UA95860U - DEVICE FOR TESTING TIGHTNESS of SPACECRAFT FUEL TANK SUPERCHARGE system - Google Patents

DEVICE FOR TESTING TIGHTNESS of SPACECRAFT FUEL TANK SUPERCHARGE system

Info

Publication number
UA95860U
UA95860U UAU201407911U UAU201407911U UA95860U UA 95860 U UA95860 U UA 95860U UA U201407911 U UAU201407911 U UA U201407911U UA U201407911 U UAU201407911 U UA U201407911U UA 95860 U UA95860 U UA 95860U
Authority
UA
Ukraine
Prior art keywords
pneumatic
fuel tank
check
line
lines
Prior art date
Application number
UAU201407911U
Other languages
Russian (ru)
Ukrainian (uk)
Inventor
Viktor Mykytovych Banin
Sergii Borysovych Zhyronkin
Yurko Anatoliiovych Kolodchenko
Andrii Oleksandrovych Mokin
Oleksandr Vasyliovych Mokin
Dmytro Sergiiovych Reshetylo
Original Assignee
Viktor Mykytovych Banin
Sergii Borysovych Zhyronkin
Yurko Anatoliiovych Kolodchenko
Andrii Oleksandrovych Mokin
Oleksandr Vasyliovych Mokin
Dmytro Sergiiovych Reshetylo
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 Viktor Mykytovych Banin, Sergii Borysovych Zhyronkin, Yurko Anatoliiovych Kolodchenko, Andrii Oleksandrovych Mokin, Oleksandr Vasyliovych Mokin, Dmytro Sergiiovych Reshetylo filed Critical Viktor Mykytovych Banin
Priority to UAU201407911U priority Critical patent/UA95860U/en
Publication of UA95860U publication Critical patent/UA95860U/en

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  • Examining Or Testing Airtightness (AREA)

Abstract

A device for testing tightness of the fuel tank of supercharge system of spacecraft containing pneumatic lines associated with supercharge cylinders and gas cavities of fuel tanks, electro-pneumatic valves mounted on pneumatic lines, gas reducers, check valves and pressure sensors, as well as consumables lines attached to the fluid cavities of fuel tanks and, check mouths. The device is equipped with a removable bypass lines, on each of which are mounted a receiver, the throttling device and an additional pressure sensor, wherein each removable bypass line with one end is connected to the check mouth installed in pneumatic line ay the inlet of the gas cavity of one of the fuel tanks and the other end - to the check mouth installed in the flow line at the outlet of the same fuel tank fluid cavity, the throttling device is mounted in the removable bypass line at the end connected to the check mouth installed in pneumatic line.
UAU201407911U 2014-07-14 2014-07-14 DEVICE FOR TESTING TIGHTNESS of SPACECRAFT FUEL TANK SUPERCHARGE system UA95860U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
UAU201407911U UA95860U (en) 2014-07-14 2014-07-14 DEVICE FOR TESTING TIGHTNESS of SPACECRAFT FUEL TANK SUPERCHARGE system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
UAU201407911U UA95860U (en) 2014-07-14 2014-07-14 DEVICE FOR TESTING TIGHTNESS of SPACECRAFT FUEL TANK SUPERCHARGE system

Publications (1)

Publication Number Publication Date
UA95860U true UA95860U (en) 2015-01-12

Family

ID=52988769

Family Applications (1)

Application Number Title Priority Date Filing Date
UAU201407911U UA95860U (en) 2014-07-14 2014-07-14 DEVICE FOR TESTING TIGHTNESS of SPACECRAFT FUEL TANK SUPERCHARGE system

Country Status (1)

Country Link
UA (1) UA95860U (en)

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