Matches 1 - 11 out of 11
Match Document Document Title
6253126 Method and apparatus for flight parameter monitoring and control  
Methods and apparatus are disclosed for three-dimensional flight control based generally upon measuring and comparing actual air pressures at or near various surfaces of an aircraft during flight....
6002972 Method and apparatus for measuring forces based upon differential pressure between surfaces of an aircraft  
A method and 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...
5796612 Method for flight parameter monitoring and control  
The present invention relates to a method for three-dimensional flight control based generally upon measuring and comparing actual air pressures at or near various surfaces of an aircraft during...
5737222 Apparatus for measuring lift forces based upon differential pressure between surfaces of an aircraft  
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...
5457630 System for onboard lift analysis and apparatus therefor  
A method and 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...
5088665 Serrated trailing edges for improving lift and drag characteristics of lifting surfaces  
An improvement in the lift and drag characteristics of a lifting surface is achieved by attaching a serrated panel to the trailing edge of the lifting surface. The serrations may have a saw-tooth...
4598886 Double parasol, favorable interference airplane  
An aircraft intended to fly at supersonic Mach mnumbers is disclosed. The aircraft utilizes a double parasol wing arrangement, with a power plant nacelle located under the wing on each side of the...
4542868 Trailing edge device for an airfoil  
The invention is a small wedge shaped flap (20) for attachment to or near the trailing edge (14) of a airfoil (10) which improves the coefficient of lift and reduces the coefficient of drag...
4483497 Wide-body supersonic aircraft  
This invention is an improvement of my system for supersonic aircraft which provides the required angular momentum reaction to the continuous generation of new lift circulation by vorticity in lieu...
4291853 Airplane all-moving airfoil with moment reducing apex  
Disclosed is an airplane all-moving airfoil having a moment reducing apex for facilitating control of the airfoil. In a preferred embodiment, the apex protrudes forward from the leading edge of an...
4067518 Drag reducer for lift surface of aircraft  
One or more aerodynamic bodies of preselected shape and placement are employed on the lower surface of an aircraft wing or other aerodynamic lifting surface for the purpose of reducing its drag....
Matches 1 - 11 out of 11