Light buzzard-type wing jet plane and its use

Light buzzard-type wing jet plane and its use

  • CN 1,435,355 B
  • Filed: 12/04/2002
  • Issued: 01/12/2011
  • Est. Priority Date: 12/04/2002
  • Status: Active Grant
First Claim
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1. light-duty buzzard-type wing jet supersonic plane, adopt the both sides air inlet, single-shot list vertical fin, tricycle landing gear, canard adds the aerodynamic arrangement of buzzard-type wing low coverage coupling, adopt modular design, it comprises the head module that is installed on the integrated wing body module, the cabin module, machine back of the body module, the tail module, the wing tip module, the vertical fin module, described integrated wing body module is by the inlet channel fuselage girder (57) of holding concurrently, wing front-axle beam (58) and integrated wing body fuel tank (67) constitute, it is characterized in that:

  • described inlet channel hold concurrently fuselage girder (57) be the inlet channel of aircraft be again the body longeron of aircraft, replace the trusses of general aircraft to add the airframe structure of bulkhead with the inlet channel tubular beams;

    Described wing front-axle beam (58) is one and runs through fuselage and from the inlet channel tubular beams that fuselage girder (57) top passes through of holding concurrently, the leading edge of the shape of cross section of wing front-axle beam (58) outer panel sweep part and the buzzard-type wing of wing matches;

    The main landing gear of described tricycle landing gear (18) is positioned at integrated wing body fuel tank (67) afterwards, nose-gear (17) is positioned at the position between aviator'"'"'s two legs of sitting cabin (13), because main landing gear places integrated wing body fuel tank (67) afterwards, and the load that makes nose-gear bear the 25%-30% of aircraft gross weight surpasses the load of the 8%-20% that general aircraft nose wheel bears;

    Described canard (12) is positioned at sits cabin (13) before.

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