GB2612455B - Thrust transfer apparatus for ignition test of solid rocket engine in form of rear skirt connection - Google Patents

Thrust transfer apparatus for ignition test of solid rocket engine in form of rear skirt connection Download PDF

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Publication number
GB2612455B
GB2612455B GB2216941.1A GB202216941A GB2612455B GB 2612455 B GB2612455 B GB 2612455B GB 202216941 A GB202216941 A GB 202216941A GB 2612455 B GB2612455 B GB 2612455B
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GB
United Kingdom
Prior art keywords
transfer apparatus
rocket engine
solid rocket
rear skirt
ignition test
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.)
Active
Application number
GB2216941.1A
Other versions
GB202216941D0 (en
GB2612455A (en
Inventor
Liu Chang
Wang Zhe
Song Feifei
Li Xianjun
Zhu Ziwen
Gao Yonggang
Zhu Yao
Cui Yujie
Sun Jianhong
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.)
Xian Aerospace Propulsion Testing Tech Research Institute
Original Assignee
Xian Aerospace Propulsion Testing Tech Research Institute
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 Xian Aerospace Propulsion Testing Tech Research Institute filed Critical Xian Aerospace Propulsion Testing Tech Research Institute
Publication of GB202216941D0 publication Critical patent/GB202216941D0/en
Publication of GB2612455A publication Critical patent/GB2612455A/en
Application granted granted Critical
Publication of GB2612455B publication Critical patent/GB2612455B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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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
    • F02K9/08—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants
    • 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
    • F02K9/95—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by starting or ignition means or arrangements
    • 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
    • F02K9/96—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by specially adapted arrangements for testing or measuring
    • 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
    • F05D2260/00—Function
    • F05D2260/83—Testing, e.g. methods, components or tools therefor

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Testing Of Engines (AREA)
GB2216941.1A 2020-10-04 2021-09-25 Thrust transfer apparatus for ignition test of solid rocket engine in form of rear skirt connection Active GB2612455B (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
CN202011066998.7A CN112012853B (en) 2020-10-04 2020-10-04 Solid rocket engine of back skirt connection form thrust transmission device for ignition test
PCT/CN2021/120509 WO2022068703A1 (en) 2020-10-04 2021-09-25 Thrust transfer apparatus for ignition test of solid rocket engine in form of rear skirt connection

Publications (3)

Publication Number Publication Date
GB202216941D0 GB202216941D0 (en) 2022-12-28
GB2612455A GB2612455A (en) 2023-05-03
GB2612455B true GB2612455B (en) 2024-06-19

Family

ID=73528116

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2216941.1A Active GB2612455B (en) 2020-10-04 2021-09-25 Thrust transfer apparatus for ignition test of solid rocket engine in form of rear skirt connection

Country Status (3)

Country Link
CN (1) CN112012853B (en)
GB (1) GB2612455B (en)
WO (1) WO2022068703A1 (en)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112012853B (en) * 2020-10-04 2021-07-06 西安航天动力测控技术研究所 Solid rocket engine of back skirt connection form thrust transmission device for ignition test
CN113638822B (en) * 2021-06-30 2023-12-29 西安航天动力测控技术研究所 Mechanical arm type interstage separation test device for rear skirt connection of solid rocket engine
CN114184386B (en) * 2021-11-29 2023-07-21 西安航天动力测控技术研究所 Spherical solid rocket engine testing device
CN114135421B (en) * 2021-11-29 2024-05-17 西安航天动力测控技术研究所 Solid rocket engine head separation test device
CN114104489B (en) * 2021-12-16 2024-06-25 上海空间推进研究所 Liquid rocket engine packing case
CN114199574A (en) * 2021-12-24 2022-03-18 内蒙航天动力机械测试所 Solid rocket engine integration test tool
CN114856867B (en) * 2022-05-27 2024-02-06 哈尔滨工程大学 Active vibration damper of solid rocket engine
CN115184028B (en) * 2022-08-25 2023-09-01 芜湖中科飞机制造有限公司 Fixing device for aeroengine detection
CN117685134B (en) * 2023-11-24 2024-05-17 北京航天试验技术研究所 Supporting device, vertical injection system and installation method of vertical injection system

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6032545A (en) * 1998-04-17 2000-03-07 California Polytechnic State University Foundation Nozzle flow thrust vector measurement
CN102818671A (en) * 2012-08-16 2012-12-12 北京航空航天大学 High-precision liquid or gas rocket engine thrust rack
CN103115716A (en) * 2013-01-25 2013-05-22 南京理工大学 Thrust block device of six-component test stand
CN104019994A (en) * 2014-04-24 2014-09-03 北京理工大学 Overload testing device and method of solid rocket engine
CN107100761A (en) * 2017-06-29 2017-08-29 湖北三江航天江河化工科技有限公司 A kind of test engine
CN108590889A (en) * 2018-05-09 2018-09-28 北京理工大学 A kind of larynx hydrant change propulsive solid propellant rocket ground test device
CN112012853A (en) * 2020-10-04 2020-12-01 西安航天动力测控技术研究所 Solid rocket engine of back skirt connection form thrust transmission device for ignition test

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9140215B2 (en) * 2012-03-14 2015-09-22 Aerojet Rocketoyne Of De, Inc. Rocket engine pressure sense line
CN205785819U (en) * 2016-05-24 2016-12-07 华中科技大学 A kind of test device for rocket engine ground firing

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6032545A (en) * 1998-04-17 2000-03-07 California Polytechnic State University Foundation Nozzle flow thrust vector measurement
CN102818671A (en) * 2012-08-16 2012-12-12 北京航空航天大学 High-precision liquid or gas rocket engine thrust rack
CN103115716A (en) * 2013-01-25 2013-05-22 南京理工大学 Thrust block device of six-component test stand
CN104019994A (en) * 2014-04-24 2014-09-03 北京理工大学 Overload testing device and method of solid rocket engine
CN107100761A (en) * 2017-06-29 2017-08-29 湖北三江航天江河化工科技有限公司 A kind of test engine
CN108590889A (en) * 2018-05-09 2018-09-28 北京理工大学 A kind of larynx hydrant change propulsive solid propellant rocket ground test device
CN112012853A (en) * 2020-10-04 2020-12-01 西安航天动力测控技术研究所 Solid rocket engine of back skirt connection form thrust transmission device for ignition test

Also Published As

Publication number Publication date
CN112012853B (en) 2021-07-06
GB202216941D0 (en) 2022-12-28
CN112012853A (en) 2020-12-01
GB2612455A (en) 2023-05-03
WO2022068703A1 (en) 2022-04-07

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