en) * 1903-04-22 1903-08-04 Gen Electric Means for adjusting intermediate buckets.
US972421A (en) * 1910-04-18 1910-10-11 George Westinghouse Turbine.
US1154777A (en) * 1914-02-21 1915-09-28 Gen Electric Attaching means for nozzles.
US1555030A (en) * 1914-09-14 1925-09-29 Westinghouse Electric & Mfg Co Fluid-translating device
US1422582A (en) * 1919-12-19 1922-07-11 Procedes Westinghouse Leblanc Steam ejector
US1362437A (en) * 1920-04-14 1920-12-14 Gen Electric Elastic-fluid turbine
US1493157A (en) * 1923-12-10 1924-05-06 Melot Henri Fabrice Propelling ejector
GB243974A (en) * 1925-04-20 1925-12-10 Jan Kieswetter Improvements relating to turbine casings having transverse partitions and the like therein
CH121403A (de) * 1926-06-10 1927-07-01 Escher Wyss Maschf Ag Leitvorrichtung für Dampf- und Gasturbinen, welche zu mindestens einer Gruppe vereinigte, mit radialem Spiel ins Turbinengehäuse eingesetzte Leiträder aufweist.
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US2468461A (en) * 1943-05-22 1949-04-26 Lockheed Aircraft Corp Nozzle ring construction for turbopower plants
US2366142A (en) * 1943-07-14 1944-12-26 Allis Chalmers Mfg Co Blade shrouding

Also Published As

Publication number Publication date
GB618493A (en) 1949-02-22
GB616696A (en) 1949-01-26
US2510606A (en) 1950-06-06
US2487588A (en) 1949-11-08

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