BE541360A - - Google Patents
Info
- Publication number
- BE541360A BE541360A BE541360DA BE541360A BE 541360 A BE541360 A BE 541360A BE 541360D A BE541360D A BE 541360DA BE 541360 A BE541360 A BE 541360A
- Authority
- BE
- Belgium
Links
Classifications
-
- E—FIXED CONSTRUCTIONS
- E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
- E05B—LOCKS; ACCESSORIES THEREFOR; HANDCUFFS
- E05B27/00—Cylinder locks or other locks with tumbler pins or balls that are set by pushing the key in
-
- 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
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16D—COUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
- F16D1/00—Couplings for rigidly connecting two coaxial shafts or other movable machine elements
- F16D1/10—Quick-acting couplings in which the parts are connected by simply bringing them together axially
- F16D1/108—Quick-acting couplings in which the parts are connected by simply bringing them together axially having retaining means rotating with the coupling and acting by interengaging parts, i.e. positive coupling
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16D—COUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
- F16D1/00—Couplings for rigidly connecting two coaxial shafts or other movable machine elements
- F16D1/06—Couplings for rigidly connecting two coaxial shafts or other movable machine elements for attachment of a member on a shaft or on a shaft-end
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16D—COUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
- F16D1/00—Couplings for rigidly connecting two coaxial shafts or other movable machine elements
- F16D1/10—Quick-acting couplings in which the parts are connected by simply bringing them together axially
- F16D2001/103—Quick-acting couplings in which the parts are connected by simply bringing them together axially the torque is transmitted via splined connections
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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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49316—Impeller making
- Y10T29/4932—Turbomachine making
- Y10T29/49321—Assembling individual fluid flow interacting members, e.g., blades, vanes, buckets, on rotary support member
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Mechanical Operated Clutches (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB28027/54A GB780434A (en) | 1954-09-28 | 1954-09-28 | Improvements in or relating to rotors of turbines and compressors |
Publications (1)
Publication Number | Publication Date |
---|---|
BE541360A true BE541360A (ko) |
Family
ID=10269083
Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BE541380D BE541380A (ko) | 1954-09-28 | ||
BE541360D BE541360A (ko) | 1954-09-28 |
Family Applications Before (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BE541380D BE541380A (ko) | 1954-09-28 |
Country Status (4)
Country | Link |
---|---|
US (1) | US2928649A (ko) |
BE (2) | BE541360A (ko) |
FR (1) | FR1130803A (ko) |
GB (1) | GB780434A (ko) |
Families Citing this family (20)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
NL246286A (ko) * | 1956-01-25 | |||
GB1286235A (en) * | 1970-01-20 | 1972-08-23 | Rolls Royce | A rotary bladed structure for a fluid flow machine |
DE2140816A1 (de) * | 1971-08-14 | 1973-03-01 | Motoren Turbinen Union | Rotor fuer stroemungsmaschinen |
BE787539A (fr) * | 1971-08-27 | 1973-02-14 | Alsthom Cgee | Elements constitutifs d'un rotor soude |
US3914070A (en) * | 1973-11-19 | 1975-10-21 | Avco Corp | Two-stage tie-down of turbomachine rotor |
US4728255A (en) * | 1985-02-25 | 1988-03-01 | General Electric Company | Removable stiffening disk |
US4664599A (en) * | 1985-05-01 | 1987-05-12 | United Technologies Corporation | Two stage turbine rotor assembly |
US4953282A (en) * | 1988-01-11 | 1990-09-04 | General Electric Company | Stator vane mounting method and assembly |
US4868963A (en) * | 1988-01-11 | 1989-09-26 | General Electric Company | Stator vane mounting method and assembly |
GB9910594D0 (en) * | 1999-05-07 | 1999-07-07 | Rolls Royce Plc | Improved rotor-shaft connector |
US6572337B1 (en) * | 1999-11-30 | 2003-06-03 | General Electric Co. | Turbine rotor torque transmission |
DE102004035611A1 (de) * | 2004-07-22 | 2006-02-16 | Gkn Driveline International Gmbh | Verbindung zweier Bauteile |
US7661260B2 (en) * | 2006-09-27 | 2010-02-16 | General Electric Company | Gas turbine engine assembly and method of assembling same |
FR2958322B1 (fr) * | 2010-04-01 | 2013-03-15 | Snecma | Rotor de moteur a turbine a gaz comprenant un tambour de rotor et une couronne de rotor |
US9169730B2 (en) | 2011-11-16 | 2015-10-27 | Pratt & Whitney Canada Corp. | Fan hub design |
US9695714B2 (en) * | 2013-04-22 | 2017-07-04 | United Technologies Corporation | Low loss bearing drain |
KR101896436B1 (ko) * | 2017-04-12 | 2018-09-10 | 두산중공업 주식회사 | 보강디스크를 포함하는 압축기 및 이를 포함하는 가스터빈 |
US10584599B2 (en) * | 2017-07-14 | 2020-03-10 | United Technologies Corporation | Compressor rotor stack assembly for gas turbine engine |
US20220407384A1 (en) * | 2021-06-22 | 2022-12-22 | Borgwarner Inc. | Rotor and method |
FR3126145B1 (fr) * | 2021-08-10 | 2024-01-05 | Safran Trans Systems | Arbre cannelé |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
BE448571A (ko) * | 1942-02-18 | |||
GB586200A (en) * | 1944-07-21 | 1947-03-11 | Karl Baumann | Improvements in bladed drum-type rotor constructions operating under high temperature conditions |
FR961172A (ko) * | 1947-02-17 | 1950-05-06 | ||
GB715044A (en) * | 1952-07-29 | 1954-09-08 | Rolls Royce | Improvements in or relating to rotors of turbines and compressors |
-
0
- BE BE541380D patent/BE541380A/xx unknown
- BE BE541360D patent/BE541360A/xx unknown
-
1954
- 1954-09-28 GB GB28027/54A patent/GB780434A/en not_active Expired
-
1955
- 1955-08-22 US US529611A patent/US2928649A/en not_active Expired - Lifetime
- 1955-09-06 FR FR1130803D patent/FR1130803A/fr not_active Expired
Also Published As
Publication number | Publication date |
---|---|
GB780434A (en) | 1957-07-31 |
BE541380A (ko) | |
FR1130803A (fr) | 1957-02-12 |
US2928649A (en) | 1960-03-15 |