FR1136237A - Improvements made to the blades for installations with gas turbines - Google Patents

Improvements made to the blades for installations with gas turbines

Info

Publication number
FR1136237A
FR1136237A FR1136237DA FR1136237A FR 1136237 A FR1136237 A FR 1136237A FR 1136237D A FR1136237D A FR 1136237DA FR 1136237 A FR1136237 A FR 1136237A
Authority
FR
France
Prior art keywords
installations
blades
improvements made
gas turbines
turbines
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.)
Expired
Application number
Other languages
French (fr)
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.)
Power Jets Research and Development Ltd
Original Assignee
Power Jets Research and Development 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 Power Jets Research and Development Ltd filed Critical Power Jets Research and Development Ltd
Application granted granted Critical
Publication of FR1136237A publication Critical patent/FR1136237A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/04—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
    • F02C3/06—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor the compressor comprising only axial stages
    • F02C3/073—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor the compressor comprising only axial stages the compressor and turbine stages being concentric
    • 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
    • F01D5/14—Form or construction
    • 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)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
FR1136237D 1954-11-30 1955-11-28 Improvements made to the blades for installations with gas turbines Expired FR1136237A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1136237X 1954-11-30

Publications (1)

Publication Number Publication Date
FR1136237A true FR1136237A (en) 1957-05-10

Family

ID=10876782

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1136237D Expired FR1136237A (en) 1954-11-30 1955-11-28 Improvements made to the blades for installations with gas turbines

Country Status (1)

Country Link
FR (1) FR1136237A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1126196B (en) * 1958-11-24 1962-03-22 Rolls Royce Gas turbine jet engine with bypass compressor
EP0333585A1 (en) * 1988-03-16 1989-09-20 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" Combined propulsion unit provided with an air breathing turbo jet
FR2652387A1 (en) * 1989-09-27 1991-03-29 Snecma PROPULSION ENGINE WITH CONTRAROTATIVE BLOWERS.

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1126196B (en) * 1958-11-24 1962-03-22 Rolls Royce Gas turbine jet engine with bypass compressor
EP0333585A1 (en) * 1988-03-16 1989-09-20 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" Combined propulsion unit provided with an air breathing turbo jet
FR2628790A1 (en) * 1988-03-16 1989-09-22 Snecma COMBINED TURBOFUSED COMBINER AEROBIE
FR2652387A1 (en) * 1989-09-27 1991-03-29 Snecma PROPULSION ENGINE WITH CONTRAROTATIVE BLOWERS.
EP0420746A1 (en) * 1989-09-27 1991-04-03 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" Contrarotative fan jet engine

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