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US 6,659,403 B2Granted
Inflatable airfoils, and elevated and propulsion driven vehicles
OwnerChih-Yu Hsiainventor
Life of this patent
Estimating the term…
Abstract
An aeronautical apparatus, the combination comprising a primary airfoil having at least one panel which is an upper panel, a lower panel, and multiple gas containing tubes associated with the airfoil and extending lengthwise thereof, the tubes including relatively larger cross-section tubes positioned chordwise of the airfoil, and relatively smaller cross-section positioners located to stabilize the relatively larger cross-section tubes.
Claims5
In an aeronautical apparatus, the combination comprising
- a) a primary airfoil, having at least one panel which is one of the following:
- i) an upper panel
- ii) a lower panel,
- b) multiple gas containing tubes associated with the airfoil and extending lengthwise thereof,
- c) said airfoil having opposite ends, and including chordwise extending structures at said opposite ends and connected to one or more of the following:
- i) the upper panel
- ii) the lower panel
- iii) ends of the tubes,
- d) said structures projecting generally forwardly of a line defined by the generally lengthwise extending leading edge of the airfoil, and said structures also projecting generally rearwardly of a line defined by the generally lengthwise extending trailing edge of the airfoil,
- e) there being a flight control surface located rearwardly of the airfoil and extending transversely relative to said structures, said flight control surface being one of the following:
- i) a panel or panels
- ii) a secondary airfoil or airfoils,
- f) and including tethers supported by said primary airfoil and by said flight control surface.
10 more elements
In an aeronautical apparatus, the combination comprising
- a) a primary airfoil, having at least one panel which is one of the following:
- i) an upper panel
- ii) a lower panel,
- b) multiple gas containing tubes associated with the associated with the airfoil and extending lengthwise thereof,
- c) said airfoil having opposite ends, and including chordwise extending structures at said opposite ends and connected to one or more of the following:
- i) the upper panel
- ii) the lower panel
- iii) ends of the tubes,
- d) said structures projecting generally forwardly of a line defined by the generally lengthwise extending leading edge of the airfoil, and said structures also projecting generally rearwardly of a line defined by the generally lengthwise extending trailing edge of the airfoil,
- e) flight control surface or surfaces located rearwardly of the airfoil and extending transversely relative to said structures,
- f) and including controls operatively connected to said control panel or panels to controllably tilt same.
8 more elements
Dependencies are inferred from the claim text.