FIELD: instrumentation.
SUBSTANCE: invention relates to the system and the method of measurement of fatigue for mechanical details of aircrafts, for example of planes, and also to the aircraft maintenance method. The system of measurement of general fatigue damage of the detail (7, 8, P, P', 9a, 6') of the aircraft exposed to mechanical tensions, containing a set of tension sensors (Ci) installed on the detail (7, 8, P, P', 9a, 6'), while each sensor is implemented with a possibility of detection of pre-set threshold (S (Ci)) of mechanical tension and with a possibility of sending of the signal (Si) of data witnessing on excess of this threshold (S (Ci)); the system contains the devices (11) for registration of these data, and the sensors (Ci) are implemented with a possibility of detection of mutually different and discrete thresholds (S (Ci)) that allows on the basis of the data registered by system to calculate the estimated fatigue of the detail (7, 8, P, P', 9a, 6') connected with the considered mechanical tension.
EFFECT: optimisation of inspections of details.
10 cl, 4 dwg, 1 tbl
Title | Year | Author | Number |
---|---|---|---|
ATTACHMENT OF MULTISTAGE TURBOJET TO AIRCRAFT | 2009 |
|
RU2483004C2 |
VIBRATION ABSORBER FOR AIRCRAFT GONDOLA | 2008 |
|
RU2467221C2 |
TURBOJET HINGED TO AIRCRAFT PYLON | 2008 |
|
RU2487056C2 |
METHOD TO CONTROL AIRCRAFT TURBOJET ENGINE THRUST DISTURBANCE | 2013 |
|
RU2638417C2 |
REAR BELT OF TURBOJET ENGINE-TO-AIRCRAFT FASTENING SYSTEM | 2000 |
|
RU2188961C1 |
AIRCRAFT POWER PLANT | 2009 |
|
RU2499745C2 |
METHOD AND DEVICE FOR MOUNTING ENGINE ON AIRCRAFT PYLON | 2015 |
|
RU2690834C2 |
AERODYNAMIC ELEMENT FOR AIRCRAFT NACELLE | 2011 |
|
RU2571981C2 |
AIRCRAFT GAS TURBINE ENGINE MOUNT BAR | 2010 |
|
RU2571680C2 |
AIRCRAFT ENGINE UNIT | 2008 |
|
RU2469917C2 |
Authors
Dates
2015-10-27—Published
2010-11-15—Filed