GB2468515B - Clean aerospace engine - Google Patents

Clean aerospace engine

Info

Publication number
GB2468515B
GB2468515B GB0904255A GB0904255A GB2468515B GB 2468515 B GB2468515 B GB 2468515B GB 0904255 A GB0904255 A GB 0904255A GB 0904255 A GB0904255 A GB 0904255A GB 2468515 B GB2468515 B GB 2468515B
Authority
GB
United Kingdom
Prior art keywords
clean
aerospace engine
aerospace
engine
clean aerospace
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 - Fee Related
Application number
GB0904255A
Other versions
GB2468515A (en
GB0904255D0 (en
Inventor
Salahuddin Rasheedsedqi Saeed
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to GB0904255A priority Critical patent/GB2468515B/en
Publication of GB0904255D0 publication Critical patent/GB0904255D0/en
Publication of GB2468515A publication Critical patent/GB2468515A/en
Application granted granted Critical
Publication of GB2468515B publication Critical patent/GB2468515B/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • F02K7/02—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 the jet being intermittent, i.e. pulse-jet
    • F02K7/04—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 the jet being intermittent, i.e. pulse-jet with resonant combustion chambers
    • 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
    • F02K7/02—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 the jet being intermittent, i.e. pulse-jet
    • F02K7/06—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 the jet being intermittent, i.e. pulse-jet with combustion chambers having valves
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
    • F02K9/44—Feeding propellants
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R7/00—Intermittent or explosive combustion chambers

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Output Control And Ontrol Of Special Type Engine (AREA)
GB0904255A 2009-03-09 2009-03-09 Clean aerospace engine Expired - Fee Related GB2468515B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB0904255A GB2468515B (en) 2009-03-09 2009-03-09 Clean aerospace engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB0904255A GB2468515B (en) 2009-03-09 2009-03-09 Clean aerospace engine

Publications (3)

Publication Number Publication Date
GB0904255D0 GB0904255D0 (en) 2009-04-22
GB2468515A GB2468515A (en) 2010-09-15
GB2468515B true GB2468515B (en) 2011-02-02

Family

ID=40600920

Family Applications (1)

Application Number Title Priority Date Filing Date
GB0904255A Expired - Fee Related GB2468515B (en) 2009-03-09 2009-03-09 Clean aerospace engine

Country Status (1)

Country Link
GB (1) GB2468515B (en)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2991300B1 (en) * 2012-06-05 2014-07-11 Snecma SPACE ENGINE EQUIPPED WITH A DESORBITATION DEVICE COMPRISING A DETONATION ENGINE
WO2014114980A2 (en) * 2012-10-12 2014-07-31 King Abdullah University Of Science And Technology Standing detonation wave engine
US11149954B2 (en) 2017-10-27 2021-10-19 General Electric Company Multi-can annular rotating detonation combustor
PL244568B1 (en) * 2021-12-16 2024-02-12 Siec Badawcza Lukasiewicz Inst Lotnictwa Rocket engine with multi-stage combustion of a mixture of propellants

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1210601A (en) * 1967-02-11 1970-10-28 Mtu Muenchen Gmbh Rocket propulsion system
GB2223809A (en) * 1988-09-13 1990-04-18 Mitsubishi Heavy Ind Ltd Rocket engine
US5551230A (en) * 1994-03-14 1996-09-03 Rockwell International Corporation Heat induced high pressure lox pump rocket engine cycle

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1210601A (en) * 1967-02-11 1970-10-28 Mtu Muenchen Gmbh Rocket propulsion system
GB2223809A (en) * 1988-09-13 1990-04-18 Mitsubishi Heavy Ind Ltd Rocket engine
US5551230A (en) * 1994-03-14 1996-09-03 Rockwell International Corporation Heat induced high pressure lox pump rocket engine cycle

Also Published As

Publication number Publication date
GB2468515A (en) 2010-09-15
GB0904255D0 (en) 2009-04-22

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Legal Events

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

Effective date: 20130309