FLIGHT MEASURING AIR PARAMETERS SYSTEM Russian patent published in 2006 - IPC G01P5/14 G01P13/02 B64D43/02 

FIELD: the invention refers to the field of aviation and particular to definition of flight air parameters of flying vehicles.

SUBSTANCE: the arrangement has receivers of air pressures with receiving openings provided with an electro heating and anti-icing system connected with the aid of pneumatic routes with pressure sensors, temperature sensors of external air and calculator of flight parameters. At that all blocks are located in a single special aerodynamically stream-lined frame fastened to the flying vehicle and composed of elements of axial symmetric bodies which are fulfilled in the shape of a cone, an ellipsoid, a cylinder, a pyramid. At that the arrangement is autonomous and is connected with the flying vehicle only through channels of transferring of information and supply of electric energy through electric joints. The technical result is contained in securing of autonomy of the system, reducing preparation time for the flight in case of determination of availability of refuse of the system, simplification of the construction of the heating system of receivers of air pressures, reducing weight of the system of measuring air parameters in the whole, reducing labor capacity and cost and also simplification of adaptation of the system to the changed external construction of the fuselage of the flying vehicle or to another flying vehicle. Expansion of working diapason measuring parameters of the flight right up to attack angles of -180ξ≤α≤180°^° and sliding -180ξ≤β≤180^ξ that is along the whole sphere.

EFFECT: efficient measuring air parameters.

13 cl, 19 dwg