FR957061A - - Google Patents
Info
- Publication number
- FR957061A FR957061A FR957061DA FR957061A FR 957061 A FR957061 A FR 957061A FR 957061D A FR957061D A FR 957061DA FR 957061 A FR957061 A FR 957061A
- Authority
- FR
- France
- 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
Links
Classifications
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- 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
- F01D5/30—Fixing blades to rotors; Blade roots ; Blade spacers
- F01D5/3023—Fixing blades to rotors; Blade roots ; Blade spacers of radial insertion type, e.g. in individual recesses
- F01D5/303—Fixing blades to rotors; Blade roots ; Blade spacers of radial insertion type, e.g. in individual recesses in a circumferential slot
- F01D5/3038—Fixing blades to rotors; Blade roots ; Blade spacers of radial insertion type, e.g. in individual recesses in a circumferential slot the slot having inwardly directed abutment faces on both sides
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- 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
- F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
- F01D11/02—Preventing or minimising internal leakage of working-fluid, e.g. between stages by non-contact sealings, e.g. of labyrinth type
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- 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
- F01D5/30—Fixing blades to rotors; Blade roots ; Blade spacers
- F01D5/3069—Fixing blades to rotors; Blade roots ; Blade spacers between two discs or rings
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- 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
- F02C3/067—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 having counter-rotating rotors
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- 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)
- Structures Of Non-Positive Displacement Pumps (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SE2611532X | 1944-09-23 |
Publications (1)
Publication Number | Publication Date |
---|---|
FR957061A true FR957061A (en) | 1950-02-14 |
Family
ID=20426543
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR957061D Expired FR957061A (en) | 1944-09-23 |
Country Status (2)
Country | Link |
---|---|
US (1) | US2611532A (en) |
FR (1) | FR957061A (en) |
Families Citing this family (23)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2700935A (en) * | 1948-04-27 | 1955-02-01 | Bendix Aviat Corp | Rocket fuel pump and the like |
US2922278A (en) * | 1948-11-30 | 1960-01-26 | Szydlowski Joseph | Coaxial combustion products generator and turbine |
US2788951A (en) * | 1951-02-15 | 1957-04-16 | Power Jets Res & Dev Ltd | Cooling of turbine rotors |
GB742241A (en) * | 1951-02-15 | 1955-12-21 | Power Jets Res & Dev Ltd | Improvements in the cooling of turbines |
USRE24810E (en) * | 1952-04-30 | 1960-04-19 | Alfred Buchi | Turbine driven multi-stage blower or pump |
US2839005A (en) * | 1953-10-14 | 1958-06-17 | Herbert E Means | Turbine driven pump |
US2929207A (en) * | 1955-08-08 | 1960-03-22 | Adolphe C Peterson | Axial flow gas turbine |
US2931563A (en) * | 1955-09-19 | 1960-04-05 | Eggleton Frederick | Construction of axial flow compressors |
US3023577A (en) * | 1955-10-24 | 1962-03-06 | Williams Res Corp | Gas turbine with heat exchanger |
US2937495A (en) * | 1956-02-27 | 1960-05-24 | Power Jets Res & Dev Ltd | Gas turbine plant |
US2922618A (en) * | 1956-03-06 | 1960-01-26 | Gen Electric | Turbo-machine rotor |
US2990108A (en) * | 1957-03-04 | 1961-06-27 | Curtiss Wright Corp | Compressor with annular discharge diffuser |
US2927724A (en) * | 1957-10-02 | 1960-03-08 | Avro Aircraft Ltd | Floating blade shrouds |
US3037352A (en) * | 1958-09-08 | 1962-06-05 | Vladimir H Pavlecka | Bypass jet engines using centripetal flow compressors and centrifugal flow turbines |
US3259195A (en) * | 1962-04-23 | 1966-07-05 | Paul W Chaney | Aircraft with non-combustion, air reaction engine |
US3194011A (en) * | 1962-04-23 | 1965-07-13 | Paul W Chaney | Aircraft with non-combustion air reaction engine |
US3157991A (en) * | 1963-04-16 | 1964-11-24 | Kemenczky Establishment | Flow regulating device for jet propulsion engine |
US3302866A (en) * | 1965-03-16 | 1967-02-07 | Polytechnic Inst Brooklyn | High velocity fluid accelerator |
GB1417587A (en) * | 1972-12-08 | 1975-12-10 | Rolls Royce | Bearings |
FR2506839B1 (en) * | 1981-05-27 | 1986-07-04 | Onera (Off Nat Aerospatiale) | SIMPLIFIED CONTRA-ROTARY TURBOREACTOR |
DE59710621D1 (en) * | 1997-09-19 | 2003-09-25 | Alstom Switzerland Ltd | Gap sealing device |
DE10338395A1 (en) * | 2003-08-21 | 2005-03-17 | Anton Niederbrunner | Impeller assembly of a turbomachine |
CN113153537B (en) * | 2021-03-19 | 2022-05-17 | 哈尔滨工业大学 | Three-wheel cooling-refrigeration cycle cooling system applied to hypersonic aircraft |
Family Cites Families (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
USRE23198E (en) * | 1950-02-21 | Reaction propelling device for | ||
GB190500372A (en) * | 1905-01-07 | 1906-04-07 | Henrik Van Meerten | Improvements in or pertaining to Turbines. |
AT51150B (en) * | 1909-09-13 | 1911-12-11 | Willibald Gelinek | Compressor combined with a steam, gas or similar turbine. |
FR411472A (en) * | 1910-01-11 | 1910-06-17 | Emile Baptiste Merigoux | Turbine capable of operating with detonating mixtures, steam and other gaseous fluids |
US2080425A (en) * | 1933-02-10 | 1937-05-18 | Milo Ab | Turbine |
US2297508A (en) * | 1940-02-29 | 1942-09-29 | Schutte Alfred | Rotor for turbines |
FR879123A (en) * | 1941-01-10 | 1943-02-15 | Improvements to thermo-propellant nozzles and to aircraft and other vehicles powered by these nozzles | |
US2405164A (en) * | 1941-03-25 | 1946-08-06 | Northrop Aircraft Inc | Turbine stator |
GB585334A (en) * | 1941-05-14 | 1947-02-05 | Alan Arnold Griffith | Improvements in or relating to internal-combustion turbines |
US2414551A (en) * | 1941-07-21 | 1947-01-21 | Northrop Aircraft Inc | Compressor |
US2411124A (en) * | 1941-11-01 | 1946-11-12 | Vickers Electrical Co Ltd | Internal-combustion turbine plant |
US2401826A (en) * | 1941-11-21 | 1946-06-11 | Dehavilland Aircraft | Turbine |
US2430398A (en) * | 1942-09-03 | 1947-11-04 | Armstrong Siddeley Motors Ltd | Jet-propulsion internal-combustion turbine plant |
US2435990A (en) * | 1945-08-17 | 1948-02-17 | Westinghouse Electric Corp | Gas turbine lubricating oil cooling and air inlet deicing system |
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0
- FR FR957061D patent/FR957061A/fr not_active Expired
-
1945
- 1945-09-22 US US618042A patent/US2611532A/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
US2611532A (en) | 1952-09-23 |