GB0602141D0 - The turboramjet - Google Patents

The turboramjet

Info

Publication number
GB0602141D0
GB0602141D0 GB0602141A GB0602141A GB0602141D0 GB 0602141 D0 GB0602141 D0 GB 0602141D0 GB 0602141 A GB0602141 A GB 0602141A GB 0602141 A GB0602141 A GB 0602141A GB 0602141 D0 GB0602141 D0 GB 0602141D0
Authority
GB
United Kingdom
Prior art keywords
turboramjet
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.)
Withdrawn
Application number
GB0602141A
Other versions
GB2434839A (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.)
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 GB0602141A priority Critical patent/GB2434839A/en
Publication of GB0602141D0 publication Critical patent/GB0602141D0/en
Publication of GB2434839A publication Critical patent/GB2434839A/en
Withdrawn legal-status Critical Current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
    • F02K7/00—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof
    • F02K7/10—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof characterised by having ram-action compression, i.e. aero-thermo-dynamic-ducts or ram-jet engines
    • F02K7/16—Composite ram-jet/turbo-jet engines
GB0602141A 2006-02-03 2006-02-03 Composite turbo-jet/ram-jet engine Withdrawn GB2434839A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB0602141A GB2434839A (en) 2006-02-03 2006-02-03 Composite turbo-jet/ram-jet engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB0602141A GB2434839A (en) 2006-02-03 2006-02-03 Composite turbo-jet/ram-jet engine

Publications (2)

Publication Number Publication Date
GB0602141D0 true GB0602141D0 (en) 2006-03-15
GB2434839A GB2434839A (en) 2007-08-08

Family

ID=36100946

Family Applications (1)

Application Number Title Priority Date Filing Date
GB0602141A Withdrawn GB2434839A (en) 2006-02-03 2006-02-03 Composite turbo-jet/ram-jet engine

Country Status (1)

Country Link
GB (1) GB2434839A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113279880A (en) * 2021-07-06 2021-08-20 中国航空发动机研究院 Combined cycle aircraft engine

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2696078A (en) * 1952-08-30 1954-12-07 Waitzman Simon Jet propulsion apparatus having a combination ram-jet and turbojet engine
FR2389772A1 (en) * 1977-05-05 1978-12-01 Mordellet Roger Jet engine for subsonic aircraft - has hollow rotor with internal blades to produce secondary stream of air within annular primary stream
US4817892A (en) * 1986-04-28 1989-04-04 Janeke Charl E Aerospace plane and engine therefor

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113279880A (en) * 2021-07-06 2021-08-20 中国航空发动机研究院 Combined cycle aircraft engine

Also Published As

Publication number Publication date
GB2434839A (en) 2007-08-08

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Legal Events

Date Code Title Description
WAP Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1)