GB8138014D0 - Jet propulsion powerplants - Google Patents

Jet propulsion powerplants

Info

Publication number
GB8138014D0
GB8138014D0 GBGB8138014.9A GB8138014A GB8138014D0 GB 8138014 D0 GB8138014 D0 GB 8138014D0 GB 8138014 A GB8138014 A GB 8138014A GB 8138014 D0 GB8138014 D0 GB 8138014D0
Authority
GB
United Kingdom
Prior art keywords
jet propulsion
powerplants
propulsion powerplants
jet
propulsion
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.)
Pending
Application number
GBGB8138014.9A
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.)
BAE Systems PLC
Original Assignee
British Aerospace 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 British Aerospace PLC filed Critical British Aerospace PLC
Priority to GBGB8138014.9A priority Critical patent/GB8138014D0/en
Priority to GB8233865A priority patent/GB2305976B/en
Priority to IT8249708A priority patent/IT8249708A0/en
Priority to FR8221473A priority patent/FR2747738A1/en
Publication of GB8138014D0 publication Critical patent/GB8138014D0/en
Pending legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K3/00Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/08Plants including a gas turbine driving a compressor or a ducted fan with supplementary heating of the working fluid; Control thereof
    • F02K3/10Plants including a gas turbine driving a compressor or a ducted fan with supplementary heating of the working fluid; Control thereof by after-burners
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K3/00Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/02Plants 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
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K3/00Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/02Plants 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
    • F02K3/04Plants 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
    • F02K3/06Plants 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 with front fan
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K3/00Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/02Plants 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
    • F02K3/04Plants 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
    • F02K3/075Plants 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
GBGB8138014.9A 1981-12-21 1981-12-21 Jet propulsion powerplants Pending GB8138014D0 (en)

Priority Applications (4)

Application Number Priority Date Filing Date Title
GBGB8138014.9A GB8138014D0 (en) 1981-12-21 1981-12-21 Jet propulsion powerplants
GB8233865A GB2305976B (en) 1981-12-21 1982-11-29 Jet propulsion powerplants
IT8249708A IT8249708A0 (en) 1981-12-21 1982-12-20 IMPROVEMENT IN JET ENGINE ENGINE
FR8221473A FR2747738A1 (en) 1981-12-21 1982-12-21 Jet propulsion powerplant, e.g. for aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GBGB8138014.9A GB8138014D0 (en) 1981-12-21 1981-12-21 Jet propulsion powerplants

Publications (1)

Publication Number Publication Date
GB8138014D0 true GB8138014D0 (en) 1996-10-23

Family

ID=10526666

Family Applications (1)

Application Number Title Priority Date Filing Date
GBGB8138014.9A Pending GB8138014D0 (en) 1981-12-21 1981-12-21 Jet propulsion powerplants

Country Status (3)

Country Link
FR (1) FR2747738A1 (en)
GB (1) GB8138014D0 (en)
IT (1) IT8249708A0 (en)

Also Published As

Publication number Publication date
FR2747738A1 (en) 1997-10-24
IT8249708A0 (en) 1982-12-20

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