Self-separation protective sleeve for airspeed tube of civil aircraft
A technology of civil aircraft and pitot tubes, applied in instruments, fluid velocity measurement, velocity/acceleration/shock measurement, etc., can solve problems such as safety accidents, pitot tube blockage, pitot tube not working properly, etc., to ensure normal operation Work, the effect of eliminating potential safety hazards
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[0030] The technical solution of this patent will be further described in detail below in conjunction with specific embodiments.
[0031] Embodiments of the present patent are described in detail below, examples of which are shown in the drawings, wherein the same or similar reference numerals designate the same or similar elements or elements having the same or similar functions throughout. The embodiments described below by referring to the figures are exemplary and are only used for explaining the patent, and should not be construed as limiting the patent.
[0032] see figure 1 , this embodiment provides a civil aircraft pitot tube self-separation protective cover, including a pipe 10, a first elastic member 20, an extension head 30, a snap-fit part 40 and a driving part 70, and the side wall of the pipe 10 is provided with an inlet An air port, a baffle 101 is movable in the air inlet, one end of the first elastic member 20 is connected with the inner wall of the pipeli...
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