MY6900151A - Contact heat fusing device - Google Patents

Contact heat fusing device

Info

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
Application number
MY1969151A
Original Assignee
Rank Xerox Ltd.
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
Application filed by Rank Xerox Ltd. filed Critical Rank Xerox Ltd.
Publication of MY6900151A publication Critical patent/MY6900151A/en

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)
MY1969151A 1965-07-31 1969-12-31 Contact heat fusing device MY6900151A (en)

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 (en)
DE (1) DE1301638B (en)
GB (1) GB1084537A (en)
MY (1) MY6900151A (en)

Families Citing this family (16)

* Cited by examiner, † Cited by third party
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 (en) * 2007-06-27 2009-01-15 Toshiba Corp Intermediate fixing and supporting structure for steam-turbine long moving blade train, and steam turbine
US8602351B2 (en) 2009-09-17 2013-12-10 Textron Innovations Inc. Removable horizontal stabilizer for helicopter
US8398374B2 (en) * 2010-01-27 2013-03-19 General Electric Company Method and apparatus for a segmented turbine bucket assembly
DE102010041702A1 (en) * 2010-09-30 2012-04-05 Siemens Aktiengesellschaft Coupling bolt for turbine blades

Family Cites Families (9)

* Cited by examiner, † Cited by third party
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 (en) * 1949-02-17 1951-10-31 Escher Wyss Ag Blading on rotors of centrifugal machines through which axial flow flows, especially steam, gas turbines and compressors
FR1033197A (en) * 1951-02-27 1953-07-08 Rateau Soc Vibration dampers for mobile turbo-machine blades
US2771267A (en) * 1952-05-27 1956-11-20 United Aircraft Corp Lacing for compressor blades
FR69842E (en) * 1956-05-30 1958-12-30 Rateau Soc Vibration dampers for mobile turbo-machine blades
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

Also Published As

Publication number Publication date
GB1084537A (en) 1967-09-27
DE1301638B (en) 1969-08-21
US3327995A (en) 1967-06-27

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