SU458184A1 - Device for testing the performance of the pressure control system in the pressurized cabin of an aircraft - Google Patents

Device for testing the performance of the pressure control system in the pressurized cabin of an aircraft

Info

Publication number
SU458184A1
SU458184A1 SU1891695/23A SU1891695A SU458184A1 SU 458184 A1 SU458184 A1 SU 458184A1 SU 1891695/23 A SU1891695/23 A SU 1891695/23A SU 1891695 A SU1891695 A SU 1891695A SU 458184 A1 SU458184 A1 SU 458184A1
Authority
SU
USSR - Soviet Union
Prior art keywords
aircraft
testing
performance
control system
pressure control
Prior art date
Application number
SU1891695/23A
Other languages
Russian (ru)
Inventor
В.Г. Воронин
Л.П. Левин
Ю.В. Чижиков
А.М. Котминов
Original Assignee
В.Г. Воронин
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 В.Г. Воронин filed Critical В.Г. Воронин
Priority to SU1891695/23A priority Critical patent/SU458184A1/en
Application granted granted Critical
Publication of SU458184A1 publication Critical patent/SU458184A1/en

Links

Landscapes

  • Testing Of Devices, Machine Parts, Or Other Structures Thereof (AREA)
  • Measuring Fluid Pressure (AREA)
  • Control Of Fluid Pressure (AREA)

Abstract

Устройство для проверки работоспособности системы регулирования давления в гермокабине летательного аппарата, содержащее высотомер, подключенный к дюзе исполнительного клапана системы, и вариометр, подключенный к трубопроводу, соединяющему входы "статика" и "атмосфера" командного прибора системы с источником давления через имитатор емкости гермокабины, отличающееся тем, что, с целью упрощения конструкции и повышения надежности работы, в качестве имитатора емкости гермокабины на указанном трубопроводе смонтирована вихревая труба, перед диафрагмой которой в месте подключения вариометра трубопровод соединен через натекатель с атмосферой.A device for testing the performance of the pressure control system in the pressurized cabin of an aircraft, containing an altimeter connected to the nozzle of the system actuating valve, and a variometer connected to the pipeline connecting the static and atmospheric inputs of the system command device with a pressure source through the pressurized container simulator, different the fact that, in order to simplify the design and increase the reliability of operation, a vortex tube was mounted on the specified pipeline as a simulator of the pressure container Power diaphragm which variometer at the connection conduit is connected through a leak valve to the atmosphere.

SU1891695/23A 1973-03-12 1973-03-12 Device for testing the performance of the pressure control system in the pressurized cabin of an aircraft SU458184A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU1891695/23A SU458184A1 (en) 1973-03-12 1973-03-12 Device for testing the performance of the pressure control system in the pressurized cabin of an aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU1891695/23A SU458184A1 (en) 1973-03-12 1973-03-12 Device for testing the performance of the pressure control system in the pressurized cabin of an aircraft

Publications (1)

Publication Number Publication Date
SU458184A1 true SU458184A1 (en) 2006-05-10

Family

ID=60522369

Family Applications (1)

Application Number Title Priority Date Filing Date
SU1891695/23A SU458184A1 (en) 1973-03-12 1973-03-12 Device for testing the performance of the pressure control system in the pressurized cabin of an aircraft

Country Status (1)

Country Link
SU (1) SU458184A1 (en)

Similar Documents

Publication Publication Date Title
GB1467106A (en) Pressure balancing device for heating systems
GB1510191A (en) Pressure-responsive valve in or for a cannula assembly
GB1370406A (en) Apparatus for testing leakage
GB1274895A (en) A liquid fuel supply control system
SU458184A1 (en) Device for testing the performance of the pressure control system in the pressurized cabin of an aircraft
GB1376613A (en) Fluid diaphragm modulator
ES401880A1 (en) Differential pressure indicating apparatus
GB751895A (en) Shock-damping means for liquid-conveying pipes
ES336136A1 (en) A reduction device-pressure regulator. (Machine-translation by Google Translate, not legally binding)
GB840675A (en) Improvements in or relating to fuel systems and warning devices therefor
GB1232496A (en)
NL6515422A (en)
SU609381A1 (en) AIR PRESSURE REGULATOR IN AIRCRAFT HERMOCABINE
GB756933A (en) Improvements in or relating to pressure control systems for aircraft pressure cabinsor the like
AU449992B2 (en) Fluid pressure actuated device anda gas turbine fuel control system incorporating such device
SU225639A1 (en) Pressure control system in aircraft fuel tanks
GB829500A (en) Improvements in fluid pressure systems and apparatus
SU200986A1 (en) Device for regulating the pressure in the hermetic cabin of the aircraft
GB1286556A (en) Apparatus for controlling pressure inside the cabin of an aircraft
SU319785A1 (en) Exhaust valve for pressure control systems in airtight cockpits of aircraft
SU581794A2 (en) Installation for testing systems for automatic control of air pressure in airtight cabins of aircraft
GB1252122A (en)
SU282859A1 (en) Exhaust valve
FR2434078A2 (en) Salvaging float for sub-marine equipment - has double inflatable membrane to give air controlled buoyancy and provides salvage container
CA608306A (en) Diaphragm pump for fluid fuel and vacuum systems