Accession Number : AD0164039

Title :   Load and Rate of Change of Load Detection System.

Descriptive Note : Patent,

Corporate Author : DEPARTMENT OF THE NAVY WASHINGTON D C

Personal Author(s) : Lenenthal,Robert S.

Report Date : 30 JUN 1970

Pagination or Media Count : 5

Abstract : The present invention relates to a system for detecting and recording the level and rate of change of landing loads in the struts of aircraft landing gear. The system uses pressure sensors in the struts. The sensors are connected to a plurality of measuring circuits which are operable in response to a minimum pressure to record the level and rate of change of pressure detected by the sensor.

Descriptors :   (*LANDING GEAR, *PATENTS), (*AIRCRAFT LANDINGS, LANDING IMPACT), SHOCK ABSORBERS, INSTRUMENTATION, PRESSURE GAGES, LOGIC CIRCUITS

Subject Categories : Aircraft

Distribution Statement : APPROVED FOR PUBLIC RELEASE