CH512005A - Ailette pour machine à flux de fluide élastique - Google Patents

Ailette pour machine à flux de fluide élastique

Info

Publication number
CH512005A
CH512005A CH1175769A CH1175769A CH512005A CH 512005 A CH512005 A CH 512005A CH 1175769 A CH1175769 A CH 1175769A CH 1175769 A CH1175769 A CH 1175769A CH 512005 A CH512005 A CH 512005A
Authority
CH
Switzerland
Prior art keywords
vane
fluid flow
flow machine
elastic fluid
elastic
Prior art date
Application number
CH1175769A
Other languages
English (en)
French (fr)
Inventor
Godfrey Morley John
Original Assignee
Rolls Royce
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 Rolls Royce filed Critical Rolls Royce
Publication of CH512005A publication Critical patent/CH512005A/fr

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
    • F01D5/28—Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
    • F01D5/282—Selecting composite materials, e.g. blades with reinforcing filaments

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Materials Engineering (AREA)
  • Composite Materials (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
CH1175769A 1968-08-01 1969-08-01 Ailette pour machine à flux de fluide élastique CH512005A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB36874/68A GB1268202A (en) 1968-08-01 1968-08-01 Composite blade for an elastic fluid flow machine

Publications (1)

Publication Number Publication Date
CH512005A true CH512005A (fr) 1971-08-31

Family

ID=10391884

Family Applications (1)

Application Number Title Priority Date Filing Date
CH1175769A CH512005A (fr) 1968-08-01 1969-08-01 Ailette pour machine à flux de fluide élastique

Country Status (6)

Country Link
US (1) US3602608A (enExample)
BE (1) BE736883A (enExample)
CA (1) CA923427A (enExample)
CH (1) CH512005A (enExample)
FR (1) FR2014880A1 (enExample)
GB (1) GB1268202A (enExample)

Families Citing this family (26)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3717419A (en) * 1971-07-09 1973-02-20 Susquehanna Corp Turbine blade
GB1411379A (en) * 1971-12-21 1975-10-22 Rolls Royce Fibre reinforced composite structures
US3799701A (en) * 1972-02-28 1974-03-26 United Aircraft Corp Composite fan blade and method of construction
US3756745A (en) * 1972-03-15 1973-09-04 United Aircraft Corp Composite blade root configuration
US3749518A (en) * 1972-03-15 1973-07-31 United Aircraft Corp Composite blade root configuration
FR2195255A5 (enExample) * 1972-08-04 1974-03-01 Snecma
US3949711A (en) * 1974-02-08 1976-04-13 Stackpole Carbon Company Rotary engine with graphite housing
US4022547A (en) * 1975-10-02 1977-05-10 General Electric Company Composite blade employing biased layup
US4000956A (en) * 1975-12-22 1977-01-04 General Electric Company Impact resistant blade
US4051289A (en) * 1976-04-12 1977-09-27 General Electric Company Composite airfoil construction
US4108572A (en) * 1976-12-23 1978-08-22 United Technologies Corporation Composite rotor blade
US4354804A (en) * 1979-11-30 1982-10-19 Williams Research Corporation Composite turbine wheel, method of manufacture and fixture therefor
US4627791A (en) * 1982-11-10 1986-12-09 Marshall Andrew C Aeroelastically responsive composite propeller
US4815940A (en) * 1986-08-04 1989-03-28 United Technologies Corporation Fatigue strengthened composite article
US5403153A (en) * 1993-10-29 1995-04-04 The United States Of America As Represented By The Secretary Of The Air Force Hollow composite turbine blade
US5449273A (en) * 1994-03-21 1995-09-12 United Technologies Corporation Composite airfoil leading edge protection
US5655883A (en) * 1995-09-25 1997-08-12 General Electric Company Hybrid blade for a gas turbine
FI101565B (fi) * 1997-01-17 1998-07-15 Flaekt Woods Ab Haihdutinpuhallin ja sen siipipyörä
FI101564B (fi) 1997-01-17 1998-07-15 Flaekt Woods Ab Korkeapainepuhallin
DE19751129C1 (de) * 1997-11-19 1999-06-17 Mtu Muenchen Gmbh FAN-Rotorschaufel für ein Triebwerk
JP2011137386A (ja) * 2009-12-25 2011-07-14 Mitsubishi Heavy Ind Ltd 風車回転翼および風車回転翼の製造方法
US20120021243A1 (en) * 2010-07-23 2012-01-26 General Electric Company Components with bonded edges
US8387504B2 (en) 2011-01-06 2013-03-05 General Electric Company Fiber-reinforced Al-Li compressor airfoil and method of fabricating
GB201111598D0 (en) 2011-07-07 2011-08-24 Rolls Royce Plc Layered composite component
JP5982837B2 (ja) 2012-01-30 2016-08-31 株式会社Ihi 航空機用ジェットエンジンのファン動翼
JP6083112B2 (ja) 2012-01-30 2017-02-22 株式会社Ihi 航空機用ジェットエンジンのファン動翼

Also Published As

Publication number Publication date
US3602608A (en) 1971-08-31
GB1268202A (en) 1972-03-22
DE1938300B2 (de) 1971-05-06
BE736883A (enExample) 1969-12-31
DE1938300A1 (enExample) 1971-05-06
CA923427A (en) 1973-03-27
FR2014880A1 (enExample) 1970-04-24

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