초록 ▼

A system for use in monitoring, measuring, recording, computing and transmitting the oxygen levels and identification of oxygen contamination within an aircraft telescopic landing gear strut. An oxygen sensor is mounted in relation to each of the landing gear struts as to monitor, recognize, measure

A system for use in monitoring, measuring, recording, computing and transmitting the oxygen levels and identification of oxygen contamination within an aircraft telescopic landing gear strut. An oxygen sensor is mounted in relation to each of the landing gear struts as to monitor, recognize, measure and record the identification of oxygen within the telescopic landing gear struts. The amount of oxygen within each landing gear strut is measured and recorded and downloaded to the responsible aircraft maintenance department. By detecting the amount of oxygen in a strut, steps can be taken to purge the gas from the strut to minimize corrosion of strut components and to prevent internal combustion of the gas and oil in the strut.

대표청구항 ▼

1. An apparatus for monitoring a landing gear strut of an aircraft, comprising: a) the landing gear strut being telescopic and containing an interior gas;b) an oxygen sensor mounted to the landing gear strut and exposed to the interior gas of the landing gear strut;c) a processor connected to the ox

1. An apparatus for monitoring a landing gear strut of an aircraft, comprising: a) the landing gear strut being telescopic and containing an interior gas;b) an oxygen sensor mounted to the landing gear strut and exposed to the interior gas of the landing gear strut;c) a processor connected to the oxygen sensor, the processor recording information from the oxygen sensor. 2. The apparatus of claim 1 wherein the landing gear strut comprises a service port, the oxygen sensor located in the service port. 3. The apparatus of claim 1 wherein the landing gear strut comprises a service port, further comprising a coupling connected to the service port, the oxygen sensor connected to the coupling. 4. The apparatus of claim 1, further comprising an accumulator in communication with the landing gear strut interior gas, the oxygen sensor located so that the interior gas flows relative to the oxygen sensor as the strut compresses and decompresses. 5. The apparatus of claim 1, further comprising a pressure sensor exposed to the interior gas, the processor connected to the pressure sensor, the processor recording information from the oxygen sensor when the pressure sensor detects a change in strut pressure. 6. The apparatus of claim 1, further comprising a pressure sensor exposed to the interior gas, the processor connected to the pressure sensor, the processor recording information from the oxygen sensor when the pressure sensor detects a predetermined strut pressure when the strut is fully extended. 7. A method of monitoring a landing gear strut of an aircraft, the landing gear strut being telescopic and containing interior gas, comprising the steps of: a) measuring oxygen in the interior gas;b) recording the measurement;c) determining by a processor if the measured oxygen is within an acceptable limit;d) if the measured oxygen is not within the acceptable limit, then providing an indication. 8. The method of claim 7 wherein the step of measuring oxygen in the interior gas further comprises the step of measuring oxygen as the strut is compressing or extending. 9. The method of claim 7 wherein if an indication is provided, then purging the interior gas from the strut. 10. The method of claim 7 wherein the strut has an estimated calendar life based upon internal corrosion of the strut, further comprising the steps of: a) taking plural measurements of oxygen in the interior gas;b) using the measurements to adjust the calendar life limitation of the strut. 11. The apparatus of claim 7, further comprising the steps of: a) measuring the pressure of the landing gear strut interior gas;b) detecting a change in the strut pressure; andc) recording the measurement of oxygen in the interior gas during the change in strut pressure. 12. The apparatus of claim 7, further comprising the steps of: a) providing a predetermined strut pressure when the strut is fully extended;b) measuring the pressure of the strut interior gas;c) detecting from the pressure measurement when the strut is fully extended; andd) recording the measurement of oxygen in the interior gas when the strut is fully extended. 13. A method of monitoring a landing gear strut of an aircraft, the landing gear strut being telescopic and containing interior gas, comprising the steps of: a) measuring oxygen in the interior gas;b) recording the measurement;c) determining by a processor if the measured oxygen is within an acceptable limit;d) if the measured oxygen is not within the acceptable limit, then providing an indication; ande) the step of determining if the measured oxygen is within an acceptable limit further comprises determining if the measured oxygen can cause combustion in the strut interior.