FR1056070A - Rotor de compresseur axial - Google Patents
Rotor de compresseur axialInfo
- Publication number
- FR1056070A FR1056070A FR1056070DA FR1056070A FR 1056070 A FR1056070 A FR 1056070A FR 1056070D A FR1056070D A FR 1056070DA FR 1056070 A FR1056070 A FR 1056070A
- Authority
- FR
- France
- Prior art keywords
- compressor rotor
- axial compressor
- axial
- rotor
- compressor
- 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
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/02—Selection of particular materials
- F04D29/023—Selection of particular materials especially adapted for elastic fluid pumps
-
- 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
- F01D5/06—Rotors for more than one axial stage, e.g. of drum or multiple disc type; Details thereof, e.g. shafts, shaft connections
- F01D5/066—Connecting means for joining rotor-discs or rotor-elements together, e.g. by a central bolt, by clamps
-
- 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
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D19/00—Axial-flow pumps
- F04D19/02—Multi-stage pumps
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/26—Rotors specially for elastic fluids
- F04D29/32—Rotors specially for elastic fluids for axial flow pumps
- F04D29/321—Rotors specially for elastic fluids for axial flow pumps for axial flow compressors
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/26—Rotors specially for elastic fluids
- F04D29/32—Rotors specially for elastic fluids for axial flow pumps
- F04D29/321—Rotors specially for elastic fluids for axial flow pumps for axial flow compressors
- F04D29/322—Blade mountings
-
- 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
- F05D2230/00—Manufacture
- F05D2230/70—Disassembly methods
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB316506X | 1950-12-08 |
Publications (1)
Publication Number | Publication Date |
---|---|
FR1056070A true FR1056070A (fr) | 1954-02-24 |
Family
ID=10326335
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1056070D Expired FR1056070A (fr) | 1950-12-08 | 1951-11-15 | Rotor de compresseur axial |
Country Status (6)
Country | Link |
---|---|
US (1) | US2738126A (de) |
BE (1) | BE507205A (de) |
CH (1) | CH316506A (de) |
DE (1) | DE967778C (de) |
FR (1) | FR1056070A (de) |
GB (1) | GB695221A (de) |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2804323A (en) * | 1954-08-19 | 1957-08-27 | Rolls Royce | Axial-flow compressors and turbines |
US2884186A (en) * | 1954-04-23 | 1959-04-28 | Stalker Corp | Rotor construction for axial flow compressors |
DE1062881B (de) * | 1956-08-24 | 1959-08-06 | Krantz H Fa | Axialventilator mit bei Stillstand im Nabenkranz auf verschiedene Anstellwinkel einstellbaren Laufschaufeln |
FR2607866A1 (fr) * | 1986-12-03 | 1988-06-10 | Snecma | Axes de fixation de rotors de turbomachine, procede de montage et rotors ainsi montes |
US5378110A (en) * | 1992-09-14 | 1995-01-03 | United Technologies Corporation | Composite compressor rotor with removable airfoils |
DE19627386A1 (de) * | 1995-07-13 | 1997-01-16 | Bmw Rolls Royce Gmbh | Verbindungs-Anordnung für zwei Turbinen-Laufradscheiben |
Families Citing this family (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB741550A (en) * | 1952-07-10 | 1955-12-07 | Havilland Engine Co Ltd | Improvements in or relating to the rotors of multi-stage axial flow compressors or turbines |
DE1095453B (de) * | 1955-07-18 | 1960-12-22 | Rolls Royce | Mehrstufige Axialstroemungsmaschine |
DE1067971B (de) * | 1955-10-18 | 1959-10-29 | ||
DE1080255B (de) * | 1957-01-17 | 1960-04-21 | Andreas Harold Andersen | Axialventilator |
FR1245518A (fr) * | 1957-04-19 | 1960-11-10 | Perfectionnements apportés aux turbines à fluide gazeux chaud | |
US3345035A (en) * | 1965-04-30 | 1967-10-03 | Gen Motors Corp | Turbine wheel |
US4688992A (en) * | 1985-01-25 | 1987-08-25 | General Electric Company | Blade platform |
EP1319805A1 (de) * | 2001-12-17 | 2003-06-18 | Techspace aero | Rotor oder Rototelement für Turbokompressoren |
EP1319842A1 (de) * | 2001-12-17 | 2003-06-18 | Techspace Aero S.A. | Rotor oder rotierendes Element für Turboverdichter |
US6887043B2 (en) | 2003-03-28 | 2005-05-03 | General Electric Company | Methods and apparatus for assembling gas turbine engines |
FR2869374B1 (fr) * | 2004-04-23 | 2009-01-30 | Snecma Moteurs Sa | Systeme de fixation de pieces par des goujons a collerettes |
FR2933887B1 (fr) * | 2008-07-18 | 2010-09-17 | Snecma | Procede de reparation ou de reprise d'un disque de turbomachine et disque de turbomachine repare ou repris |
FR2935429B1 (fr) * | 2008-08-26 | 2011-11-25 | Snecma | Aubage fixe de turbomachine a masse reduite et turbomachine comportant au moins un tel aubage fixe |
US8162615B2 (en) * | 2009-03-17 | 2012-04-24 | United Technologies Corporation | Split disk assembly for a gas turbine engine |
US10233941B2 (en) * | 2013-07-12 | 2019-03-19 | United Technologies Corporation | Plastic variable inlet guide vane |
Family Cites Families (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB599809A (en) * | 1945-01-15 | 1948-03-22 | Bristol Aeroplane Co Ltd | Improvements in axial flow compressors, turbines and the like |
US768597A (en) * | 1902-08-21 | 1904-08-30 | Gen Electric | Turbine-bucket. |
US980732A (en) * | 1910-07-09 | 1911-01-03 | Gen Electric | Bucket structure for turbines. |
US1118361A (en) * | 1914-06-19 | 1914-11-24 | Gen Electric | Wheel for elastic-fluid turbines. |
GB394001A (en) * | 1931-12-18 | 1933-06-19 | Parsons C A & Co Ltd | Improvements in and relating to built-up rotors, suitable for steam turbines |
DE729493C (de) * | 1941-01-07 | 1942-12-17 | Siemens Ag | Aus axial miteinander verschraubten Drehkoerpern zusammengesetzter Laeufer fuer Kreiselmaschinen, insbesondere Dampf- oder Gasturbinen |
DE840880C (de) * | 1941-09-08 | 1952-06-09 | Daimler Benz Ag | Laufrad fuer Axialturbomaschinen, insbesondere fuer Axialverdichter |
GB578191A (en) * | 1941-11-21 | 1946-06-19 | Frank Bernard Halford | Improvements in or relating to turbines |
FR895583A (fr) * | 1942-05-21 | 1945-01-29 | Roue motrice ou rotor pour turbines à gaz refroidies | |
GB579425A (en) * | 1943-10-06 | 1946-08-02 | Frank Robert Bell | Improvements in blade drums for axial-flow compressors and turbines |
US2452782A (en) * | 1945-01-16 | 1948-11-02 | Power Jets Res & Dev Ltd | Construction of rotors for compressors and like machines |
GB642287A (en) * | 1948-07-01 | 1950-08-30 | English Electric Co Ltd | Improvements in and relating to the connection of spigotted components of multi-stage compressor rotors |
FR1012335A (fr) * | 1949-07-13 | 1952-07-08 | Hispano Suiza Sa | Perfectionnements apportés aux engins, notamment aux compresseurs axiaux, à rotor équipé de plusieurs aubages disposés en tandem |
-
0
- BE BE507205D patent/BE507205A/xx unknown
-
1950
- 1950-12-08 GB GB30065/50A patent/GB695221A/en not_active Expired
-
1951
- 1951-11-09 DE DEA14374A patent/DE967778C/de not_active Expired
- 1951-11-15 FR FR1056070D patent/FR1056070A/fr not_active Expired
- 1951-11-15 US US256475A patent/US2738126A/en not_active Expired - Lifetime
- 1951-11-21 CH CH316506D patent/CH316506A/fr unknown
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2884186A (en) * | 1954-04-23 | 1959-04-28 | Stalker Corp | Rotor construction for axial flow compressors |
US2804323A (en) * | 1954-08-19 | 1957-08-27 | Rolls Royce | Axial-flow compressors and turbines |
DE1062881B (de) * | 1956-08-24 | 1959-08-06 | Krantz H Fa | Axialventilator mit bei Stillstand im Nabenkranz auf verschiedene Anstellwinkel einstellbaren Laufschaufeln |
FR2607866A1 (fr) * | 1986-12-03 | 1988-06-10 | Snecma | Axes de fixation de rotors de turbomachine, procede de montage et rotors ainsi montes |
EP0272966A1 (de) * | 1986-12-03 | 1988-06-29 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" | Verbindungselement für die Rotorscheiben einer Turbomaschine |
US4844694A (en) * | 1986-12-03 | 1989-07-04 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation (Snecma) | Fastening spindle and method of assembly for attaching rotor elements of a gas-turbine engine |
US5378110A (en) * | 1992-09-14 | 1995-01-03 | United Technologies Corporation | Composite compressor rotor with removable airfoils |
DE19627386A1 (de) * | 1995-07-13 | 1997-01-16 | Bmw Rolls Royce Gmbh | Verbindungs-Anordnung für zwei Turbinen-Laufradscheiben |
Also Published As
Publication number | Publication date |
---|---|
US2738126A (en) | 1956-03-13 |
CH316506A (fr) | 1956-10-15 |
DE967778C (de) | 1958-01-16 |
BE507205A (de) | |
GB695221A (en) | 1953-08-05 |
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