Apparatus for measuring lift forces based upon differential pres

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364427, 36442406, 364424016, 36455101, 244 121, 244201, 244203, 340959, 340967, 73178R, 73178T, 180116, 180117, G06G 776, B64C 1500

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057372225

ABSTRACT:
An apparatus for measuring the lift generated by airfoils of an aircraft. This real-time analysis is accomplished by measuring a differential pressure between the upper and lower lift surfaces of the airfoils. The apparatus a) measures an actual differential pressure between the upper and lower lift surfaces for a given aircraft speed, b) transmits this actual differential pressure measurement to a computer, c) compares the actual differential pressure measurement with an optimal pressure differential for the same aircraft speed, and d) evaluates performance of the aircraft based on the result of the comparison. The apparatus comprises a fixed array of differential pressure sensor mechanisms for measuring actual pressure differentials and a computer for comparing optimal differential pressure measurements to the actual differential pressure measurements. Each sensor mechanism preferably contains a piezoelectric sensor that communicates with the upper and lower lift surfaces.

REFERENCES:
patent: 2601962 (1952-07-01), Douglas
patent: 2744698 (1956-05-01), Baynes
patent: 2950879 (1960-08-01), Smith
patent: 3142457 (1964-07-01), Quenzler
patent: 3646811 (1972-03-01), DeLeo et al.
patent: 3691356 (1972-09-01), Miller
patent: 4110605 (1978-08-01), Miller
patent: 4122522 (1978-10-01), Smith
patent: 4194707 (1980-03-01), Sharpe
patent: 4202518 (1980-05-01), Burnham et al.
patent: 4490802 (1984-12-01), Miller
patent: 4516124 (1985-05-01), Shannon et al.
patent: 4586140 (1986-04-01), Millen
patent: 4728951 (1988-03-01), Johnson et al.
patent: 4775118 (1988-10-01), Daniels
patent: 4837695 (1989-06-01), Baldwin
patent: 4843554 (1989-06-01), Middleton et al.
patent: 4886224 (1989-12-01), Joy
patent: 4899284 (1990-02-01), Lewis et al.
patent: 4936142 (1990-06-01), Davidson
patent: 4980833 (1990-12-01), Milligan et al.
patent: 5016837 (1991-05-01), Willis
patent: 5047942 (1991-09-01), Middleton et al.
patent: 5071088 (1991-12-01), Betts
patent: 5082207 (1992-01-01), Tulinius
patent: 5083279 (1992-01-01), Burdoin
patent: 5103224 (1992-04-01), Arad
patent: 5186415 (1993-02-01), Li
patent: 5191791 (1993-03-01), Gerardi et al.
patent: 5275358 (1994-01-01), Goldhammer et al.
AIAA AIAA-94-0800 Effect of Initial Ice Roughness on Airfoil Aerodynamics, M. Bragg et al., 32nd Aerospace Sciences Meeting and Exhibit, Jan. 10-13, 1994, pp. 1-19.
Maximum Lift Degradation Due to Wing Upper Surface Contamination, Walter O. Valarezo, Nov. 1993, Montreal, Canada.
Journal of Aircraft, Sep.-Oct. 1993, vol. 30, No. 5, pp. 689-694.
AIAA AIAA-93-3534 Navier-Stokes Applications to High-Lift Airfoil Analysis, W.O. Valarezo et al., AIAA 11th Applied Aerodynamics Conference, Aug. 9-11, 1993, pp. 1-12.
AIAA AIAA-93-3136 Topics in High-Lift Aerodynamics, Walter O. Valarezo, AIAA 24th Fluid Dynamics Conference, Jul. 6-9, 1993, pp. 1-15.
AIAA AIAA-92-0401 Maximum Lift Prediction for Multielement Wings, W.O. Valarezo et al., 30th Aerospace Sciences Meeting and Exhibit, Jan. 6-9, 1992, pp. 1-13.

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