METHOD FOR TESTING OF PNEUMATIC SYSTEM AIR-TIGHTNESS Russian patent published in 1997 - IPC

Abstract RU 2077708 C1

FIELD: instruments. SUBSTANCE: method involves putting space ship to vacuum-chamber, which is connected to leakage detector, connecting vacuum chamber to inner chamber of compartment, pumping vacuum chamber and compartment down to minimal rest pressure of vacuum chamber, pumping weighed flow of testing gas of Qtw to compartment, measuring change in concentration Ctw(com) of testing gas in vacuum chamber with respect to weighed flow which is supplied to compartment, finishing supply of weighed flow of testing gas of Qtw to compartment, starting supply of this weighed flow to vacuum chamber, measuring change in concentration Ctw(vac)(c) of testing gas in vacuum chamber with respect to weighed flow which is supplied to vacuum chamber, when vacuum chamber and inner chamber of compartment are connected, disconnecting vacuum chamber and inner chamber of compartment, measuring change in concentration Ctw(vac)(d) of testing gas in vacuum chamber with respect to weighed flow which is supplied to vacuum chamber, when vacuum chamber and inner chamber of compartment are disconnected, finishing supply of weighed flow of testing gas of Qtw to vacuum chamber, connecting vacuum chamber and inner chamber of compartment anew, filling pneumatic system with testing gas, measuring change in concentration Csyst(c) of testing gas in vacuum chamber caused by small-scale leakage in units and pipes of pneumatic system when vacuum chamber and inner chamber of compartment are connected, disconnecting vacuum chamber and inner chamber of compartment, measuring change in concentration Csyst(d) of testing gas in vacuum chamber caused by small-scale leakage in units and pipes of pneumatic system when vacuum chamber and inner chamber of compartment are disconnected. This results in possibility to judge pneumatic system air-tightness Qsyst by ratio of measured values. EFFECT: increased precision of testing.

Similar patents RU2077708C1

Title Year Author Number
PROCESS OF TEST FOR LEAKS OF PNEUMATIC-HYDRAULIC SYSTEMS 1994
  • Lipnjak L.V.
  • Panov N.G.
  • Shcherbakov Eh.V.
RU2086941C1
METHOD TESTING LEAK-PROOFNESS OF PNEUMATIC-HYDRAULIC SYSTEMS 1994
  • Lipnjak L.V.
  • Panov N.G.
  • Shcherbakov Eh.V.
RU2077040C1
DEVICE FOR CHECK-UP OF SPACESHIP AIR-TIGHTNESS 1994
  • Lipnjak L.V.
  • Panov N.G.
  • Shcherbakov Eh.V.
RU2080576C1
METHOD OF LEAK-PROOFNESS TEST OF MECHANICALLY LINKED SPACESHIP MODULES 1994
  • Panov N.G.
RU2082134C1
METHOD FOR TESTING AIR-TIGHTNESS OF MULTIPLE-CHAMBER ARTICLES 1994
  • Panov N.G.
  • Shcherbakov Eh.V.
RU2077707C1
METHOD OF TEST OF AIR-TIGHTNESS OF MULTISPACE ARTICLES 1994
  • Panov N.G.
  • Shcherbakov Eh.V.
RU2077039C1
PROCESS TESTING TIGHTNESS OF ARTICLE 1994
  • Zjablov V.A.
  • Kapustkin D.P.
  • Lipnjak L.V.
  • Shcherbakov Eh.V.
RU2079121C1
METHOD OF CHECKING OF PRODUCT LEAK-PROOFNESS 1993
  • Panov N.G.
RU2073836C1
METHOD TESTING VACUUM TIGHTNESS OF SYSTEMS OF SPACECRAFT 1996
  • Zjablov V.A.
  • Lipnjak L.V.
  • Shcherbakov Eh.V.
RU2112945C1
METHOD OF DETECTION OF LOSS OF TIGHTNESS OF TECHNOLOGICAL LINE IN MIX OF AIR-TIGHT COMPARTMENT 1994
  • Lipnjak L.V.
  • Ol'Shanskij V.A.
  • Panov N.G.
  • Shcherbakov Eh.V.
RU2085887C1

RU 2 077 708 C1

Authors

Lipnjak L.V.

Panov N.G.

Shcherbakov Eh.V.

Dates

1997-04-20Published

1994-02-04Filed