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GB0602140D0 - The supersonic turbofan 1 - Google Patents

The supersonic turbofan 1

Info

Publication number
GB0602140D0
GB0602140D0 GBGB0602140.6A GB0602140A GB0602140D0 GB 0602140 D0 GB0602140 D0 GB 0602140D0 GB 0602140 A GB0602140 A GB 0602140A GB 0602140 D0 GB0602140 D0 GB 0602140D0
Authority
GB
United Kingdom
Prior art keywords
turbofan
supersonic
supersonic turbofan
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.)
Ceased
Application number
GBGB0602140.6A
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.)
LEWIS STEPHEN D
Original Assignee
LEWIS STEPHEN D
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 LEWIS STEPHEN D filed Critical LEWIS STEPHEN D
Priority to GBGB0602140.6A priority Critical patent/GB0602140D0/en
Publication of GB0602140D0 publication Critical patent/GB0602140D0/en
Priority to GB0605939A priority patent/GB2434838A/en
Ceased 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
    • F02K3/105—Heating the by-pass flow
    • F02K3/11—Heating the by-pass flow by means of burners or combustion chambers

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)
GBGB0602140.6A 2006-02-03 2006-02-03 The supersonic turbofan 1 Ceased GB0602140D0 (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
GBGB0602140.6A GB0602140D0 (en) 2006-02-03 2006-02-03 The supersonic turbofan 1
GB0605939A GB2434838A (en) 2006-02-03 2006-03-24 Supersonic turbofan engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GBGB0602140.6A GB0602140D0 (en) 2006-02-03 2006-02-03 The supersonic turbofan 1

Publications (1)

Publication Number Publication Date
GB0602140D0 true GB0602140D0 (en) 2006-03-15

Family

ID=36100945

Family Applications (2)

Application Number Title Priority Date Filing Date
GBGB0602140.6A Ceased GB0602140D0 (en) 2006-02-03 2006-02-03 The supersonic turbofan 1
GB0605939A Withdrawn GB2434838A (en) 2006-02-03 2006-03-24 Supersonic turbofan engine

Family Applications After (1)

Application Number Title Priority Date Filing Date
GB0605939A Withdrawn GB2434838A (en) 2006-02-03 2006-03-24 Supersonic turbofan engine

Country Status (1)

Country Link
GB (2) GB0602140D0 (en)

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3677012A (en) * 1962-05-31 1972-07-18 Gen Electric Composite cycle turbomachinery
GB1008322A (en) * 1964-08-04 1965-10-27 Rolls Royce Gas turbine engine
US4137708A (en) * 1973-07-02 1979-02-06 General Motors Corporation Jet propulsion
GB1503425A (en) * 1976-08-04 1978-03-08 Hallowell E Gas turbine ducted fan jet engines for supersonic flight
GB2118248A (en) * 1982-03-23 1983-10-26 Rolls Royce Double flow path gas turbine engine
US5311735A (en) * 1993-05-10 1994-05-17 General Electric Company Ramjet bypass duct and preburner configuration
JP3120113B1 (en) * 1999-11-10 2000-12-25 科学技術庁航空宇宙技術研究所長 Jet engine for high-speed aircraft

Also Published As

Publication number Publication date
GB2434838A (en) 2007-08-08
GB0605939D0 (en) 2006-05-03

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Legal Events

Date Code Title Description
AT Applications terminated before publication under section 16(1)