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GB2038948B - Gas turbine by-pass jet engines - Google Patents

Gas turbine by-pass jet engines

Info

Publication number
GB2038948B
GB2038948B GB7942014A GB7942014A GB2038948B GB 2038948 B GB2038948 B GB 2038948B GB 7942014 A GB7942014 A GB 7942014A GB 7942014 A GB7942014 A GB 7942014A GB 2038948 B GB2038948 B GB 2038948B
Authority
GB
United Kingdom
Prior art keywords
gas turbine
jet engines
pass jet
pass
engines
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
GB7942014A
Other versions
GB2038948A (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.)
SECR DEFENCE
UK Secretary of State for Defence
Original Assignee
SECR DEFENCE
UK Secretary of State for Defence
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 SECR DEFENCE, UK Secretary of State for Defence filed Critical SECR DEFENCE
Publication of GB2038948A publication Critical patent/GB2038948A/en
Application granted granted Critical
Publication of GB2038948B publication Critical patent/GB2038948B/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
    • F02K3/02—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
    • F02K3/077—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 the plant being of the multiple flow type, i.e. having three or more flows

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
GB7942014A 1978-12-21 1979-12-05 Gas turbine by-pass jet engines Expired GB2038948B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB7849653 1978-12-21

Publications (2)

Publication Number Publication Date
GB2038948A GB2038948A (en) 1980-07-30
GB2038948B true GB2038948B (en) 1982-09-22

Family

ID=10501895

Family Applications (1)

Application Number Title Priority Date Filing Date
GB7942014A Expired GB2038948B (en) 1978-12-21 1979-12-05 Gas turbine by-pass jet engines

Country Status (1)

Country Link
GB (1) GB2038948B (en)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2119859A (en) * 1982-05-06 1983-11-23 Rolls Royce Exhaust mixer for bypass gas turbine aeroengine
FR2645911B1 (en) * 1989-04-18 1991-06-07 Snecma HIGH DILUTION MOTOR WITH UPSTREAM BLOWER AND DOWNSTREAM BLOWER
US7614210B2 (en) * 2006-02-13 2009-11-10 General Electric Company Double bypass turbofan
US8371806B2 (en) * 2007-10-03 2013-02-12 United Technologies Corporation Gas turbine engine having core auxiliary duct passage
RU2424438C1 (en) * 2010-03-17 2011-07-20 Николай Борисович Болотин Turboprop gas turbine engine with nuclear power plant
RU2424441C1 (en) * 2010-03-17 2011-07-20 Николай Борисович Болотин Nuclear turboprop gas turbine engine
RU2425243C1 (en) * 2010-03-23 2011-07-27 Николай Борисович Болотин Nuclear turboprop gas turbine engine
US9279388B2 (en) * 2011-11-01 2016-03-08 United Technologies Corporation Gas turbine engine with two-spool fan and variable vane turbine

Also Published As

Publication number Publication date
GB2038948A (en) 1980-07-30

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Legal Events

Date Code Title Description
PCNP Patent ceased through non-payment of renewal fee