DUAL-STAGE, STROKE-ACTIVATED, MIXED FLUID GAS SHOCK STRUT SERVICING MONITORING SYSTEM

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DUAL-STAGE, STROKE-ACTIVATED, MIXED FLUID GAS SHOCK STRUT SERVICING MONITORING SYSTEM

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FAZELI AMIR / CEPIC ADNAN / REBER SUSANNE M

A monitoring system for a dual-stage, stroke activated, mixed fluid gas shock strut may comprise a controller (201), and a tangible, non-transitory memory (208) configured to communicate with the controller. The tangible, non-transitory memory may have instructions stored thereon that, in response to execution by the controller, cause the controller to perform various operations. Said operations may include calculating, by the controller, a compression factor, determining, by the controller, a plurality of compression factors for known oil volumes based on at least one of the primary chamber temperature sensor reading and the shock strut stroke sensor reading, and calculating, by the controller, an oil volume in a primary chamber of the shock strut.

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Title :

DUAL-STAGE, STROKE-ACTIVATED, MIXED FLUID GAS SHOCK STRUT SERVICING MONITORING SYSTEM

Additional title:

ZWEISTUFIGES, HUBAKTIVIERTES, MISCHFLUID-GASFEDERBEINWARTUNGSÜBERWACHUNGSSYSTEM
SYSTÈME DE SURVEILLANCE D'ENTRETIEN D'AMORTISSEUR À GAZ-FLUIDE MÉLANGÉ À DEUX ÉTAGES ET ACTIVÉ PAR COURSE

Contributors:

FAZELI AMIR (author) / CEPIC ADNAN (author) / REBER SUSANNE M (author)

Publication date :

2021-01-06

Type of media :

Patent

Type of material :

Electronic Resource

Language :

English

Classification :

IPC:

F16F SPRINGS , Federn / B64C AEROPLANES , Flugzeuge / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen