RU95105028A - Flying vehicle engine plant - Google Patents

Flying vehicle engine plant

Info

Publication number
RU95105028A
RU95105028A RU95105028/06A RU95105028A RU95105028A RU 95105028 A RU95105028 A RU 95105028A RU 95105028/06 A RU95105028/06 A RU 95105028/06A RU 95105028 A RU95105028 A RU 95105028A RU 95105028 A RU95105028 A RU 95105028A
Authority
RU
Russia
Prior art keywords
flying vehicle
engine plant
wall
reaction chamber
tank
Prior art date
Application number
RU95105028/06A
Other languages
Russian (ru)
Other versions
RU2089743C1 (en
Inventor
А.А. Бахмутов
И.А. Клепиков
В.И. Прищепа
Original Assignee
А.А. Бахмутов
И.А. Клепиков
В.И. Прищепа
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 А.А. Бахмутов, И.А. Клепиков, В.И. Прищепа filed Critical А.А. Бахмутов
Priority to RU95105028A priority Critical patent/RU2089743C1/en
Publication of RU95105028A publication Critical patent/RU95105028A/en
Application granted granted Critical
Publication of RU2089743C1 publication Critical patent/RU2089743C1/en

Links

Landscapes

  • Cooling, Air Intake And Gas Exhaust, And Fuel Tank Arrangements In Propulsion Units (AREA)
  • Toys (AREA)

Abstract

FIELD: aeronautical engineering. SUBSTANCE: engine plant of flying vehicle contains propellant tanks, service lines and reaction chamber in hinged suspension for turning about fixed center of rotation lying in axis of chamber between its outlet and band for transmission of thrust to flying vehicle board; at this level, tank wall is provided with flexible angular displacement compensator. Reaction chamber is located in propellant tank and is fastened to its wall. EFFECT: simplified construction, reduced mass and improved power characteristics of engine plant.

Claims (1)

Двигательная установка летательного аппарата включает топливные баки, расходные магистрали, размещенную в топливном баке и скрепленную с его стенкой реактивную камеру, которая установлена в шарнирном подвесе с возможностью поворота вокруг неподвижно о центра вращения, находящегося на оси камеры между ее выходом и поясом передачи тяги на борт аппарата, и на указанном уровне стенка бака снабжена гибким компенсатором углового перемещения камеры. Технический результат состоит в упрощении, снижении массы и повышении энергетических характеристик двигательной установки. Изобретение целесообразно для двигательных установок летательных аппаратов с жидким топливам на борту.Aircraft propulsion system includes fuel tanks, consumables, a reaction chamber located in the fuel tank and fastened to its wall, which is mounted in a hinged suspension with the possibility of rotation around the center of rotation located on the axis of the camera between its exit and the transmission belt apparatus, and at the indicated level, the tank wall is equipped with a flexible compensator for the angular movement of the camera. The technical result consists in simplifying, reducing weight and increasing the energy characteristics of the propulsion system. The invention is suitable for propulsion systems of aircraft with liquid fuels on board.
RU95105028A 1995-04-04 1995-04-04 Aircraft engine unit RU2089743C1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU95105028A RU2089743C1 (en) 1995-04-04 1995-04-04 Aircraft engine unit

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU95105028A RU2089743C1 (en) 1995-04-04 1995-04-04 Aircraft engine unit

Publications (2)

Publication Number Publication Date
RU95105028A true RU95105028A (en) 1997-02-20
RU2089743C1 RU2089743C1 (en) 1997-09-10

Family

ID=20166377

Family Applications (1)

Application Number Title Priority Date Filing Date
RU95105028A RU2089743C1 (en) 1995-04-04 1995-04-04 Aircraft engine unit

Country Status (1)

Country Link
RU (1) RU2089743C1 (en)

Also Published As

Publication number Publication date
RU2089743C1 (en) 1997-09-10

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