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CH466641A - Compressor blade, especially for the first stage of a jet engine - Google Patents

Compressor blade, especially for the first stage of a jet engine

Info

Publication number
CH466641A
CH466641A CH1226667A CH1226667A CH466641A CH 466641 A CH466641 A CH 466641A CH 1226667 A CH1226667 A CH 1226667A CH 1226667 A CH1226667 A CH 1226667A CH 466641 A CH466641 A CH 466641A
Authority
CH
Switzerland
Prior art keywords
stage
jet engine
compressor blade
compressor
blade
Prior art date
Application number
CH1226667A
Other languages
German (de)
Inventor
John Stoffer Lewis
Original Assignee
Gen Electric
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 Gen Electric filed Critical Gen Electric
Publication of CH466641A publication Critical patent/CH466641A/en

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00—Details, component parts, or accessories
    • F04D29/26—Rotors specially for elastic fluids
    • F04D29/32—Rotors specially for elastic fluids for axial flow pumps
    • F04D29/321—Rotors specially for elastic fluids for axial flow pumps for axial flow compressors
    • F04D29/324—Blades

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
CH1226667A 1966-12-01 1967-09-01 Compressor blade, especially for the first stage of a jet engine CH466641A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US59842866A 1966-12-01 1966-12-01

Publications (1)

Publication Number Publication Date
CH466641A true CH466641A (en) 1968-12-15

Family

ID=24395500

Family Applications (1)

Application Number Title Priority Date Filing Date
CH1226667A CH466641A (en) 1966-12-01 1967-09-01 Compressor blade, especially for the first stage of a jet engine

Country Status (6)

Country Link
BE (1) BE702035A (en)
CH (1) CH466641A (en)
DE (1) DE1628267A1 (en)
GB (1) GB1187076A (en)
NL (1) NL6711968A (en)
SE (1) SE319857B (en)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3234011A1 (en) * 1982-09-14 1984-03-15 Braun Ag, 6000 Frankfurt Axial fan
US9249666B2 (en) 2011-12-22 2016-02-02 General Electric Company Airfoils for wake desensitization and method for fabricating same
CN103835995B (en) * 2012-11-22 2016-04-27 威海克莱特菲尔风机股份有限公司 There is the large-scale axial-flow blower of profile of tooth leading edge blade
CN102927046B (en) * 2012-11-22 2015-04-29 威海克莱特菲尔风机股份有限公司 Low-noise efficient impeller of axial-flow fan
CN113266602A (en) * 2021-06-18 2021-08-17 中山百得厨卫有限公司 Noise-reduction centrifugal wind wheel capable of maintaining static pressure and range hood
CN115673669B (en) * 2022-11-11 2024-05-14 中国航发沈阳黎明航空发动机有限责任公司 Repair method for low-pressure turbine working She Pianju tooth crown
CN116641913B (en) * 2023-01-13 2025-11-07 新界泵业(浙江)有限公司 Centrifugal pump impeller for stirring and diluting non-Newtonian fluid delivery and design method thereof

Also Published As

Publication number Publication date
GB1187076A (en) 1970-04-08
NL6711968A (en) 1968-06-04
SE319857B (en) 1970-01-26
DE1628267A1 (en) 1971-11-04
BE702035A (en) 1968-01-02

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