SYSTEM AND METHOD OF MEASUREMENT OF FATIGUE FOR MECHANICAL DETAILS OF AIRCRAFT AND AIRCRAFT MAINTENANCE METHOD Russian patent published in 2015 - IPC G01N3/32 G01M5/00 G07C3/00 

Abstract RU 2566373 C2

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

Similar patents RU2566373C2

Title Year Author Number
ATTACHMENT OF MULTISTAGE TURBOJET TO AIRCRAFT 2009
  • Bal'K Vuter
RU2483004C2
VIBRATION ABSORBER FOR AIRCRAFT GONDOLA 2008
  • Moradell-Casellas Pierre
RU2467221C2
TURBOJET HINGED TO AIRCRAFT PYLON 2008
  • Bajar Andre Bruno Deni
  • Shuar P'Er-Alen Zhan-Mari Filipp Jug
  • Konte Fransua Rajmon
  • Lefor Gijom
RU2487056C2
METHOD TO CONTROL AIRCRAFT TURBOJET ENGINE THRUST DISTURBANCE 2013
  • Dzhelassi Sedrik
RU2638417C2
REAR BELT OF TURBOJET ENGINE-TO-AIRCRAFT FASTENING SYSTEM 2000
  • Marchukov E.Ju.
  • Rajkov Ju.V.
RU2188961C1
AIRCRAFT POWER PLANT 2009
  • Bal'K Vuter
  • De Gall' Ann-Lor Mari Klemans
RU2499745C2
METHOD AND DEVICE FOR MOUNTING ENGINE ON AIRCRAFT PYLON 2015
  • Lambey, Mario
  • Beutin, Bruno, Albert
  • Tesniere, Marc, Patrick
RU2690834C2
AERODYNAMIC ELEMENT FOR AIRCRAFT NACELLE 2011
  • Blin Celine
  • Strub Guillaume
  • Reyron Vincent
RU2571981C2
AIRCRAFT GAS TURBINE ENGINE MOUNT BAR 2010
  • Djunleavi Patrik
  • Masson Rishar
  • Sehz Gilem
  • Ru Tibo Fransua
  • Lefor Gijom
RU2571680C2
AIRCRAFT ENGINE UNIT 2008
  • Baillard Andre
RU2469917C2

RU 2 566 373 C2

Authors

Sehz Gilem

Dates

2015-10-27Published

2010-11-15Filed