FR2995017B1 - Dispositif electrothermique pour systeme de propulsion, notamment pour turboreacteur, systeme de propulsion comprenant un tel dispositif electrothermique, et procede associe. - Google Patents

Dispositif electrothermique pour systeme de propulsion, notamment pour turboreacteur, systeme de propulsion comprenant un tel dispositif electrothermique, et procede associe.

Info

Publication number
FR2995017B1
FR2995017B1 FR1258040A FR1258040A FR2995017B1 FR 2995017 B1 FR2995017 B1 FR 2995017B1 FR 1258040 A FR1258040 A FR 1258040A FR 1258040 A FR1258040 A FR 1258040A FR 2995017 B1 FR2995017 B1 FR 2995017B1
Authority
FR
France
Prior art keywords
propulsion system
turbojet engine
associated method
electrothermic
electrothermal
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 - Fee Related
Application number
FR1258040A
Other languages
English (en)
Other versions
FR2995017A1 (fr
Inventor
Xavier Morin
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to FR1258040A priority Critical patent/FR2995017B1/fr
Priority to PCT/EP2013/067637 priority patent/WO2014033091A1/fr
Priority to US14/423,837 priority patent/US10047732B2/en
Priority to EP13756388.8A priority patent/EP2890887A1/fr
Publication of FR2995017A1 publication Critical patent/FR2995017A1/fr
Application granted granted Critical
Publication of FR2995017B1 publication Critical patent/FR2995017B1/fr
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/40—Arrangements or adaptations of propulsion systems
    • B64G1/411—Electric propulsion
    • B64G1/415—Arcjets or resistojets
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03H—PRODUCING A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03H1/00—Using plasma to produce a reactive propulsive thrust
    • F03H1/0093—Electro-thermal plasma thrusters, i.e. thrusters heating the particles in a plasma
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C1/00—Gas-turbine plants characterised by the use of hot gases or unheated pressurised gases, as the working fluid
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K99/00—Subject matter not provided for in other groups of this subclass
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03H—PRODUCING A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03H1/00—Using plasma to produce a reactive propulsive thrust
    • F03H1/0006—Details applicable to different types of plasma thrusters
    • F03H1/0012—Means for supplying the propellant
    • 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
    • F05D2220/00—Application
    • F05D2220/30—Application in turbines
    • F05D2220/32—Application in turbines in gas turbines
    • F05D2220/323—Application in turbines in gas turbines for aircraft propulsion, e.g. jet engines

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Plasma & Fusion (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
FR1258040A 2012-08-28 2012-08-28 Dispositif electrothermique pour systeme de propulsion, notamment pour turboreacteur, systeme de propulsion comprenant un tel dispositif electrothermique, et procede associe. Expired - Fee Related FR2995017B1 (fr)

Priority Applications (4)

Application Number Priority Date Filing Date Title
FR1258040A FR2995017B1 (fr) 2012-08-28 2012-08-28 Dispositif electrothermique pour systeme de propulsion, notamment pour turboreacteur, systeme de propulsion comprenant un tel dispositif electrothermique, et procede associe.
PCT/EP2013/067637 WO2014033091A1 (fr) 2012-08-28 2013-08-26 Dispositif électrothermique pour système de propulsion, notamment pour turboréacteur, système de propulsion comprenant un tel dispositif électrothermique, et procédé associé
US14/423,837 US10047732B2 (en) 2012-08-28 2013-08-26 Electrothermal device for a propulsion system, especially for a turbojet, propulsion system comprising such an electrothermal device, and associated method
EP13756388.8A EP2890887A1 (fr) 2012-08-28 2013-08-26 Dispositif électrothermique pour système de propulsion, notamment pour turboréacteur, système de propulsion comprenant un tel dispositif électrothermique, et procédé associé

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1258040A FR2995017B1 (fr) 2012-08-28 2012-08-28 Dispositif electrothermique pour systeme de propulsion, notamment pour turboreacteur, systeme de propulsion comprenant un tel dispositif electrothermique, et procede associe.

Publications (2)

Publication Number Publication Date
FR2995017A1 FR2995017A1 (fr) 2014-03-07
FR2995017B1 true FR2995017B1 (fr) 2017-09-01

Family

ID=47003133

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1258040A Expired - Fee Related FR2995017B1 (fr) 2012-08-28 2012-08-28 Dispositif electrothermique pour systeme de propulsion, notamment pour turboreacteur, systeme de propulsion comprenant un tel dispositif electrothermique, et procede associe.

Country Status (4)

Country Link
US (1) US10047732B2 (fr)
EP (1) EP2890887A1 (fr)
FR (1) FR2995017B1 (fr)
WO (1) WO2014033091A1 (fr)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10559864B2 (en) 2014-02-13 2020-02-11 Birmingham Technologies, Inc. Nanofluid contact potential difference battery
FR3018315A1 (fr) * 2014-03-07 2015-09-11 Elwing Europ S A Dispositif electrothermique de generation d'energie mecanique optimise, et systeme de propulsion associe
FR3018311A1 (fr) * 2014-03-07 2015-09-11 Elwing Europ S A Dispositif electrothermique de generation d'energie mecanique thermiquement optimise, et systeme de propulsion associe
FR3026281B1 (fr) 2014-09-25 2018-08-24 L'oreal Organe d'application comportant deux parties assemblees.
US11493066B2 (en) * 2016-01-20 2022-11-08 Soliton Holdings Generalized jet-effect and enhanced devices
CN110318963B (zh) * 2019-07-08 2020-07-17 哈尔滨工业大学 一种基于热节流阀的工质流量供给量调节装置
FR3101383B1 (fr) * 2019-09-26 2023-06-09 Tarek Romain Imtital Propulseur électrothermique à double-flux
US11649525B2 (en) 2020-05-01 2023-05-16 Birmingham Technologies, Inc. Single electron transistor (SET), circuit containing set and energy harvesting device, and fabrication method
US11713140B2 (en) * 2020-06-11 2023-08-01 The Aerospace Corporation Lithium ion battery de-orbiter
US11417506B1 (en) 2020-10-15 2022-08-16 Birmingham Technologies, Inc. Apparatus including thermal energy harvesting thermionic device integrated with electronics, and related systems and methods
US11616186B1 (en) 2021-06-28 2023-03-28 Birmingham Technologies, Inc. Thermal-transfer apparatus including thermionic devices, and related methods
US20240278939A1 (en) * 2023-02-20 2024-08-22 Eagle Technology, Llc Satellite propulsion system including combustion chamber and electrical arc heater and related methods

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3071705A (en) * 1958-10-06 1963-01-01 Grumman Aircraft Engineering C Electrostatic propulsion means
GB897577A (en) * 1959-07-15 1962-05-30 Bristol Siddeley Engines Ltd Improvements in or relating to apparatus for producing a jet consisting of a plasma of ions and electrons
US3593525A (en) * 1969-02-19 1971-07-20 Us Army Rocket motor thrust controller
US4577461A (en) * 1983-06-22 1986-03-25 Cann Gordon L Spacecraft optimized arc rocket
US4882465A (en) * 1987-10-01 1989-11-21 Olin Corporation Arcjet thruster with improved arc attachment for enhancement of efficiency
GB2241746A (en) * 1990-03-03 1991-09-11 Whittaker D G M Method of energising a working fluid and deriving useful work.
US6145298A (en) * 1997-05-06 2000-11-14 Sky Station International, Inc. Atmospheric fueled ion engine
US6357700B1 (en) * 2000-10-02 2002-03-19 Anthony Italo Provitola Electrically powered spacecraft/airship
US6834492B2 (en) * 2001-06-21 2004-12-28 Busek Company, Inc. Air breathing electrically powered hall effect thruster

Also Published As

Publication number Publication date
EP2890887A1 (fr) 2015-07-08
US10047732B2 (en) 2018-08-14
US20150211499A1 (en) 2015-07-30
WO2014033091A1 (fr) 2014-03-06
FR2995017A1 (fr) 2014-03-07

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