Infrared sensing air vehicle

Infrared sensing air vehicle

  • CN 202,128,908 U
  • Filed: 06/03/2011
  • Issued: 02/01/2012
  • Est. Priority Date: 06/03/2011
  • Status: Active Grant
First Claim
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1. infrared induction aircraft is characterized in that comprising:

  • Be provided with the aircraft base (1) of infrared induction assembly (3);

    Be arranged at the power plant module (4) in the aircraft base (1);

    AndCoaxial and go to upper and lower two screw assemblies (2) of position relation each other;

    Be positioned at said aircraft base (1) top jointly;

    And respectively through two with one heart and the power plant module (4) in first, second rotating shaft that is set-located each other (51,52) and the aircraft base (1) be connected;

    According to power plant module (4) rotary power is provided, passes to two screw assemblies (2) respectively by first, second rotating shaft (51,52) and realize rotation;

    WhereinThe direction of rotation of said two screw assemblies (2) is opposite.

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