DE60020740D1 - Elektropumpe mit einem hochfrequenz reluktanzantrieb - Google Patents

Elektropumpe mit einem hochfrequenz reluktanzantrieb

Info

Publication number
DE60020740D1
DE60020740D1 DE60020740T DE60020740T DE60020740D1 DE 60020740 D1 DE60020740 D1 DE 60020740D1 DE 60020740 T DE60020740 T DE 60020740T DE 60020740 T DE60020740 T DE 60020740T DE 60020740 D1 DE60020740 D1 DE 60020740D1
Authority
DE
Germany
Prior art keywords
high frequency
electric pump
fuel
reluctance drive
pressure
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 - Lifetime
Application number
DE60020740T
Other languages
English (en)
Other versions
DE60020740T2 (de
Inventor
Isabelle Gibek
Jean-Claude Vannier
Francois Dugue
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.)
Centre National dEtudes Spatiales CNES
Original Assignee
Centre National dEtudes Spatiales CNES
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 Centre National dEtudes Spatiales CNES filed Critical Centre National dEtudes Spatiales CNES
Publication of DE60020740D1 publication Critical patent/DE60020740D1/de
Application granted granted Critical
Publication of DE60020740T2 publication Critical patent/DE60020740T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime 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
    • F02K9/42—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
    • F02K9/563—Control of propellant feed pumps
    • 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
    • F02K9/46—Feeding propellants using pumps
    • 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
    • F02K9/80—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control
    • F02K9/88—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control using auxiliary rocket nozzles
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04B—POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
    • F04B17/00—Pumps characterised by combination with, or adaptation to, specific driving engines or motors
    • F04B17/03—Pumps characterised by combination with, or adaptation to, specific driving engines or motors driven by electric motors
    • F04B17/04—Pumps characterised by combination with, or adaptation to, specific driving engines or motors driven by electric motors using solenoids
    • F04B17/042—Pumps characterised by combination with, or adaptation to, specific driving engines or motors driven by electric motors using solenoids the solenoid motor being separated from the fluid flow
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04B—POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
    • F04B43/00—Machines, pumps, or pumping installations having flexible working members
    • F04B43/02—Machines, pumps, or pumping installations having flexible working members having plate-like flexible members, e.g. diaphragms
    • F04B43/06—Pumps having fluid drive
    • F04B43/067—Pumps having fluid drive the fluid being actuated directly by a piston
    • 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
    • F05D2270/50—Control logic embodiments
    • F05D2270/54—Control logic embodiments by electronic means, e.g. electronic tubes, transistors or IC's within an electronic circuit
    • 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
    • F05D2270/60—Control system actuates means
    • F05D2270/62—Electrical actuators

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Combustion & Propulsion (AREA)
  • Chemical & Material Sciences (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Electromagnetic Pumps, Or The Like (AREA)
  • Details Of Reciprocating Pumps (AREA)
  • Jet Pumps And Other Pumps (AREA)
  • Fluid-Pressure Circuits (AREA)
  • Filling Or Discharging Of Gas Storage Vessels (AREA)
  • Cooling, Air Intake And Gas Exhaust, And Fuel Tank Arrangements In Propulsion Units (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Valve Device For Special Equipments (AREA)
  • Output Control And Ontrol Of Special Type Engine (AREA)
  • Saccharide Compounds (AREA)
DE60020740T 1999-12-21 2000-12-19 Elektropumpe mit einem hochfrequenz reluktanzantrieb Expired - Lifetime DE60020740T2 (de)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR9916149 1999-12-21
FR9916149A FR2802575B1 (fr) 1999-12-21 1999-12-21 Systeme et procede d'alimentation d'au moins un propulseur, et electropompe a actionneur a reluctance variable haute frequence
PCT/FR2000/003585 WO2001046581A2 (fr) 1999-12-21 2000-12-19 Systeme et procede d'alimentation d'au moins un propulseur, et electropompe a actionneur a reluctance variable haute frequence

Publications (2)

Publication Number Publication Date
DE60020740D1 true DE60020740D1 (de) 2005-07-14
DE60020740T2 DE60020740T2 (de) 2006-05-04

Family

ID=9553547

Family Applications (2)

Application Number Title Priority Date Filing Date
DE60045929T Expired - Lifetime DE60045929D1 (de) 1999-12-21 2000-12-19 Verfahren und System zur Treibstoffzufuhr für mindestens ein Raketentriebwerk
DE60020740T Expired - Lifetime DE60020740T2 (de) 1999-12-21 2000-12-19 Elektropumpe mit einem hochfrequenz reluktanzantrieb

Family Applications Before (1)

Application Number Title Priority Date Filing Date
DE60045929T Expired - Lifetime DE60045929D1 (de) 1999-12-21 2000-12-19 Verfahren und System zur Treibstoffzufuhr für mindestens ein Raketentriebwerk

Country Status (7)

Country Link
EP (2) EP1568877B1 (de)
AT (2) ATE297501T1 (de)
DE (2) DE60045929D1 (de)
ES (2) ES2244493T3 (de)
FR (1) FR2802575B1 (de)
IL (1) IL150283A (de)
WO (1) WO2001046581A2 (de)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6892525B2 (en) * 2003-06-06 2005-05-17 Honeywell International Inc. Micropump-based microthruster
FR2916107B1 (fr) * 2007-05-11 2015-11-27 Centre Nat Etd Spatiales Actionneur alternatif a asservissement en boucle fermee
FR2916103B1 (fr) 2007-05-11 2009-06-26 Cnes Epic Actionneur electromagnetique a reluctance variable
FR2991391B1 (fr) * 2012-05-30 2014-07-04 Snecma Dispositif et procede d'alimentation d'une chambre propulsive de moteur-fusee
RU2651703C1 (ru) * 2016-02-12 2018-04-23 Акционерное общество "Информационные спутниковые системы" имени академика М.Ф. Решетнёва" Блок подачи рабочего тела в реактивный двигатель космического аппарата
DE102017120229B4 (de) 2017-09-03 2019-05-09 Tesat-Spacecom Gmbh & Co.Kg Regleranordnung mit adaptiver Anpassung der Stellgröße
US11155368B1 (en) 2018-03-13 2021-10-26 Space Systems/Loral, Llc Multiple thruster firing on a single articulable module
US11148833B1 (en) 2018-05-21 2021-10-19 Space Systems/Loral, Llc Spacecraft propellant management system
CN110821710B (zh) * 2019-10-28 2020-08-21 西安航天动力试验技术研究所 火箭发动机试验入口压力快速增压装置及液氧供应系统

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3088406A (en) * 1959-06-22 1963-05-07 Thompson Ramo Wooldridge Inc Quantized impulse rocket
US3769879A (en) * 1971-12-09 1973-11-06 A Lofquist Self-compensating diaphragm pump
US4696160A (en) * 1985-05-14 1987-09-29 Trw Inc. Pressure pump and injector valve system for liquid-propellant engines
US5026259A (en) 1990-07-09 1991-06-25 The United States Of America As Represented By The United States Department Of Energy Miniaturized pressurization system

Also Published As

Publication number Publication date
DE60045929D1 (de) 2011-06-16
ATE508271T1 (de) 2011-05-15
EP1568877A3 (de) 2007-06-27
EP1250526B1 (de) 2005-06-08
EP1568877B1 (de) 2011-05-04
IL150283A0 (en) 2002-12-01
EP1568877A2 (de) 2005-08-31
EP1250526A2 (de) 2002-10-23
FR2802575A1 (fr) 2001-06-22
IL150283A (en) 2005-07-25
ATE297501T1 (de) 2005-06-15
ES2244493T3 (es) 2005-12-16
ES2365787T3 (es) 2011-10-11
WO2001046581A2 (fr) 2001-06-28
WO2001046581A3 (fr) 2002-01-17
DE60020740T2 (de) 2006-05-04
FR2802575B1 (fr) 2002-02-08

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Legal Events

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