DE602005000196D1 - Ringförmiges Kühlmittelsammelrohr - Google Patents

Ringförmiges Kühlmittelsammelrohr

Info

Publication number
DE602005000196D1
DE602005000196D1 DE602005000196T DE602005000196T DE602005000196D1 DE 602005000196 D1 DE602005000196 D1 DE 602005000196D1 DE 602005000196 T DE602005000196 T DE 602005000196T DE 602005000196 T DE602005000196 T DE 602005000196T DE 602005000196 D1 DE602005000196 D1 DE 602005000196D1
Authority
DE
Germany
Prior art keywords
collection tube
annular coolant
coolant collection
annular
tube
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
DE602005000196T
Other languages
English (en)
Other versions
DE602005000196T2 (de
Inventor
Jim A Clark
Mark Ricciardo
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.)
Raytheon Technologies Corp
Original Assignee
United Technologies Corp
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 United Technologies Corp filed Critical United Technologies Corp
Publication of DE602005000196D1 publication Critical patent/DE602005000196D1/de
Application granted granted Critical
Publication of DE602005000196T2 publication Critical patent/DE602005000196T2/de
Active 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
    • 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
    • F02K9/60—Constructional parts; Details not otherwise provided for
    • F02K9/62—Combustion or thrust chambers
    • F02K9/64—Combustion or thrust chambers having cooling arrangements

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Testing Of Engines (AREA)
  • Jet Pumps And Other Pumps (AREA)
  • Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)
  • Cooling, Air Intake And Gas Exhaust, And Fuel Tank Arrangements In Propulsion Units (AREA)
DE602005000196T 2004-02-12 2005-02-10 Ringförmiges Kühlmittelsammelrohr Active DE602005000196T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US777435 2004-02-12
US10/777,435 US7373774B2 (en) 2004-02-12 2004-02-12 Enhanced performance torroidal coolant-collection manifold

Publications (2)

Publication Number Publication Date
DE602005000196D1 true DE602005000196D1 (de) 2006-12-07
DE602005000196T2 DE602005000196T2 (de) 2007-02-08

Family

ID=34701379

Family Applications (1)

Application Number Title Priority Date Filing Date
DE602005000196T Active DE602005000196T2 (de) 2004-02-12 2005-02-10 Ringförmiges Kühlmittelsammelrohr

Country Status (5)

Country Link
US (1) US7373774B2 (de)
EP (1) EP1564398B1 (de)
JP (1) JP2005226640A (de)
DE (1) DE602005000196T2 (de)
RU (1) RU2283965C1 (de)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2008010748A1 (en) * 2006-07-19 2008-01-24 Volvo Aero Corporation Method for manufacturing a wall structure
US8904752B2 (en) * 2010-03-12 2014-12-09 Aerojet Rocketdyne Of De, Inc. Injector assembly for a rocket engine
US20120227408A1 (en) * 2011-03-10 2012-09-13 Delavan Inc. Systems and methods of pressure drop control in fluid circuits through swirling flow mitigation
US9194335B2 (en) * 2012-03-09 2015-11-24 Aerojet Rocketdyne Of De, Inc. Rocket engine coolant system including an exit manifold having at least one flow guide within the manifold
DE102016215244A1 (de) 2016-08-16 2018-02-22 Airbus Ds Gmbh Brennkammerstruktur, insbesondere für ein raketentriebwerk
CN109812352A (zh) * 2019-03-06 2019-05-28 中南大学 引射火箭及其热防护结构与热防护方法
CN110282163B (zh) * 2019-07-08 2021-04-02 盐城科宇机械制造有限公司 一种航天用带法兰的集合器

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3001726A (en) * 1959-06-23 1961-09-26 United Aircraft Corp Manifold attachment
US3062566A (en) * 1959-06-25 1962-11-06 United Aircraft Corp Manifold attachment to tubular wall
US4811556A (en) 1986-10-14 1989-03-14 General Electric Company Multiple-propellant air vehicle and propulsion system
JP2809370B2 (ja) 1993-05-19 1998-10-08 科学技術庁航空宇宙技術研究所長 高温燃焼エンジン
US5557928A (en) 1994-08-16 1996-09-24 United Technologies Corporation Tube rocket thrust chamber construction and method
US6688100B1 (en) * 2002-07-16 2004-02-10 The Boeing Company Combustion chamber having a multiple-piece liner and associated assembly method
US6829884B2 (en) * 2002-11-19 2004-12-14 The Boeing Company Rocket engine combustion chamber having multiple conformal throat supports

Also Published As

Publication number Publication date
RU2283965C1 (ru) 2006-09-20
EP1564398A1 (de) 2005-08-17
JP2005226640A (ja) 2005-08-25
DE602005000196T2 (de) 2007-02-08
US7373774B2 (en) 2008-05-20
US20050178106A1 (en) 2005-08-18
EP1564398B1 (de) 2006-10-25

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition