MY6900151A - Contact heat fusing device - Google Patents
Contact heat fusing deviceInfo
- Publication number
- MY6900151A MY6900151A MY1969151A MY6900151A MY6900151A MY 6900151 A MY6900151 A MY 6900151A MY 1969151 A MY1969151 A MY 1969151A MY 6900151 A MY6900151 A MY 6900151A MY 6900151 A MY6900151 A MY 6900151A
- Authority
- MY
- Malaysia
- Prior art keywords
- contact heat
- fusing device
- heat fusing
- contact
- heat
- Prior art date
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
- F01D5/22—Blade-to-blade connections, e.g. for damping vibrations
-
- 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)
- Structures Of Non-Positive Displacement Pumps (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB32861/65A GB1084537A (en) | 1965-07-31 | 1965-07-31 | A compressor or turbine rotor for a gas turbine engine |
Publications (1)
Publication Number | Publication Date |
---|---|
MY6900151A true MY6900151A (en) | 1969-12-31 |
Family
ID=10345112
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
MY1969151A MY6900151A (en) | 1965-07-31 | 1969-12-31 | Contact heat fusing device |
Country Status (4)
Country | Link |
---|---|
US (1) | US3327995A (de) |
DE (1) | DE1301638B (de) |
GB (1) | GB1084537A (de) |
MY (1) | MY6900151A (de) |
Families Citing this family (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1142877A (en) * | 1966-06-28 | 1969-02-12 | Rolls Royce | Improvements in or relating to bladed rotors, particularly for use in gas turbine engines |
US3799701A (en) * | 1972-02-28 | 1974-03-26 | United Aircraft Corp | Composite fan blade and method of construction |
US3796513A (en) * | 1972-06-19 | 1974-03-12 | Westinghouse Electric Corp | High damping blades |
US3936230A (en) * | 1974-05-09 | 1976-02-03 | The United States Of America As Represented By The Secretary Of The Air Force | Self-supported, self-locating seal for turbine engines |
US4257741A (en) * | 1978-11-02 | 1981-03-24 | General Electric Company | Turbine engine blade with airfoil projection |
US4326836A (en) * | 1979-12-13 | 1982-04-27 | United Technologies Corporation | Shroud for a rotor blade |
US5083903A (en) * | 1990-07-31 | 1992-01-28 | General Electric Company | Shroud insert for turbomachinery blade |
US5137426A (en) * | 1990-08-06 | 1992-08-11 | General Electric Company | Blade shroud deformable protective coating |
US5267834A (en) * | 1992-12-30 | 1993-12-07 | General Electric Company | Bucket for the last stage of a steam turbine |
US6039542A (en) * | 1997-12-24 | 2000-03-21 | General Electric Company | Panel damped hybrid blade |
US6282786B1 (en) | 1999-08-16 | 2001-09-04 | General Electric Company | Method of making injection formed hybrid airfoil |
US6099257A (en) * | 1999-08-31 | 2000-08-08 | General Electric Company | Plastically formed hybrid airfoil |
JP2009007981A (ja) * | 2007-06-27 | 2009-01-15 | Toshiba Corp | 蒸気タービン用長動翼翼列の中間固定支持構造及び蒸気タービン |
IN2012DN02173A (de) | 2009-09-17 | 2015-08-21 | Bell Helicopter Textron Inc | |
US8398374B2 (en) * | 2010-01-27 | 2013-03-19 | General Electric Company | Method and apparatus for a segmented turbine bucket assembly |
DE102010041702A1 (de) * | 2010-09-30 | 2012-04-05 | Siemens Aktiengesellschaft | Koppelbolzen für Turbinenschaufeln |
Family Cites Families (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1618296A (en) * | 1925-08-01 | 1927-02-22 | Westinghouse Electric & Mfg Co | Turbine-blade lashing |
US1749449A (en) * | 1928-06-06 | 1930-03-04 | Westinghouse Electric & Mfg Co | Turbine blading and lashing therefor |
GB358406A (en) * | 1930-02-28 | 1931-10-08 | British Thomson Houston Co Ltd | Improvements in and relating to elastic fluid turbines |
DE819242C (de) * | 1949-02-17 | 1951-10-31 | Escher Wyss Ag | Beschaufelung an Rotoren von axial durchstroemten Kreiselmaschinen, insbesondere von Dampf-, Gasturbinen und Verdichtern |
FR1033197A (fr) * | 1951-02-27 | 1953-07-08 | Rateau Soc | Amortisseurs de vibrations pour aubages mobiles de turbo-machines |
US2771267A (en) * | 1952-05-27 | 1956-11-20 | United Aircraft Corp | Lacing for compressor blades |
FR69842E (fr) * | 1956-05-30 | 1958-12-30 | Rateau Soc | Amortisseurs de vibrations pour aubages mobiles de turbo-machines |
US2912157A (en) * | 1957-05-10 | 1959-11-10 | United Aircraft Corp | Cambered shroud |
US3216699A (en) * | 1963-10-24 | 1965-11-09 | Gen Electric | Airfoil member assembly |
-
1965
- 1965-07-31 GB GB32861/65A patent/GB1084537A/en not_active Expired
-
1966
- 1966-07-07 US US563558A patent/US3327995A/en not_active Expired - Lifetime
- 1966-07-18 DE DER43722A patent/DE1301638B/de active Pending
-
1969
- 1969-12-31 MY MY1969151A patent/MY6900151A/xx unknown
Also Published As
Publication number | Publication date |
---|---|
DE1301638B (de) | 1969-08-21 |
US3327995A (en) | 1967-06-27 |
GB1084537A (en) | 1967-09-27 |
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