GB867849A - Improvements in or relating to axial flow compressors, and their applications - Google Patents

Improvements in or relating to axial flow compressors, and their applications

Info

Publication number
GB867849A
GB867849A GB8979/58A GB897958A GB867849A GB 867849 A GB867849 A GB 867849A GB 8979/58 A GB8979/58 A GB 8979/58A GB 897958 A GB897958 A GB 897958A GB 867849 A GB867849 A GB 867849A
Authority
GB
United Kingdom
Prior art keywords
air
returned
nozzles
stream
intake
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
GB8979/58A
Other languages
English (en)
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Publication of GB867849A publication Critical patent/GB867849A/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
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
    • F02C7/047—Heating to prevent icing
    • 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
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D27/00—Control, e.g. regulation, of pumps, pumping installations or pumping systems specially adapted for elastic fluids
    • F04D27/02—Surge control
    • F04D27/0207—Surge control by bleeding, bypassing or recycling fluids
    • F04D27/0238—Details or means for fluid reinjection
    • 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)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Sustainable Development (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
GB8979/58A 1957-04-04 1958-03-20 Improvements in or relating to axial flow compressors, and their applications Expired GB867849A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1192929T 1957-04-04

Publications (1)

Publication Number Publication Date
GB867849A true GB867849A (en) 1961-05-10

Family

ID=9667625

Family Applications (1)

Application Number Title Priority Date Filing Date
GB8979/58A Expired GB867849A (en) 1957-04-04 1958-03-20 Improvements in or relating to axial flow compressors, and their applications

Country Status (2)

Country Link
FR (1) FR1192929A (fr)
GB (1) GB867849A (fr)

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5429644B1 (fr) * 1970-05-04 1979-09-25
FR2464863A1 (fr) * 1979-09-10 1981-03-20 Do Gpkexi Komplex Mekh Shakht Groupe moteur de propulsion d'un vehicule de transport a coussin d'air
EP1783048A3 (fr) * 2005-11-08 2009-08-19 Hamilton Sundstrand Corporation Soupape intégrée d'un compresseur pour la régulation de l'apport de chaleur et du pompage
CN101900102A (zh) * 2010-08-16 2010-12-01 黑龙江建龙钢铁有限公司 空气压缩机入口防冻方法及其装置
US8128347B2 (en) 2006-08-25 2012-03-06 Rolls-Royce Plc Aeroengine bleed valve
WO2017017378A1 (fr) * 2015-07-30 2017-02-02 Safran Aircraft Engines Systeme d'antigivrage d'une aube de turbomachine.
FR3039590A1 (fr) * 2015-07-30 2017-02-03 Snecma Systeme d'antigivrage d'une aube de turbomachine
EP3225813A1 (fr) * 2016-03-30 2017-10-04 General Electric Company Ensemble de passage de flux d'air à soupape permettant de régler la distorsion de flux d'air dans un moteur à turbine à gaz
US10753278B2 (en) 2016-03-30 2020-08-25 General Electric Company Translating inlet for adjusting airflow distortion in gas turbine engine
US10794281B2 (en) 2016-02-02 2020-10-06 General Electric Company Gas turbine engine having instrumented airflow path components

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3123285A (en) * 1964-03-03 Diffuser with boundary layer control
US3121312A (en) * 1961-02-28 1964-02-18 United Aircraft Corp Unified pitch, yaw and roll shock control

Cited By (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5429644B1 (fr) * 1970-05-04 1979-09-25
FR2464863A1 (fr) * 1979-09-10 1981-03-20 Do Gpkexi Komplex Mekh Shakht Groupe moteur de propulsion d'un vehicule de transport a coussin d'air
EP1783048A3 (fr) * 2005-11-08 2009-08-19 Hamilton Sundstrand Corporation Soupape intégrée d'un compresseur pour la régulation de l'apport de chaleur et du pompage
EP2377759A1 (fr) * 2005-11-08 2011-10-19 Hamilton Sundstrand Corporation Soupape intégrée d'un compresseur pour la régulation de l'apport de chaleur et du pompage
US8128347B2 (en) 2006-08-25 2012-03-06 Rolls-Royce Plc Aeroengine bleed valve
CN101900102A (zh) * 2010-08-16 2010-12-01 黑龙江建龙钢铁有限公司 空气压缩机入口防冻方法及其装置
US20180216528A1 (en) * 2015-07-30 2018-08-02 Safran Aircraft Engines Anti-icing system for a turbine engine vane
FR3039590A1 (fr) * 2015-07-30 2017-02-03 Snecma Systeme d'antigivrage d'une aube de turbomachine
WO2017017378A1 (fr) * 2015-07-30 2017-02-02 Safran Aircraft Engines Systeme d'antigivrage d'une aube de turbomachine.
US10683805B2 (en) 2015-07-30 2020-06-16 Safran Aircraft Engines Anti-icing system for a turbine engine vane
US10794281B2 (en) 2016-02-02 2020-10-06 General Electric Company Gas turbine engine having instrumented airflow path components
EP3225813A1 (fr) * 2016-03-30 2017-10-04 General Electric Company Ensemble de passage de flux d'air à soupape permettant de régler la distorsion de flux d'air dans un moteur à turbine à gaz
US20170284304A1 (en) * 2016-03-30 2017-10-05 General Electric Company Valved airflow passage assembly for adjusting airflow distortion in gas turbine engine
JP2017180456A (ja) * 2016-03-30 2017-10-05 ゼネラル・エレクトリック・カンパニイ ガスタービンエンジンにおける気流歪曲を調整するためのバルブ付き空気流通路アセンブリ
CN107269392A (zh) * 2016-03-30 2017-10-20 通用电气公司 用于调整燃气涡轮发动机中气流畸变的阀式气流通道组件
CN107269392B (zh) * 2016-03-30 2020-04-21 通用电气公司 用于调整燃气涡轮发动机中气流畸变的阀式气流通道组件
US10753278B2 (en) 2016-03-30 2020-08-25 General Electric Company Translating inlet for adjusting airflow distortion in gas turbine engine
US11073090B2 (en) * 2016-03-30 2021-07-27 General Electric Company Valved airflow passage assembly for adjusting airflow distortion in gas turbine engine
US11448127B2 (en) 2016-03-30 2022-09-20 General Electric Company Translating inlet for adjusting airflow distortion in gas turbine engine

Also Published As

Publication number Publication date
FR1192929A (fr) 1959-10-29

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