GB201318110D0 - Mounting Assembly - Google Patents

Mounting Assembly

Info

Publication number
GB201318110D0
GB201318110D0 GB201318110A GB201318110A GB201318110D0 GB 201318110 D0 GB201318110 D0 GB 201318110D0 GB 201318110 A GB201318110 A GB 201318110A GB 201318110 A GB201318110 A GB 201318110A GB 201318110 D0 GB201318110 D0 GB 201318110D0
Authority
GB
United Kingdom
Prior art keywords
mounting assembly
mounting
assembly
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Withdrawn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
GB201318110A
Other versions
GB2519154A (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.)
Reaction Engines Ltd
Original Assignee
Reaction Engines Ltd
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 Reaction Engines Ltd filed Critical Reaction Engines Ltd
Priority to GB1318110.2A priority Critical patent/GB2519154A/en
Publication of GB201318110D0 publication Critical patent/GB201318110D0/en
Priority to US14/296,618 priority patent/US20150102129A1/en
Priority to EP14784337.9A priority patent/EP3055545A1/en
Priority to PCT/GB2014/000406 priority patent/WO2015052470A1/en
Publication of GB2519154A publication Critical patent/GB2519154A/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Withdrawn legal-status Critical Current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
    • F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/80—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control
    • F02K9/84—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control using movable nozzles
    • 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
    • F02K9/97—Rocket nozzles
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00—Geometry
    • F05D2250/60—Structure; Surface texture
    • F05D2250/61—Structure; Surface texture corrugated
    • F05D2250/611—Structure; Surface texture corrugated undulated
GB1318110.2A 2013-10-11 2013-10-11 Mounting Assembly Withdrawn GB2519154A (en)

Priority Applications (4)

Application Number Priority Date Filing Date Title
GB1318110.2A GB2519154A (en) 2013-10-11 2013-10-11 Mounting Assembly
US14/296,618 US20150102129A1 (en) 2013-10-11 2014-06-05 Mounting assembly
EP14784337.9A EP3055545A1 (en) 2013-10-11 2014-10-10 Mounting assembly for a rocket nozzle
PCT/GB2014/000406 WO2015052470A1 (en) 2013-10-11 2014-10-10 Mounting assembly for a rocket nozzle

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1318110.2A GB2519154A (en) 2013-10-11 2013-10-11 Mounting Assembly

Publications (2)

Publication Number Publication Date
GB201318110D0 true GB201318110D0 (en) 2013-11-27
GB2519154A GB2519154A (en) 2015-04-15

Family

ID=49679977

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1318110.2A Withdrawn GB2519154A (en) 2013-10-11 2013-10-11 Mounting Assembly

Country Status (1)

Country Link
GB (1) GB2519154A (en)

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3179447A (en) * 1960-06-27 1965-04-20 Fairchild Camera Instr Co Limited movement hinge connection
US3258915A (en) * 1962-07-09 1966-07-05 Thiokol Chemical Corp Control system
US3392918A (en) * 1962-07-09 1968-07-16 Thiokol Chemical Corp Rocket motor thrust control system
US3270505A (en) * 1964-10-21 1966-09-06 Norman L Crabill Control system for rocket vehicles
RU2159352C2 (en) * 1999-01-21 2000-11-20 Открытое акционерное общество "НПО Энергомаш им. акад. В.П. Глушко" Chamber swinging unit of reheat liquid propellant rocket engine
US7216476B2 (en) * 2003-12-09 2007-05-15 The Boeing Company Two-axis thrust vectoring nozzle
US8696033B2 (en) * 2011-07-15 2014-04-15 Aerojet Rocketdyne Of De, Inc. Scissor duct flex joint damper

Also Published As

Publication number Publication date
GB2519154A (en) 2015-04-15

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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)