Aerodynamic probe internal constructions

Details Aerodynamic probe internal constructions Aerodynamic probe internal constructions

G - Physics

01

C

G01C 21/00 (2006.01) G01F 1/46 (2006.01) G01L 19/00 (2006.01) G01P 5/165 (2006.01)

Patent

CA 2069110

PCT/US90/06567 ABSTRACT OF THE DISCLOSURE A short, strut-mounted, multifunction air data sensing probe (20) providing reduced drag, weight and radial cross section has a modular internal construction providing a multiple passageway pressure assembly (35) to transfer sensed pressure signals from individual sensing ports (25,31,32) on a probe barrel (21) to pressure carrying conduits (57,62,66,73,74) extending into the mounting strut (30) of the probe (20). The modular construction eliminates the need for having interior chambers made by fixing a series of difficult to locate bulkheads on the probe interior, with separate lines running from each of the chambers to provide the pressure signal from each of the ports. The modular construction also permits mounting a deicing heater (95) on internal parts other than the outer probe shell so that the manufacture of the probe (20) is further simplified, and the types of material used for the probe shell (21) can be changed without concern about heater mounting.

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