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1. 发明授权

CN1030978C 翼型伞盖飞机失效
公开(公告)号：CN1030978C
公开(公告)日：1996-02-14
申请号：CN92108825.6
申请日：1992-06-30
申请人：史蒂芬·L·斯奈德
发明人：史蒂芬·L·斯奈德
IPC分类号： B64C39/00 , B64D17/00
CPC分类号： B64C31/036 , Y10S244/902 , Y10S244/903 , Y10S244/904
摘要：一种无线电控制的飞机，包括一个由电机(36)带动推进器(38)提供动力的机体(1)，在飞行中机体通过可转动地安装在飞机机身上的操纵控制杆(68)而被悬挂，操纵控制杆有连接于负载悬挂吊索(3，5，6)的下端的外端(12，14)，负载悬挂吊索的上端与冲压空气充气式的柔性翼形伞盖部分(2)相连。飞机的操纵是通过控制杆(68)的转动调节负载悬挂吊索并由此调节伞盖表面。在机身内装有一个无线电接收机(112)，用来控制驱动电机(36)速度。飞机由一个控制飞机的转向和速度的遥控发射机控制。

2. 发明公开

CN1073146A 机翼型伞盖式飞机失效
公开(公告)号：CN1073146A
公开(公告)日：1993-06-16
申请号：CN92108825.6
申请日：1992-06-30
申请人：史蒂芬·L·斯奈德
发明人：史蒂芬·L·斯奈德
IPC分类号： B64C39/00 , B64D17/00
CPC分类号： B64C31/036 , Y10S244/902 , Y10S244/903 , Y10S244/904
摘要：一种无线电控制的飞机，包括一个由电机(36)带动推进器(38)提供动力的机体(1)，在飞行中机体通过可转动地安装在飞机机身上的操纵控制杆(68)而被悬挂，操纵控制杆有连接于负载悬挂吊索(3，5，6)的下端的外端(12，14)，负载悬挂吊索的上端与冲压空气充气式的柔性机翼型伞盖部分(2)相连。飞机的操纵是通过控制杆(68)的转动调节负载悬挂吊索并由此调节伞盖表面。在机身内装有一个无线电接收机(112)，用来控制驱动电机(36)速度。飞机由一个控制飞机的转向和速度的摇控发射机控制。

3. 发明公开

EP0592593A1 AIRFOIL CANOPY AIRCRAFT 失效
标题翻译：降落伞的翅膀飞行大队。
公开(公告)号：EP0592593A1
公开(公告)日：1994-04-20
申请号：EP92915577.0
申请日：1992-07-01
申请人： SNYDER, Stephen, L.
发明人： SNYDER, Stephen, L.
IPC分类号： B64C31
CPC分类号： B64C31/036 , Y10S244/902 , Y10S244/903 , Y10S244/904
摘要： Aéronef télécommandé comprenant un engin (1) actionné par un moteur électrique (36) commandant une hélice propulsive (38). L'engin est suspendu en vol par une tige de commande de direction (68) montée rotative sur le corps de l'engin et possédant des extrémités extérieures (12, 14) reliées aux extrémités inférieures de câble de supension de charge (3, 5, 6) reliés par leurs extrémités supérieures à une aile souple (2) constituée par une voilure à plan de sustentation de type gonflable par air sous pression dynamique. La direction de l'aéronef s'effectue au moyen du déplacement rotatif de la tige de commande (68), afin de manipuler les câbles de suspension de charge et, de ce fait, les surfaces de la voilure. Le corps de l'engin loge un récepteur radio (112) agissant sur la vitesse du moteur de transmission (36), ainsi qu'un moteur de direction (98) accouplé à la tige de commande (68) par l'intermédiaire d'un système d'accouplement approprié. Une batterie (104) est montée de façon amovible dans le corps de l'engin et sert à alimenter électriquement le récepteur et les moteurs. L'aéronef est piloté au moyen d'un émetteur à distance commandant sa direction et sa vitesse.

4. 发明申请

WO1993001087A1 AIRFOIL CANOPY AIRCRAFT 审中-公开
标题翻译： AIRFOIL CANOPY飞机
公开(公告)号：WO1993001087A1
公开(公告)日：1993-01-21
申请号：PCT/US1992005474
申请日：1992-07-01
申请人： SNYDER, Stephen, L.
IPC分类号： B64C39/00
CPC分类号： B64C31/036 , Y10S244/902 , Y10S244/903 , Y10S244/904
摘要： A radio controlled aircraft comprises a vehicle (1) powered by an electric motor (36) driving propeller (38) as a pusher type. The vehicle is suspended in flight by a steering control rod (68) pivotally mounted to the body of the vehicle having outer ends (12, 14) connected to the lower ends of load suspension lines (3, 5, 6) connected at their upper ends to a flexible wing portion (2) of a ram air inflatable type of airfoil canopy. Steering of the aircraft is by pivotal movement of control rod (68) to manipulate the load suspension lines and thereby the canopy surfaces. The vehicle body houses a radio receiver (112) for operating the speed of the drive motor (36) and a steering drive motor (98) coupled to the control rod (68) by a suitable linkage system. Battery pack (104) is removably mounted in the body for providing power to the receiver and motors therein. The aircraft is controlled by a remote transmitter which controls the steering and speed of the aircraft.

5. 发明申请

WO01046009A1 SMALL-SIZE RADIO-CONTROLLED FLYING DEVICE 审中-公开
标题翻译：小型无线遥控飞行器
公开(公告)号：WO01046009A1
公开(公告)日：2001-06-28
申请号：PCT/FR2000/003618
申请日：2000-12-20
IPC分类号： A63H27/08 , A63H30/04 , B64C31/036 , B64C39/02 , B64D47/08
CPC分类号： A63H27/08 , A63H30/04 , B64C2201/086 , B64C2201/105 , B64C2201/107 , B64C2201/127 , B64C2201/165 , B64C2201/187 , Y10S244/902 , Y10S244/903
摘要： The invention concerns a small-size radio-controlled flying device propelled by a heat engine (20) with pusher propeller (10) for remote sensing, said device enabling short take-off and landing and a maximum flying speed of 34 Km/h. The device comprises a nacelle and a wing system, the nacelle (1) being a rigid three-wheeled carriage capable of being disassembled by denesting a more or less pyramidal jig with rear base (2) and front top (7), a lower plane (3) two lateral planes (4, 5) and an upper plane (6), the base being a single-piece welded element and comprising the engine, the propeller, a tank and the remote sensing unit, the top being a single-piece welded element, the lower plane and the two lateral planes comprising side members (11, 12) at least assembled at the base and at the top, the lower plane comprising at its three end angles two rear wheels (8) and a front wheel (9), the front wheel being arranged overlapping forward in the top and the wheels being low pressure tyres, the wing system (13) being a wing box flexible parafoil, said wing system being linked to the nacelle adjustable by two front suspension cables (17), two braking suspension cables (18) acting on the two flaps/wings.
摘要翻译：本发明涉及一种由具有用于遥感的推进推进器（10）的热机（20）推进的小型无线电控制飞行装置，所述装置能够进行短时起飞和着陆，并且最大飞行速度为34公里/小时。该装置包括机舱和机翼系统，所述机舱（1）是刚性三轮车架，其能够通过使后座（2）和前顶（7）破坏或多或少的金字塔夹具而被拆卸，下平面（3）两个横向平面（4,5）和上平面（6），底座是单件焊接元件，包括发动机，螺旋桨，油箱和遥感单元，所述下平面和所述两个横向平面包括至少组装在所述基部和顶部处的侧部构件（11,12），所述下平面在其三个端角处包括两个后轮（8）和前轮（9），所述前轮在顶部布置成向前，所述车轮是低压轮胎，所述机翼系统（13）是翼盒柔性parafoil，所述翼系统与所述机舱连接，所述机舱可由两个前悬挂缆索 17），两个制动悬挂电缆（18）作用在两个翼/翼上。

6. 发明专利

JP3745754B2 Small unmanned airplane 有权
公开(公告)号：JP3745754B2
公开(公告)日：2006-02-15
申请号：JP2003299869
申请日：2003-08-25
申请人：正人岡本 , 川田工業株式会社
发明人：正人岡本 , 千晴戸塚 , 安忠田辺 , 剛史赤坂
IPC分类号： B64C39/10 , B64C39/02
CPC分类号： A63H27/02 , B64C39/028 , B64C39/10 , B64C2201/028 , B64C2201/141 , B64C2201/146 , B64C2201/165 , Y10S244/903

7. 发明授权

EP1242279B1 APPAREIL VOLANT RADIOCOMMANDE DE TAILLE REDUITE 有权
标题翻译：内置小型遥控飞机
公开(公告)号：EP1242279B1
公开(公告)日：2004-01-07
申请号：EP00990085.3
申请日：2000-12-20
申请人： Institut de Recherche pour le Développement ( IRD)
发明人： ASSELINE, Jean , DE NONI, George
IPC分类号： B64C39/02 , B64C31/036 , B64D47/08
CPC分类号： A63H27/08 , A63H30/04 , B64C2201/086 , B64C2201/105 , B64C2201/107 , B64C2201/127 , B64C2201/165 , B64C2201/187 , Y10S244/902 , Y10S244/903
摘要： The invention concerns a small-size radio-controlled flying device propelled by a heat engine (20) with pusher propeller (10) for remote sensing, said device enabling short take-off and landing and a maximum flying speed of 34 Km/h. The device comprises a nacelle and a wing system, the nacelle (1) being a rigid three-wheeled carriage capable of being disassembled by denesting a more or less pyramidal jig with rear base (2) and front top (7), a lower plane (3) two lateral planes (4, 5) and an upper plane (6), the base being a single-piece welded element and comprising the engine, the propeller, a tank and the remote sensing unit, the top being a single-piece welded element, the lower plane and the two lateral planes comprising side members (11, 12) at least assembled at the base and at the top, the lower plane comprising at its three end angles two rear wheels (8) and a front wheel (9), the front wheel being arranged overlapping forward in the top and the wheels being low pressure tyres, the wing system (13) being a wing box flexible parafoil, said wing system being linked to the nacelle adjustable by two front suspension cables (17), two braking suspension cables (18) acting on the two flaps/wings.

8. 发明公开

EP1242279A1 APPAREIL VOLANT RADIOCOMMANDE DE TAILLE REDUITE 有权
标题翻译：内置小型遥控飞机
公开(公告)号：EP1242279A1
公开(公告)日：2002-09-25
申请号：EP00990085.3
申请日：2000-12-20
申请人： Institut de Recherche pour le Développement ( IRD)
发明人： ASSELINE, Jean , DE NONI, George
IPC分类号： B64C39/02 , B64C31/036 , B64D47/08
CPC分类号： A63H27/08 , A63H30/04 , B64C2201/086 , B64C2201/105 , B64C2201/107 , B64C2201/127 , B64C2201/165 , B64C2201/187 , Y10S244/902 , Y10S244/903
摘要： The invention concerns a small-size radio-controlled flying device propelled by a heat engine (20) with pusher propeller (10) for remote sensing, said device enabling short take-off and landing and a maximum flying speed of 34 Km/h. The device comprises a nacelle and a wing system, the nacelle (1) being a rigid three-wheeled carriage capable of being disassembled by denesting a more or less pyramidal jig with rear base (2) and front top (7), a lower plane (3) two lateral planes (4, 5) and an upper plane (6), the base being a single-piece welded element and comprising the engine, the propeller, a tank and the remote sensing unit, the top being a single-piece welded element, the lower plane and the two lateral planes comprising side members (11, 12) at least assembled at the base and at the top, the lower plane comprising at its three end angles two rear wheels (8) and a front wheel (9), the front wheel being arranged overlapping forward in the top and the wheels being low pressure tyres, the wing system (13) being a wing box flexible parafoil, said wing system being linked to the nacelle adjustable by two front suspension cables (17), two braking suspension cables (18) acting on the two flaps/wings.

9. 发明公开

EP0592593A4 AIRFOIL CANOPY AIRCRAFT 失效
公开(公告)号：EP0592593A4
公开(公告)日：1994-09-07
申请号：EP92915577
申请日：1992-07-01
申请人： SNYDER, STEPHEN, L.
发明人： SNYDER STEPHEN L
IPC分类号： B64C31/036 , B64C39/00
CPC分类号： B64C31/036 , Y10S244/902 , Y10S244/903 , Y10S244/904

10. 发明公开

EP1590239A4 AUTOMATED CARGO TRANSPORTATION SYSTEM 有权
标题翻译： AUTOMATED货运系统
公开(公告)号：EP1590239A4
公开(公告)日：2011-06-15
申请号：EP04701733
申请日：2004-01-13
申请人： BOXAIR ENGINEERING LLC
发明人： STUPAKIS JOHN S
IPC分类号： B64C39/02 , B64C1/00
CPC分类号： B64C39/024 , B64C39/02 , B64C2201/048 , B64C2201/086 , B64C2201/104 , B64C2201/128 , B64C2201/141 , B64C2201/165 , B64C2201/187 , B64C2211/00 , B64D2011/0046 , Y10S244/903

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