GB712633A - Improvements relating to gas-turbine engines - Google Patents

Improvements relating to gas-turbine engines

Info

Publication number
GB712633A
GB712633A GB18370/51A GB1837051A GB712633A GB 712633 A GB712633 A GB 712633A GB 18370/51 A GB18370/51 A GB 18370/51A GB 1837051 A GB1837051 A GB 1837051A GB 712633 A GB712633 A GB 712633A
Authority
GB
United Kingdom
Prior art keywords
outlet
gas
turbine engines
improvements relating
segments
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
GB18370/51A
Other languages
English (en)
Inventor
Donald Hamilton Mattinson
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.)
Rolls Royce PLC
Original Assignee
Rolls Royce PLC
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 PLC filed Critical Rolls Royce PLC
Priority to GB18370/51A priority Critical patent/GB712633A/en
Priority to US300595A priority patent/US2753685A/en
Priority to FR1066903D priority patent/FR1066903A/fr
Priority to CH304500D priority patent/CH304500A/de
Publication of GB712633A publication Critical patent/GB712633A/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
    • F02K—JET-PROPULSION PLANTS
    • F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/08—Plants including a gas turbine driving a compressor or a ducted fan with supplementary heating of the working fluid; Control thereof
    • F02K3/10—Plants including a gas turbine driving a compressor or a ducted fan with supplementary heating of the working fluid; Control thereof by after-burners
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/06—Varying effective area of jet pipe or nozzle
    • F02K1/15—Control or regulation
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/78—Other construction of jet pipes
    • F02K1/82—Jet pipe walls, e.g. liners
    • F02K1/822—Heat insulating structures or liners, cooling arrangements, e.g. post combustion liners; Infrared radiation suppressors
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
    • F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
    • F02K3/075—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type controlling flow ratio between flows
    • 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)
  • Supercharger (AREA)
GB18370/51A 1951-08-02 1952-07-22 Improvements relating to gas-turbine engines Expired GB712633A (en)

Priority Applications (4)

Application Number Priority Date Filing Date Title
GB18370/51A GB712633A (en) 1952-07-22 1952-07-22 Improvements relating to gas-turbine engines
US300595A US2753685A (en) 1951-08-02 1952-07-24 Gas turbine engine with exhaust gas heating means
FR1066903D FR1066903A (fr) 1952-07-22 1952-07-31 Perfectionnements aux moteurs à turbine à gaz
CH304500D CH304500A (de) 1952-07-22 1952-08-01 Gasturbinenanlage.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB18370/51A GB712633A (en) 1952-07-22 1952-07-22 Improvements relating to gas-turbine engines

Publications (1)

Publication Number Publication Date
GB712633A true GB712633A (en) 1954-07-28

Family

ID=32011990

Family Applications (1)

Application Number Title Priority Date Filing Date
GB18370/51A Expired GB712633A (en) 1951-08-02 1952-07-22 Improvements relating to gas-turbine engines

Country Status (3)

Country Link
CH (1) CH304500A (de)
FR (1) FR1066903A (de)
GB (1) GB712633A (de)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1276969B (de) * 1962-10-30 1968-09-05 Bristol Siddeley Engines Ltd Gasturbinenstrahltriebwerk

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB805418A (en) * 1955-10-05 1958-12-03 Power Jets Res & Dev Ltd Jet propulsion plant
US4064692A (en) * 1975-06-02 1977-12-27 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Variable cycle gas turbine engines
US4142365A (en) * 1976-11-01 1979-03-06 General Electric Company Hybrid mixer for a high bypass ratio gas turbofan engine
FR2713749B1 (fr) * 1993-12-15 1996-01-12 Snecma Chambre de post combustion de turbine à gaz.

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1276969B (de) * 1962-10-30 1968-09-05 Bristol Siddeley Engines Ltd Gasturbinenstrahltriebwerk

Also Published As

Publication number Publication date
CH304500A (de) 1955-01-15
FR1066903A (fr) 1954-06-10

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