Arrangements for mounting a probe on an aircraft

Details Arrangements for mounting a probe on an aircraft Arrangements for mounting a probe on an aircraft

1981-10-23

1984-01-31

Basinger, S. D.

Aeronautics and astronautics

Miscellaneous

244 45A, 2441291, 244131, 73182, B64D 4700, B64C 3912

Patent

active

044285493

ABSTRACT:
An aircraft 10 includes a pair of aerodynamic control members 11 pivotally mounted one to each side of the cockpit, each for movement about a pivotal axis P. A probe 13 is carried adjacent the outboard end of each control member in a predetermined orientation by fixed support means 25 anchored to the aircraft body and extending through the aerodynamic control member 11 adjacent the pivotal axis P. By this arrangement, the probe 13 remains in its predetermined orientation with respect to the aircraft irrespective of the angular disposition of the control member. The probe may be an air-data probe.

REFERENCES:
patent: 2246510 (1941-06-01), Diehl
patent: 2430793 (1947-11-01), Wells
patent: 3222926 (1965-12-01), Carver
patent: 3318146 (1967-05-01), DeLea et al.
patent: 3666209 (1972-05-01), Taylor

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