FIELD: transport.
SUBSTANCE: invention relates to maintenance of aircraft, particularly, to control over serviceability of aircraft hydraulic system signalling and shutoff hardware. Proposed device comprises fluid flow rate controller arranged between aircraft fluid tank and ground hydraulic unit fluid tank. Besides, it includes automatic control unit with its input connected with second output of working fluid level metre in aircraft fluid tank and its output connected to fluid flow rate controller input.
EFFECT: accurate determination of working fluid critical pressure in aircraft hydraulic tank.
1 dwg
Title | Year | Author | Number |
---|---|---|---|
DEVICE FOR AIR BLEEDING FROM WORKING FLUID OF CLOSED HYDRAULIC SYSTEMS OF AIRCRAFTS | 2013 |
|
RU2553404C1 |
DEVICE OF HYDRAULIC SYSTEM OF SMALL HYDRAULIC UNIT AND METHOD OF ITS APPLICATION | 2023 |
|
RU2809868C1 |
AIR REMOVAL FROM AIRCRAFT CLOSED HYDRAULIC SYSTEM WORKING FLUID | 2014 |
|
RU2576554C1 |
DEVICE FOR AIR REMOVAL FROM AIRCRAFT CLOSED HYDRAULIC SYSTEM WORKING FLUID | 2014 |
|
RU2575733C1 |
METHOD FOR CONTINUOUS MONITORING OF INTEGRITY OF AIRCRAFT AT ALL FLIGHT PHASES THEREOF | 2013 |
|
RU2542746C2 |
MULTI-PURPOSE HIGHLY MANOEUVRABLE SUPERSONIC AIRCRAFT, ITS AIRFRAME, EQUIPMENT AND SYSTEMS | 1996 |
|
RU2207968C2 |
REMOTE AUTOMATED SYSTEM FOR PROPELLER PITCH CONTROL | 2007 |
|
RU2340489C1 |
SYSTEM FOR CONTROLLING TECHNICAL MEANS AND MOVEMENT OF AMSV | 2023 |
|
RU2825914C1 |
AIRCRAFT MOBILE ELECTRIC UNIT | 2024 |
|
RU2826191C1 |
AIRCRAFT TRANSPORTATION FACILITY | 2002 |
|
RU2307771C2 |
Authors
Dates
2014-04-27—Published
2012-08-10—Filed