FIELD: test engineering.
SUBSTANCE: device comprises pipelines of supply and discharge of air with valves located on them, as well as the means of automatic program control of these valves. The structure of the means of automatic control comprises a pressure regulator, a pressure sensor, a program setting unit, two blocks of comparison, two blocks of setting the pressure levels and the logic element and connections to arrange interaction of these functional elements.
EFFECT: improved accuracy of development of loading programs, and reduction of technical means necessary to create plants of such type.
2 dwg
Title | Year | Author | Number |
---|---|---|---|
PLANT FOR ENDURANCE TESTING OF AIRCRAFT HULL | 2013 |
|
RU2538043C1 |
AIRCRAFT FUSELAGE DURABILITY TEST BENCH | 2013 |
|
RU2548054C2 |
DEVICE OF PNEUMATIC LOADING OF AIRCRAFT FUSELAGE DURING STRENGTH TESTS ON RESOURCE | 2015 |
|
RU2598778C1 |
METHOD OF COMPRESSED AIR LOADING OF AIRCRAFT FUSELAGE DURING ENDURANCE TEST | 2013 |
|
RU2537752C1 |
METHOD FOR PNEUMATIC LOADING OF AIRCRAFT FUSELAGE DURING STRENGTH TESTS ON RESOURCE | 2015 |
|
RU2598700C1 |
CLOSED VOLUME PRESSURE CONTROL METHOD | 2018 |
|
RU2692935C1 |
METHOD OF FATIGUE TESTS OF AIRCRAFT FUSELAGE | 2013 |
|
RU2538045C1 |
COMPRESSED AIR LOADING PLANT OF PRESSURISED FUSELAGE OF AIRCRAFT DURING ENDURANCE TEST | 2009 |
|
RU2416075C1 |
SAFETY DEVICE | 2021 |
|
RU2767086C1 |
DEVICE FOR DETERMINING AIR-TIGHTNESS AT STRENGTH TESTS | 2014 |
|
RU2562155C1 |
Authors
Dates
2015-02-10—Published
2013-09-24—Filed