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RU2018113687A - KNOCKING REACTIVE ENGINE - Google Patents

KNOCKING REACTIVE ENGINE Download PDF

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Publication number
RU2018113687A
RU2018113687A RU2018113687A RU2018113687A RU2018113687A RU 2018113687 A RU2018113687 A RU 2018113687A RU 2018113687 A RU2018113687 A RU 2018113687A RU 2018113687 A RU2018113687 A RU 2018113687A RU 2018113687 A RU2018113687 A RU 2018113687A
Authority
RU
Russia
Prior art keywords
translucent
housing
knocking
movable
shell
Prior art date
Application number
RU2018113687A
Other languages
Russian (ru)
Other versions
RU2018113687A3 (en
RU2740739C2 (en
Inventor
Владимир Дмитриевич Шкилев
Алексей Пантелеевич Коржавый
Анатолий Александрович Анкудинов
Виталий Владимирович Коротков
Андрей Николаевич Маклачков
Original Assignee
Владимир Дмитриевич Шкилев
Алексей Пантелеевич Коржавый
Анатолий Александрович Анкудинов
Виталий Владимирович Коротков
Андрей Николаевич Маклачков
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 Владимир Дмитриевич Шкилев, Алексей Пантелеевич Коржавый, Анатолий Александрович Анкудинов, Виталий Владимирович Коротков, Андрей Николаевич Маклачков filed Critical Владимир Дмитриевич Шкилев
Priority to RU2018113687A priority Critical patent/RU2740739C2/en
Publication of RU2018113687A publication Critical patent/RU2018113687A/en
Publication of RU2018113687A3 publication Critical patent/RU2018113687A3/ru
Application granted granted Critical
Publication of RU2740739C2 publication Critical patent/RU2740739C2/en

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
    • 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
    • F03H99/00—Subject matter not provided for in other groups of this subclass

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Plasma & Fusion (AREA)
  • Combustion Methods Of Internal-Combustion Engines (AREA)
  • Plasma Technology (AREA)

Claims (1)

Светоэрозионный ракетный двигатель, содержащий корпус с подвижной и управляемой поверхностью и сверхзвуковым соплом, светопрозрачной цилиндрической оболочкой, заполненной инертным газом, с электродами, расположенными на противоположных концах светопрозрачной оболочки и подключенными к высоковольтному разрядному конденсатору через импульсный размыкатель, отличающийся тем, что подвижная поверхность выполнена в виде твердого светопоглощающего материала, например эбонита, между корпусом и поверхностью расположен светопрозрачный цилиндр, с соплом, образующий канал, корпус снабжен отражателем, а светопрозрачная оболочка выполнена в виде спирали и расположена внутри корпуса.A light-erosive rocket engine containing a housing with a movable and controllable surface and a supersonic nozzle, a translucent cylindrical shell filled with an inert gas, with electrodes located at opposite ends of the translucent shell and connected to the high-voltage discharge capacitor through a pulse disconnector, characterized in that the movable surface is made in as a solid light-absorbing material, for example ebonite, a translucent qi is located between the body and the surface the cylinder, with a nozzle forming a channel, the housing is equipped with a reflector, and the translucent shell is made in the form of a spiral and is located inside the housing.
RU2018113687A 2018-04-16 2018-04-16 Detonation jet engine RU2740739C2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2018113687A RU2740739C2 (en) 2018-04-16 2018-04-16 Detonation jet engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2018113687A RU2740739C2 (en) 2018-04-16 2018-04-16 Detonation jet engine

Publications (3)

Publication Number Publication Date
RU2018113687A true RU2018113687A (en) 2019-10-17
RU2018113687A3 RU2018113687A3 (en) 2020-02-13
RU2740739C2 RU2740739C2 (en) 2021-01-20

Family

ID=68279233

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2018113687A RU2740739C2 (en) 2018-04-16 2018-04-16 Detonation jet engine

Country Status (1)

Country Link
RU (1) RU2740739C2 (en)

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4608821A (en) * 1984-07-31 1986-09-02 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Heat exchanger for electrothermal devices
US4805400A (en) * 1987-04-27 1989-02-21 Olin Corporation Non-erosive arcjet starting control system and method
JPH03122087A (en) * 1989-10-04 1991-05-24 Osaka Gas Co Ltd Solid propellant and method for propelling object with solid propellant
RU2099573C1 (en) * 1995-04-27 1997-12-20 Исследовательский центр им.М.В.Келдыша Electric arc rocket engine
RU2479673C1 (en) * 2011-09-05 2013-04-20 Александр Григорьевич Григорьянц Impulse electrogasdynamic formation method of identification marks on surface of solid material
RU2644798C1 (en) * 2016-03-18 2018-02-14 Владимир Дмитриевич Шкилев Pulsed detonation rocket engine

Also Published As

Publication number Publication date
RU2018113687A3 (en) 2020-02-13
RU2740739C2 (en) 2021-01-20

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Legal Events

Date Code Title Description
MM4A The patent is invalid due to non-payment of fees

Effective date: 20200417