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1. 发明授权

US09283490B1 Device for stabilising a flying attitude of a remote-controlled fixed-wing aircraft 有权
标题翻译：用于稳定遥控固定翼飞机的飞行姿态的装置
公开(公告)号：US09283490B1
公开(公告)日：2016-03-15
申请号：US14017952
申请日：2013-09-04
申请人： Richard Deutsch
发明人： Richard Deutsch
IPC分类号： G05D1/12 , A63H27/00 , A63H27/26 , G05D1/08 , G05D1/02
CPC分类号： A63H27/02 , A63H27/06 , A63H30/04 , B64C2203/00 , G05D1/0033 , G05D1/0204 , G05D1/0816
摘要： The invention relates to a method for adjusting parameters in a stabilizing device (4) for stabilizing a flying attitude of a remote-controlled fixed-wing aircraft. To adjust a first parameter for a first axis, a first adjustment signal is transmitted from the transmitter (1) to the stabilizing device (4). The first parameter (P1) is stored during the flight as a result of a first memory signal transmitted from the transmitter (1). A second parameter (P2) for a second axis is then adjusted and stored in a similar manner.
摘要翻译：本发明涉及一种用于调整稳定装置（4）中用于稳定遥控固定翼飞行器的飞行姿态的参数的方法。为了调整第一轴的第一参数，第一调整信号从发射器（1）传输到稳定装置（4）。作为从发射机（1）发送的第一存储器信号的结果，第一参数（P1）在飞行期间被存储。然后以类似的方式调整和存储第二轴的第二参数（P2）。

2. 发明授权

US08998669B2 Method and apparatus for a two-stage model rocket 有权
标题翻译：两阶段模型火箭的方法和装置
公开(公告)号：US08998669B2
公开(公告)日：2015-04-07
申请号：US13920793
申请日：2013-06-18
申请人： Estes-Cox Corp.
发明人： John G. Boren
IPC分类号： A63H27/26
CPC分类号： A63H27/06 , A63H27/005
摘要： A reconfigurable model rocket that can be flown either in a single-stage or a two-stage configuration is disclosed. The model rocket has a main body tube, a nose cone, a first tail section, a second tail section, and a staging adapter. The nose cone is removably coupleable to a top end of the main body tube and the first tail section is removably coupleable to a bottom end of the main body tube. The first tail section accommodates a first rocket engine to propel the model rocket by allowing gases from a combustible propellant to escape from the bottom end of the first tail section. The second tail section is removably coupleable to a bottom end of the first tail section and accommodates a second rocket engine to propel the model rocket by allowing gases from a combustible propellant to escape from the bottom end of the second tail section.
摘要翻译：公开了可以以单级或两级配置流动的可重构模型火箭。模型火箭具有主体管，鼻锥，第一尾部，第二尾部和分段适配器。鼻锥可拆卸地联接到主体管的顶端，并且第一尾部可拆卸地联接到主体管的底端。第一尾部容纳第一火箭发动机以通过允许来自可燃推进剂的气体从第一尾部的底端逸出来推动模型火箭。第二尾部可拆卸地联接到第一尾部的底端，并容纳第二火箭发动机以通过允许来自可燃推进剂的气体从第二尾部的底端逸出来推动模型火箭。

3. 发明申请

US20090137181A1 Toy plane powered by hydraulic power 审中-公开
标题翻译：玩具飞机由液压动力供电
公开(公告)号：US20090137181A1
公开(公告)日：2009-05-28
申请号：US11987143
申请日：2007-11-28
申请人： Ping-Sung Chang
发明人： Ping-Sung Chang
IPC分类号： A63H27/26
CPC分类号： A63H27/005 , A63H27/02 , A63H27/06
摘要： A toy plane includes a body made by light material such as polylone and a pressurized container is securely engaged with a groove defined in an underside of the body. The pressurized container includes a closed front end and a nozzle which connected to a rear end of the pressurized container. Water and pressurized air are received in the pressurized container. The wings and stabilizers on the body are well secured by any known method so that they do not separated from the body when the pressurized container releases the pressure to launch the plane.
摘要翻译：玩具平面包括由诸如多边形的轻质材料制成的主体，并且加压容器与限定在身体的下侧中的凹槽牢固地接合。加压容器包括封闭的前端和连接到加压容器的后端的喷嘴。水和加压空气被容纳在加压容器中。身体上的机翼和稳定器通过任何已知的方法很好地固定，使得当加压容器释放压力以发射飞机时，它们不与身体分离。

4. 发明授权

US4685289A Power plant for model jet aircraft 失效
标题翻译：喷气式飞机发电厂
公开(公告)号：US4685289A
公开(公告)日：1987-08-11
申请号：US797922
申请日：1985-11-14
申请人： Robert S. Violett , W. Lee Anderson
发明人： Robert S. Violett , W. Lee Anderson
IPC分类号： A63H27/26 , F02B75/02 , F02B75/34 , F02K5/02 , F02M9/08 , A63H27/06
CPC分类号： F02B75/34 , A63H27/06 , F02K5/02 , F02M9/085 , F02B2075/025
摘要： A ducted fan type model aircraft power plant having a mounting for a one cylinder internal combustion model aircraft engine. The preferred engine utilized a special vertically oriented carburetor. A duct is supported by a set of stators having an aerodynamic shape for straightening airflow through the duct. A fan having seven identical individual replaceable blades is disposed at the front of the duct and directly driven by the engine. One stator is adapted to essentially enclose the vertical carburetor and to smoothly direct the airflow from the fan around the carburetor to the engine cylinder for cooling. The stator has an opening to the carburetor air inlet for providing air under pressure thereto. The stator shapes cooperate with the duct and aft fairings of the power plant to deliver a smooth airstream having a uniform non-turbulent flow to produce a maximum propulsive efficiency.
摘要翻译：具有用于单缸内燃模型飞机发动机的安装件的管道式风扇型模型飞机发电厂。优选的发动机使用特殊的垂直定向化油器。管道由具有空气动力学形状的一组定子支撑，用于矫正通过管道的气流。具有七个相同的单独可替换叶片的风扇设置在管道的前部并由发动机直接驱动。一个定子适于基本上包围垂直化油器并且平滑地将气流从化油器周围的风扇引导到发动机气缸以进行冷却。定子具有通向化油器空气入口的开口，用于在其上提供空气。定子形状与发电厂的管道和后整流罩配合以输送具有均匀非湍流的平滑气流，以产生最大的推进效率。

5. 发明授权

US4573937A Jet propelled model airplane 失效
标题翻译：喷气推进模型飞机
公开(公告)号：US4573937A
公开(公告)日：1986-03-04
申请号：US632388
申请日：1984-07-19
申请人： Victor Stanzel
发明人： Victor Stanzel
IPC分类号： A63H27/04 , A63H27/26
CPC分类号： A63H27/04 , A63H27/06
摘要： A line-controlled, centrifugal fan, jet-propelled model airplane is disclosed in which the impeller of a fan contained within the fuselage of the aircraft is driven from a remote drive unit by an elongated flexible cable contained within a flexible sheath. The impeller rotates about an axis perpendicular to the longitudinal axis of the airplane and is driven in a direction of rotation tending to rotate the airplane about its lateral axis in a nose-up direction, due to the frictional contact of the compressed air between the rotating impeller and the housing of the centrifugal fan mounted within the fuselage. A flywheel powered by the electric motor in the remote drive unit controls the rate of acceleration and deceleration of the aircraft as an electric motor in the drive unit is switched on and off.
摘要翻译：公开了一种线路控制的离心式风扇，喷气推进型飞机，其中包含在飞行器的机身内的风扇的叶轮由远程驱动单元通过包含在柔性护套内的细长柔性电缆驱动。叶轮围绕垂直于飞机的纵向轴线的轴线旋转，并且在旋转方向上被驱动，倾向于使飞机围绕其横向轴线在向上的方向上旋转，这是由于压缩空气在旋转叶轮和安装在机身内的离心风机壳体。由远程驱动单元中的电动机供电的飞轮控制飞行器的加速和减速速率，因为驱动单元中的电动马达被打开和关闭。

6. 发明授权

US3943656A Two stage rocket with pressure responsive means for frictionally engaging second stage 失效
标题翻译：具有压力响应装置的两级火箭，用于摩擦接合第二级
公开(公告)号：US3943656A
公开(公告)日：1976-03-16
申请号：US454088
申请日：1974-03-25
申请人： Charles J. Green
发明人： Charles J. Green
IPC分类号： A63H27/26 , F42B15/36 , A63H27/06
CPC分类号： F42B15/36 , A63H27/06
摘要： A toy rocket has a motor receptacle designed to receive a rocket motor of the type fueled by a self-pressurizing liquid propellant. The rocket motor during the fueling operation has its nozzle seated in a launcher through which liquid propellant flows into the propellant cavity of the rocket motor. When the propellant cavity of the rocket motor is pressurized, a member responsive to propellant pressure in the rocket motor engages a portion of the walls of the motor receptacle in the rocket body. When the pressure responsive member releases the receptacle walls, relative motion is provided between at least a portion of the rocket body and the rocket motor. For example, in one embodiment of the toy rocket, a second stage portion of the rocket is spring-biased away from a first stage portion of the rocket body. The major section of the rocket motor is fixed to the first stage portion. The pressure responsive member on the rocket motor engages the second stage portion while the rocket motor contains propellant to prevent separation of the first and second stages. When the propellant is expended, the pressure responsive member releases the second stage, allowing separation of the second stage from the first stage. A parachute is then deployed from the second stage to brake the descent of the rocket.
摘要翻译：玩具火箭具有设计成接收由自加压液体推进剂燃料类型的火箭发动机的马达插座。加油操作期间的火箭发动机的喷嘴位于发射器中，液体推进剂通过该喷射器流入火箭发动机的推进剂腔。当火箭发动机的推进剂腔被加压时，响应于火箭发动机中的推进剂压力的构件与火箭弹体中马达容座的壁的一部分接合。当压力响应构件释放容器壁时，在火箭主体的至少一部分与火箭发动机之间提供相对运动。例如，在玩具火箭的一个实施例中，火箭的第二台部分被弹簧偏压远离火箭主体的第一台部分。火箭发动机的主要部分固定在第一阶段部分。火箭发动机上的压力响应构件接合第二级部分，而火箭发动机包含推进剂以防止第一级和第二级的分离。当推进剂消耗时，压力响应构件释放第二级，允许第二级与第一级分离。然后从第二阶段部署降落伞来制动火箭的下降。

7. 发明授权

US3700172A Reaction powered toy flying craft 失效
标题翻译：反应动力玩具飞机
公开(公告)号：US3700172A
公开(公告)日：1972-10-24
申请号：US3700172D
申请日：1971-09-09
申请人： JAMES P GALLEGOS SR
发明人： GALLEGOS JAMES P SR
IPC分类号： A63H27/26 , B05B3/18 , B05B3/00
CPC分类号： A63H27/06 , B05B3/18
摘要： A toy craft which is lifted aloft by water jet means. This device includes internal tubes directed to spray nozzles on the underside of the craft and the rate of flow of the water is controlled by valve means and a control box which is placed on the ground and is connected to a water faucet.
摘要翻译：用喷水器高空举起的玩具。该装置包括指向工艺底面上的喷嘴的内管，并且水的流量由阀装置控制，并且控制箱被放置在地面上并连接到水龙头。

8. 发明授权

US3080676A Jet propelled model aircraft 失效
标题翻译：喷气推进模型飞机
公开(公告)号：US3080676A
公开(公告)日：1963-03-12
申请号：US79440159
申请日：1959-02-19
申请人： VICTOR STANZEL
发明人： VICTOR STANZEL
IPC分类号： A63H27/04 , A63H27/26
CPC分类号： A63H27/04 , A63H27/06

9. 发明授权

US2545586A Toy jet vehicle 失效
标题翻译：玩具喷气车
公开(公告)号：US2545586A
公开(公告)日：1951-03-20
申请号：US65766346
申请日：1946-03-28
申请人： POLLAK MANFRED J
发明人： POLLAK MANFRED J
IPC分类号： A63H27/26
CPC分类号： A63H27/06

10. 发明授权

US2505526A Inflated elastic body within another inflated elastic body 失效
标题翻译：另一个充气弹性体内充气的弹性体
公开(公告)号：US2505526A
公开(公告)日：1950-04-25
申请号：US78039347
申请日：1947-10-17
申请人： LOUIS COSTEA
发明人： LOUIS COSTEA
IPC分类号： A63H27/26
CPC分类号： A63H27/06

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