IPC분류정보
국가/구분 |
United States(US) Patent
등록
|
국제특허분류(IPC7판) |
|
출원번호 |
US-0035856
(2002-01-04)
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발명자
/ 주소 |
|
대리인 / 주소 |
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인용정보 |
피인용 횟수 :
2 인용 특허 :
10 |
초록
▼
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 position
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.
대표청구항
▼
1. 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 tubes includ
1. 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 tubes including i) relatively larger cross-section tubes positioned chordwise of the airfoil, ii) relatively smaller cross-section positioners located to stabilize said relatively larger cross-section tubes, d) including propulsion apparatus operatively connected to the airfoil, e) a frame to be propelled, f) and a tether or tethers connecting the airfoil to the frame, g) and including propulsion apparatus operatively connected to the airfoil, h) and wherein said propulsion apparatus comprises at least one of the following: i) a propeller and a drive therefore, ii) a rocket, i) a ground surface engaging wheel or wheels and a drive therefore, j) and including a selection mechanism carried by the frame to enable operator selection of drive activation to the wheel or wheels, or drive actuation to the propeller, or rocket. 2. 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 tubes including i) relatively larger cross-section tubes positioned chordwise of the airfoil, ii) relatively smaller cross-section positioners located to stabilize said relatively larger cross-section tubes, d) and including propulsion apparatus operatively connected to the airfoil, e) and wherein said propulsion apparatus comprises i) a frame and a ground engaging wheel or wheels carried by the frame, and a drive therefore carried by the frame, ii) a propeller and a drive therefore carried by the frame, iii) tethers connecting the airfoil to the frame, f) and including a selection mechanism carried by the frame to enable operator selection of drive activation to the wheel or wheels, or drive actuation to the propeller. 3. 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 tubes including i) relatively larger cross-section tubes positioned chordwise of the airfoil, ii) relatively smaller cross-section positioners located to stabilize said relatively larger cross-section tubes, d) and including propulsion apparatus operatively connected to the airfoil, e) and wherein said propulsion apparatus comprises at least one of the following: i) a propeller and a drive therefore, ii) a rocket, f) a ground surface engaging wheel or wheels and a drive therefore, g) and including selection mechanism carried by the frame to enable operator selection of drive activation to the wheel or wheels, or drive actuation to the propeller, or rocket. 4. The combination of claim 3 wherein said mechanism includes a clutch carried by a sprocket via which drive is selectively transmitted via a chain or chains.
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