RU96111298A - SPEED AIRCRAFT FUEL TANKS SUPPLY SYSTEM - Google Patents

SPEED AIRCRAFT FUEL TANKS SUPPLY SYSTEM

Info

Publication number
RU96111298A
RU96111298A RU96111298/06A RU96111298A RU96111298A RU 96111298 A RU96111298 A RU 96111298A RU 96111298/06 A RU96111298/06 A RU 96111298/06A RU 96111298 A RU96111298 A RU 96111298A RU 96111298 A RU96111298 A RU 96111298A
Authority
RU
Russia
Prior art keywords
fuel tanks
supply system
pneumatic
aircraft fuel
speed aircraft
Prior art date
Application number
RU96111298/06A
Other languages
Russian (ru)
Other versions
RU2119082C1 (en
Inventor
В.И. Гореликов
Л.Н. Сарычев
В.М. Цихоцкий
Original Assignee
Ракетно-космическая корпорация "Энергия" им.С.П.Королева
Filing date
Publication date
Application filed by Ракетно-космическая корпорация "Энергия" им.С.П.Королева filed Critical Ракетно-космическая корпорация "Энергия" им.С.П.Королева
Priority to RU96111298A priority Critical patent/RU2119082C1/en
Priority claimed from RU96111298A external-priority patent/RU2119082C1/en
Publication of RU96111298A publication Critical patent/RU96111298A/en
Application granted granted Critical
Publication of RU2119082C1 publication Critical patent/RU2119082C1/en

Links

Claims (1)

Система наддува топливных баков двигательной установки космического летательного аппарата, содержащая герметичный газонаполненный контейнер с размещенным в нем бортовым компрессором, связанным пневмомагистралями низкого давления с газовыми полостями соответствующих топливных баков и блок управления электропневмоклапанами, отличающаяся тем, что одна из пневмомагистралей через последовательно установленные фильтр, электропневмоклапан, газовый редуктор и сигнализатор давления сообщена дополнительной магистралью непосредственно с объемом контейнера, причем электропневмоклапан электрически связан через блок управления электропневмоклапанами с сигнализатором давления.A system for pressurizing the fuel tanks of a spacecraft’s propulsion system, comprising a sealed gas-filled container with an onboard compressor located in it, connected by low pressure pneumatic lines to the gas cavities of the respective fuel tanks, and an electric pneumatic valve control unit, characterized in that one of the pneumatic lines is connected through a filter, an electric pneumatic valve, gas pressure regulator and pressure switch communicated by additional line directly with the volume of the container, and the electro-pneumatic valve is electrically connected through the control unit of the electro-pneumatic valves with a pressure switch.
RU96111298A 1996-06-04 1996-06-04 Spacecraft propellant tank pressurization system RU2119082C1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU96111298A RU2119082C1 (en) 1996-06-04 1996-06-04 Spacecraft propellant tank pressurization system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU96111298A RU2119082C1 (en) 1996-06-04 1996-06-04 Spacecraft propellant tank pressurization system

Publications (2)

Publication Number Publication Date
RU96111298A true RU96111298A (en) 1998-09-10
RU2119082C1 RU2119082C1 (en) 1998-09-20

Family

ID=20181527

Family Applications (1)

Application Number Title Priority Date Filing Date
RU96111298A RU2119082C1 (en) 1996-06-04 1996-06-04 Spacecraft propellant tank pressurization system

Country Status (1)

Country Link
RU (1) RU2119082C1 (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2976626B1 (en) 2011-06-17 2013-07-05 Snecma CRYOGENIC PROPULSIVE ASSEMBLY
CN110566369A (en) * 2019-08-27 2019-12-13 上海空间推进研究所 Pressure supplementing type space propulsion system suitable for high-capacity surface tension storage tank

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