DE277906T1 - Rotorscheibe aus verbundwerkstoff. - Google Patents

Rotorscheibe aus verbundwerkstoff.

Info

Publication number
DE277906T1
DE277906T1 DE198888630016T DE88630016T DE277906T1 DE 277906 T1 DE277906 T1 DE 277906T1 DE 198888630016 T DE198888630016 T DE 198888630016T DE 88630016 T DE88630016 T DE 88630016T DE 277906 T1 DE277906 T1 DE 277906T1
Authority
DE
Germany
Prior art keywords
rotor disc
composite rotor
composite
disc
rotor
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.)
Pending
Application number
DE198888630016T
Other languages
English (en)
Inventor
William T. Vernon Connecticut 06066 Us Dennison
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Raytheon Technologies Corp
Original Assignee
United Technologies Corp
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 United Technologies Corp filed Critical United Technologies Corp
Publication of DE277906T1 publication Critical patent/DE277906T1/de
Pending legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/02Blade-carrying members, e.g. rotors
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12Blades
    • F01D5/28Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
    • F01D5/282Selecting composite materials, e.g. blades with reinforcing filaments
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D7/00Rotors with blades adjustable in operation; Control thereof
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00Function
    • F05D2260/70Adjusting of angle of incidence or attack of rotating blades
    • F05D2260/74Adjusting of angle of incidence or attack of rotating blades by turning around an axis perpendicular the rotor centre line
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00Function
    • F05D2260/70Adjusting of angle of incidence or attack of rotating blades
    • F05D2260/76Adjusting of angle of incidence or attack of rotating blades the adjusting mechanism using auxiliary power sources
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient propulsion technologies, e.g. for aircraft
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/21Circular sheet or circular blank
    • Y10T428/218Aperture containing
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/24Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24058Structurally defined web or sheet [e.g., overall dimension, etc.] including grain, strips, or filamentary elements in respective layers or components in angular relation
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/24Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24058Structurally defined web or sheet [e.g., overall dimension, etc.] including grain, strips, or filamentary elements in respective layers or components in angular relation
    • Y10T428/24124Fibers

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Materials Engineering (AREA)
  • Composite Materials (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Mounting Of Bearings Or Others (AREA)
  • Laminated Bodies (AREA)
DE198888630016T 1987-02-02 1988-02-01 Rotorscheibe aus verbundwerkstoff. Pending DE277906T1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US07/010,237 US4717610A (en) 1987-02-02 1987-02-02 Composite disk for supporting fan blades

Publications (1)

Publication Number Publication Date
DE277906T1 true DE277906T1 (de) 1988-12-15

Family

ID=21744716

Family Applications (2)

Application Number Title Priority Date Filing Date
DE198888630016T Pending DE277906T1 (de) 1987-02-02 1988-02-01 Rotorscheibe aus verbundwerkstoff.
DE8888630016T Expired - Fee Related DE3871973T2 (de) 1987-02-02 1988-02-01 Rotorscheibe aus verbundwerkstoff.

Family Applications After (1)

Application Number Title Priority Date Filing Date
DE8888630016T Expired - Fee Related DE3871973T2 (de) 1987-02-02 1988-02-01 Rotorscheibe aus verbundwerkstoff.

Country Status (4)

Country Link
US (1) US4717610A (de)
EP (1) EP0277906B1 (de)
JP (1) JP2602682B2 (de)
DE (2) DE277906T1 (de)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5102302A (en) * 1988-06-02 1992-04-07 General Electric Company Fan blade mount
US5165856A (en) * 1988-06-02 1992-11-24 General Electric Company Fan blade mount
DE4237031C1 (de) * 1992-11-03 1994-02-10 Mtu Muenchen Gmbh Verstellbare Leitschaufel
US8794925B2 (en) 2010-08-24 2014-08-05 United Technologies Corporation Root region of a blade for a gas turbine engine
EP2997230B1 (de) 2013-05-17 2021-08-11 Raytheon Technologies Corporation Tangentialer schaufelfusshals mit konischer form
US10247102B2 (en) 2013-06-12 2019-04-02 United Technologies Corporation Fuel/oil manifold
US9869198B2 (en) 2015-05-13 2018-01-16 General Electric Company Intershaft integrated seal and lock-nut
US9976429B2 (en) 2015-06-09 2018-05-22 General Electric Company Composite disk

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2802680A (en) * 1952-05-15 1957-08-13 Kennametal Inc Turbine wheel assembly
AT232635B (de) * 1962-08-17 1964-03-25 Simmering Graz Pauker Ag Laufradschaufelbefestigung für eine Axial-Turbomaschine mit Verstellschaufeln
FR1494085A (fr) * 1966-02-01 1967-09-08 Calor App Electro Domestiques Ventilateur à hélice à pas variable
US3532439A (en) * 1966-11-29 1970-10-06 Rolls Royce Fibrous reinforced bladed rotor
US3622249A (en) * 1968-08-18 1971-11-23 Aisin Seiki Fan assembly
US3687569A (en) * 1971-03-19 1972-08-29 Gen Electric Rotor with variable angle blades
FR2143561B1 (de) * 1971-06-29 1974-03-08 Snecma
US4021142A (en) * 1974-10-09 1977-05-03 United Technologies Corporation Pitch-change apparatus for a ducted thrust fan
US4045149A (en) * 1976-02-03 1977-08-30 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Platform for a swing root turbomachinery blade
US4863352A (en) * 1984-11-02 1989-09-05 General Electric Company Blade carrying means

Also Published As

Publication number Publication date
EP0277906A2 (de) 1988-08-10
JPS63266131A (ja) 1988-11-02
DE3871973T2 (de) 1993-02-18
US4717610A (en) 1988-01-05
EP0277906A3 (en) 1990-01-31
EP0277906B1 (de) 1992-06-17
DE3871973D1 (de) 1992-07-23
JP2602682B2 (ja) 1997-04-23

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