ABLATIVE PULSE PLASMA ENGINE Russian patent published in 2018 - IPC F03H1/00 

Abstract RU 2664892 C1

FIELD: engines and pumps; astronautics.

SUBSTANCE: invention relates to space vehicle engines. Ablative pulse plasma engine (APPE) contains parallel located flat cathode and anode forming a discharge channel. Two dielectric checkers made of ablating material are installed between the cathode and the anode from opposite sides of the discharge channel symmetrically with respect to its longitudinal median plane, oriented perpendicular to the flat working surfaces of the cathode and the anode and dividing the discharge channel into two equal parts in volume. Moving dielectric blocks device ensures their feeding in the direction of the longitudinal median plane. Between the cathode and the anode there is an end insulator that forms the closed end part of the discharge channel. In the opening of the cathode are located the electrodes of the device for initiating an electric discharge. Current leads that connect the discharge electrodes to a capacitive energy storage device include two power sections having a planar shape and located between the cathode and the anode perpendicularly to their flat working surfaces. Power sections are electrically isolated relative to each other and located outside the discharge channel in a plane parallel to the closed end part of the discharge channel, symmetrically with respect to the longitudinal median plane between the planes passing through the side surfaces of the discharge electrodes. First power section is connected from one side with the cathode, and from the opposite side, located opposite the end part of the anode, with a negative polarity contact of the capacitive accumulator. Second power section is connected from one side with the anode, and from the opposite side, located opposite the end part of the cathode, with a positive polarity contact of the capacitive accumulator.

EFFECT: invention allows to increase the average mass velocity of plasma outflow from the discharge channel and the specific impulse of the APPE, to simplify the design of the APPE and to increase its reliability.

4 cl, 5 dwg

Similar patents RU2664892C1

Title Year Author Number
ABLATION PULSE PLASMA ENGINE 2018
  • Bogatyj Aleksandr Vladimirovich
  • Dyakonov Grigorij Aleksandrovich
  • Lyubinskaya Nataliya Valentinovna
  • Semenikhin Sergej Anatolevich
RU2688049C1
ERODING PULSE PLASMA ACCELERATOR 2013
  • Bogatyj Aleksandr Vladimirovich
  • D'Jakonov Grigorij Aleksandrovich
  • Nechaev Ivan Leonidovich
RU2542354C1
PULSE PLASMA ACCELERATOR AND PLASMA ACCELERATION METHOD 2003
  • Antropov N.N.
  • D'Jakonov G.A.
  • Orlov M.M.
  • Popov G.A.
  • Tjutin V.K.
  • Jakovlev V.N.
RU2253953C1
ERODING PULSE PLASMA ACCELERATOR 2012
  • Bogatyj Aleksandr Vladimirovich
  • D'Jakonov Grigorij Aleksandrovich
  • Popov Garri Alekseevich
RU2516011C1
METHOD OF OPERATING PULSED PLASMA ACCELERATOR 2010
  • Bogatyj Aleksandr Vladimirovich
  • D'Jakonov Grigorij Aleksandrovich
RU2452142C1
IMPULSE EROSION PLASMA ENGINE 1998
  • Antropov N.N.
  • D'Jakonov G.A.
  • Krivonosov I.G.
  • Gomilka L.A.
  • Orlov M.M.
  • Popov G.A.
  • Rudikov A.I.
  • Jakovlev V.N.
RU2143586C1
ELECTRIC JET ENGINE PLANT 2014
  • Zheleznjakov Il'Ja Konstantinovich
  • Zimina Tamara Aleksandrovna
  • Radchenko Anatolij Vasil'Evich
  • Shelkov Nikolaj Pavlovich
RU2568825C2
PROPULSION SYSTEM WITH PULSE ELECTRIC PROPULSION ENGINE 2016
  • Potabachnyj Leonid Alekseevich
RU2666918C2
IONIC ROCKET ENGINE OF SPACECRAFT 2018
  • Tsybin Oleg Yurevich
  • Makarov Sergej Borisovich
RU2682962C1
HIGH-FREQUENCY PLASMA SOURCE 2022
  • Bondarenko Dmitrij Alekseevich
  • Vavilin Konstantin Viktorovich
  • Zadiriev Ilya Igorevich
  • Kralkina Elena Aleksandrovna
  • Marinin Sergej Yurevich
RU2789534C1

RU 2 664 892 C1

Authors

Dyakonov Grigorij Aleksandrovich

Lebedev Vladimir Leonidovich

Lyubinskaya Nataliya Valentinovna

Nechaev Ivan Leonidovich

Semenikhin Sergej Anatolevich

Dates

2018-08-23Published

2017-12-08Filed