Method of measuring the compression of a shock absorber, and an airplane undercarriage constituting an application thereof
View Patent ↗An airplane undercarriage including a shock absorber having first and second portions that are movable relative to each other. The undercarriage further including a first wave transceiver assembly disposed on the first movable portion. The assembly includes a first transmitter for transmitting a first wave towards the second movable portion and a first receiver for receiving the first wave after it has been reflected on an obstacle formed by a mechanical part secured to the second movable portion. The undercarriage also includes an independent second wave transceiver assembly disposed on the first movable portion. The second assembly includes a second transmitter for transmitting a second wave towards the second movable portion, and a second receiver for receiving the second wave after it has been reflected on an obstacle formed by a free surface of a hydraulic fluid contained in the shock absorber or a mechanical part defining the free surface.
1. An airplane undercarriage including a shock absorber having first and second portions that are slidably movable relative to each other, the undercarriage further including:
a first wave transceiver assembly disposed on the first movable portion, the first wave transceiver comprising:
a first transmitter for transmitting a first wave towards the second movable portion;
a first receiver for receiving the first wave after it has been reflected on an obstacle formed by a mechanical part secured to the second movable portion; and
an independent second wave transceiver assembly disposed on the first movable portion, the independent second transceiver comprising:
a second transmitter for transmitting a second wave towards the second movable portion; and
a second receiver for receiving the second wave after it has been reflected on an obstacle formed by a free surface of a hydraulic fluid contained in the shock absorber or a mechanical part defining said free surface.
2. An undercarriage according to claim 1 , wherein the transceiver assemblies are disposed on the undercarriage in such a manner that the paths followed by the waves transmitted by the transceiver assemblies are contained fully within the shock absorber.
3. An airplane including at least one undercarriage according to claim 1 , the airplane including means for determining a theoretical level of hydraulic fluid in the shock absorber from the measurement of a characteristic of the first wave, and for determining a real level of hydraulic fluid in the shock absorber from the measurement of a characteristic of the second wave.
4. An airplane according to claim 3 , further including means for comparing the theoretical level of fluid in the shock absorber with the real level of fluid in the shock absorber.