The invention discloses an integrated active heat dissipation device used for an undercarriage
shock absorber. The integrated active heat dissipation device comprises a heat dissipation medium
storage tank, a heat dissipation medium pump body, an annular heat dissipation medium injection
pipe assembly, an
infrared temperature sensor and a battery. The heat dissipation medium
storage tank is detachably mounted on the outer wall of the top of the undercarriage
shock absorber. An inlet of the heat dissipation medium pump body is connected with a medium outlet of the heat dissipation medium
storage tank, an outlet of the heat dissipation medium pump body is fixed to one end of a guide
pipe, a
temperature control switch electrically connected with an airborne
avionics system is arranged on the heat dissipation medium pump body, and the
temperature control switch is electrically connected with the heat dissipation medium pump body. The annular heat dissipation medium injection
pipe assembly is fixed to the undercarriage
shock absorber in a sleeving manner and is connected with the other end of the guide pipe. The
infrared temperature sensor is electrically connected with the airborne
avionics system and is fixed to the annular heat dissipation medium injection pipe
assembly. The battery is detachably mounted on the heat dissipation medium storage tank. By means of the device, the problems that when an aircraft lands, the temperature of the shock absorber is too high and the working performance is greatly reduced can be solved to a certain degree, the safety of
aircraft landing is improved, and the device is simple and compact in structure, convenient to use and easy to manufacture and produce.