ELECTROJET PROPULSION DEVICE AND METHOD FOR MONITORING AND CONTROL OF TEMPERATURE IN ELECTROJET ENGINE WITH MAGNETISATION COILS Russian patent published in 2009 - IPC F03H1/00 H05H1/54 

Abstract RU 2370668 C2

FIELD: transportation.

SUBSTANCE: invention may be used in ground tests and operation of electrojet engines (EJE) of various capacity, for instance Hall plasma engines, and electrojet propulsion devices (EJPD) on their basis. EJPD comprises at least one EJE (1) with magnetisation coils (2), device for conversion and control (3) with controllable source of magnetisation coils power supply (4) and command-telemetric device (5), which sets current level in magnetisation coils (2). Command-telemetric device (5) is equipped with additional device (6) of voltage measurement, which is connected to magnetisation coils. In EJE (1) with magnetisation coils (2) with current fed to magnetisation coils (2), voltage drop in them is measured, EJE (1) temperature is controlled by value of electric resistance in magnetisation coils, identified from ratio of measured voltage drop in them and value of supplied current, and temperature is adjusted by changing of current value in magnetisation coils.

EFFECT: reduced weight and higher reliability of electrojet propulsion device, improved accuracy of electrojet engine temperature measurement and reduced power inputs for maintenance of required temperature mode of electrojet engines.

2 cl, 1 dwg

Similar patents RU2370668C2

Title Year Author Number
SPACECRAFT ELECTROJET ENGINE INSTALLATION 1990
  • Baranov A.P.
  • Gopanchuk V.V.
  • Kastusik I.B.
  • Sorokin I.B.
RU1753775C
METHOD OF LAUNCH AND POWER SUPPLY OF ELECTROJET PLASMA ENGINE (VERSIONS) AND DEVICE FOR ITS IMPLEMENTATION (VERSIONS) 2008
  • Kozubskij Konstantin Nikolaevich
  • Murashko Vjacheslav Mikhajlovich
  • Gopanchuk Vladimir Vasil'Evich
  • Olotin Sergej Vladimirovich
RU2366123C1
ELECTROJET ENGINE 2007
  • Tjutjukin Aleksandr Evgen'Evich
  • Urtmintsev Igor' Aleksandrovich
RU2348832C2
ELECTROREACTIVE PROPULSION PLANT 2002
  • Gopanchuk V.V.
  • Zhasan V.S.
  • Kovalenko T.V.
RU2230221C2
METHOD OF DETERMINATION OF WORKING MEDIUM RATE IN PLASMA ENGINE INCORPORATED WITH SPACECRAFT ELECTROJET POWER PLANT 2006
  • Gnizdor Roman Jur'Evich
  • Murashko Vjacheslav Mikhajlovich
  • Gopanchuk Vladimir Vasil'Evich
RU2327132C1
ELECTRIC JET PROPULSION PLANT 2018
  • Gecha Vladimir Yakovlevich
  • Sidnyaev Nikolaj Ivanovich
  • Onufriev Valerij Valentinovich
RU2727103C2
MULTIFUNCTIONAL ELECTRIC PROPULSION ENGINE SUBSYSTEM OF THE SPACECRAFT 2021
  • Ermoshkin Iurii Mikhailovich
  • Kochev Iurii Vladimirovich
  • Ostapushchenko Aleksandr Anatolevich
  • Iakimov Evgenii Nikolaevich
RU2764819C1
HOLLOW CATHODE 2017
  • Gopanchuk Vladimir Vasilevich
  • Gorbachev Yurij Mitrofanovich
  • Parakhin Grigorij Aleksandrovich
RU2663241C1
MAGNETOPLASMA ELECTRIC JET ENGINE 2021
  • Arakelyan Aleksandr Vladimirovich
  • Gorbunov Kirill Sergeevich
  • Larin Aleksandr Petrovich
  • Smolentsev Aleksandr Alekseevich
  • Terentev Igor Petrovich
RU2764496C1
METHOD FOR ARRANGING CATHODE-COMPENSATOR IN PLASMA ENGINE, AND DEVICE FOR ITS IMPLEMENTATION 2010
  • Gnizdor Roman Jur'Evich
  • Mitrofanova Ol'Ga Aleksandrovna
  • Gopanchuk Vladimir Vasil'Evich
  • Kozubskij Konstantin Nikolaevich
  • Murashko Vjacheslav Mikhajlovich
RU2426913C1

RU 2 370 668 C2

Authors

Gnizdor Roman Jur'Evich

Gopanchuk Vladimir Vasil'Evich

Kozubskij Konstantin Nikolaevich

Murashko Vjacheslav Mikhajlovich

Dates

2009-10-20Published

2007-09-25Filed