PL3951157T3 - Silnik rakietowy oraz jego części składowe - Google Patents

Silnik rakietowy oraz jego części składowe

Info

Publication number
PL3951157T3
PL3951157T3 PL21189573.5T PL21189573T PL3951157T3 PL 3951157 T3 PL3951157 T3 PL 3951157T3 PL 21189573 T PL21189573 T PL 21189573T PL 3951157 T3 PL3951157 T3 PL 3951157T3
Authority
PL
Poland
Prior art keywords
components
rocket engine
rocket
engine
Prior art date
Application number
PL21189573.5T
Other languages
English (en)
Inventor
Stefan Johannes POWELL
Tobias René KNOP
James Robert Powell
Robert Mark WERNER
Jeroen WINK
Original Assignee
Dawn Aerospace Limited
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
Family has litigation
First worldwide family litigation filed litigation Critical https://patents.darts-ip.com/?family=77207082&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=PL3951157(T3) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Application filed by Dawn Aerospace Limited filed Critical Dawn Aerospace Limited
Publication of PL3951157T3 publication Critical patent/PL3951157T3/pl

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
    • F02K9/44—Feeding propellants
    • F02K9/52—Injectors
    • 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
    • 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
    • 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
    • F02K9/50—Feeding propellants using pressurised fluid to pressurise the 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
    • F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
    • F02K9/44—Feeding propellants
    • F02K9/56—Control
    • 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
    • F02K9/56—Control
    • F02K9/58—Propellant feed 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
    • F02K9/60—Constructional parts; Details not otherwise provided for
    • F02K9/62—Combustion or thrust chambers
    • F02K9/64—Combustion or thrust chambers having cooling 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
    • F05D2270/00—Control
    • F05D2270/30—Control parameters, e.g. input parameters
    • F05D2270/306—Mass flow

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Testing Of Engines (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)
  • Toys (AREA)
PL21189573.5T 2020-08-06 2021-08-04 Silnik rakietowy oraz jego części składowe PL3951157T3 (pl)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US202063061959P 2020-08-06 2020-08-06

Publications (1)

Publication Number Publication Date
PL3951157T3 true PL3951157T3 (pl) 2025-06-16

Family

ID=77207082

Family Applications (1)

Application Number Title Priority Date Filing Date
PL21189573.5T PL3951157T3 (pl) 2020-08-06 2021-08-04 Silnik rakietowy oraz jego części składowe

Country Status (6)

Country Link
US (2) US12116958B2 (pl)
EP (2) EP3951157B1 (pl)
AU (1) AU2021211979A1 (pl)
ES (1) ES3017607T3 (pl)
FI (1) FI3951157T3 (pl)
PL (1) PL3951157T3 (pl)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
IT202200020457A1 (it) * 2022-10-05 2024-04-05 D Orbit S P A Propulsore per manovre orbitali, sistema propulsivo per manovre orbitali e veicolo di trasporto orbitale
CN115680943B (zh) * 2022-10-31 2024-07-30 北京航天试验技术研究所 火箭发动机热辐射测量装置

Family Cites Families (44)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2719584A (en) * 1953-03-05 1955-10-04 Elizabeth L Winslow Nozzle for rocket motor
US3001365A (en) * 1957-05-27 1961-09-26 Aerojet General Co Shut-off valve
US3094838A (en) * 1959-06-17 1963-06-25 United Aircraft Corp Thrust control system
US3088406A (en) * 1959-06-22 1963-05-07 Thompson Ramo Wooldridge Inc Quantized impulse rocket
US3172254A (en) * 1961-04-17 1965-03-09 Chandler Evans Corp Propellant control system for a rocket engine
US3453827A (en) * 1962-11-26 1969-07-08 North American Rockwell Injection throttling
US3166900A (en) * 1963-02-01 1965-01-26 United Aircraft Corp Method and apparatus for fluid flow control in two phase aeration systems
BE644309A (pl) 1963-02-25 1900-01-01
US3368353A (en) * 1965-09-30 1968-02-13 United Aircraft Corp Automatic o/f control
US3581495A (en) * 1968-05-01 1971-06-01 United Aircraft Corp Slot tube swirler injector
US3848806A (en) 1973-04-30 1974-11-19 Rockwell International Corp Throttling venturi valve
US4424679A (en) * 1981-09-10 1984-01-10 The United States Of America As Represented By The Secretary Of The Air Force Constant thrust hybrid rocket motor
US4782660A (en) * 1987-01-20 1988-11-08 Rockwell International Corporation Sequenced and pressure controlled injector
US5063734A (en) * 1990-01-26 1991-11-12 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Method for providing real-time control of a gaseous propellant rocket propulsion system
US5148674A (en) * 1990-01-26 1992-09-22 Morris Brian G Method and apparatus for providing real-time control of a gaseous propellant rocket propulsion system
US5819526A (en) * 1996-02-23 1998-10-13 Trw Inc. Low power arcjet propellant feed system
US6193187B1 (en) * 1998-12-31 2001-02-27 Harry Scott Payload carry and launch system
US6250602B1 (en) 1999-01-18 2001-06-26 Jansen's Aircraft Systems Controls, Inc. Positive shut-off metering valve with axial thread drive
US6205770B1 (en) * 1999-03-10 2001-03-27 Gregg G. Williams Rocket engine
US6783108B2 (en) 2001-08-17 2004-08-31 Jansen's Aircraft Systems Controls, Inc. Fueldraulic pintle valve
JP3783040B2 (ja) * 2002-07-11 2006-06-07 独立行政法人 宇宙航空研究開発機構 ２液式エンジンおよび２液式エンジンを搭載したロケット
US6799417B2 (en) * 2003-02-05 2004-10-05 Aerojet-General Corporation Diversion of combustion gas within a rocket engine to preheat fuel
US6832471B2 (en) * 2003-03-12 2004-12-21 Aerojet-General Corporation Expander cycle rocket engine with staged combustion and heat exchange
US7757476B2 (en) * 2003-07-22 2010-07-20 The Aerospace Corporation Catalytically activated transient decomposition propulsion system
US20080016846A1 (en) * 2006-07-18 2008-01-24 United Technologies Corporation System and method for cooling hydrocarbon-fueled rocket engines
US20100257839A1 (en) * 2006-08-15 2010-10-14 United Technologies Corporation Hydrocarbon-fueled rocket engine with endothermic fuel cooling
US7784269B1 (en) * 2006-08-25 2010-08-31 Xcor Aerospace System and method for cooling rocket engines
US20080264035A1 (en) * 2007-04-25 2008-10-30 Ricciardo Mark J Coolant flow swirler for a rocket engine
US20090288390A1 (en) * 2008-05-23 2009-11-26 Thomas Clayton Pavia Simplified thrust chamber recirculating cooling system
US8438930B2 (en) * 2009-01-08 2013-05-14 United Launch Alliance, Llc Mechanical signal processing accumulator attenuation device and method
US8381508B2 (en) * 2009-05-28 2013-02-26 Alliant Techsystems Inc. Closed-cycle rocket engine assemblies and methods of operating such rocket engine assemblies
CN101644627B (zh) 2009-09-11 2011-05-04 北京航空航天大学 音速喷嘴自动标定系统及自动标定方法
US8572948B1 (en) * 2010-10-15 2013-11-05 Florida Turbine Technologies, Inc. Rocket engine propulsion system
WO2013105988A2 (en) * 2011-02-15 2013-07-18 Firestar Engineering, Llc Clustered, fixed cant, throttleable rocket assembly
US8250853B1 (en) * 2011-02-16 2012-08-28 Florida Turbine Technologies, Inc. Hybrid expander cycle rocket engine
KR101180430B1 (ko) * 2011-08-24 2012-09-07 한국항공우주연구원 Ｄｃ 모터를 이용한 유량제어 밸브의 다단제어 방법
FR2994587B1 (fr) * 2012-08-20 2017-07-07 Snecma Allumeur bimodal et procede d'injection bimodale pour allumeur de moteur-fusee
CN103089488A (zh) 2013-01-21 2013-05-08 北京航空航天大学 一种适用于高浓度过氧化氢的可调汽蚀文氏管
US10940961B2 (en) 2015-01-14 2021-03-09 Ventions, Llc Small satellite propulsion system
US10072612B2 (en) * 2015-10-05 2018-09-11 Vector Launch Inc. Enhanced liquid oxygen-propylene rocket engine
US20180171933A1 (en) * 2016-12-19 2018-06-21 Flight Works, Inc. Micropump-fed autogenous pressurization system
DE102018114868B4 (de) 2018-06-20 2026-01-15 Deutsches Zentrum für Luft- und Raumfahrt e.V. Antriebssystem für ein Raumfahrzeug und Verfahren zum Antrieb eines Raumfahrzeugs
US12060853B2 (en) * 2019-01-30 2024-08-13 Laboratoire Reaction Dynamics Inc. Rocket engine with integrated oxidizer catalyst in manifold and injector assembly
EP4350138B1 (en) * 2020-09-30 2026-04-22 Rolls-Royce plc Complex cycle gas turbine engine

Also Published As

Publication number Publication date
US12116958B2 (en) 2024-10-15
EP3951157A1 (en) 2022-02-09
EP3951157B1 (en) 2025-02-26
ES3017607T3 (en) 2025-05-13
EP4520950A3 (en) 2025-05-07
US20260078719A1 (en) 2026-03-19
FI3951157T3 (fi) 2025-05-22
US20220112867A1 (en) 2022-04-14
EP4520950A2 (en) 2025-03-12
AU2021211979A1 (en) 2022-02-24

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