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    • 1. 发明授权
    • Jet propelled model vehicle
    • 喷气机型号车辆
    • US3664056A
    • 1972-05-23
    • US3664056D
    • 1970-08-07
    • VICTOR STANZEL
    • STANZEL VICTOR
    • A63H27/00
    • A63H27/005
    • A model or toy vehicle of the jet propelled type employing a rapidly vaporizing liquid propellant of the chlorofluoromethane type, commonly known as Freon. The vehicle may be of the airplane or rocket type, and includes a barrel for holding a charge of the propellant which is allowed to vaporize and is discharged through a jet at the rear end of the barrel. Means is provided for allowing the escape of air and the bleeding off of vapor during the charging of the barrel with liquid propellant preliminary to the launching of the craft.
    • 使用快速蒸发的氯氟甲烷型液体推进剂(通常称为氟利昂)的喷射推进型的模型或玩具车辆。 车辆可以是飞机或火箭类型,并且包括用于保持推进剂的装料的桶,其被允许蒸发并通过筒的后端处的喷嘴排出。 提供了用于在用液体推进剂对筒进行装料之前允许空气逸出和蒸汽渗出的装置,以初步推动该工艺。
    • 2. 发明授权
    • Jet-propelled model airplane
    • 喷气式推进型飞机
    • US4133139A
    • 1979-01-09
    • US796541
    • 1977-05-13
    • Victor Stanzel
    • Victor Stanzel
    • A63H27/04A63H27/26A63H27/06
    • A63H27/04A63H27/06
    • 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. This abstract is not to be construed in any way to define or limit the invention set forth below.
    • 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。 本摘要不得以任何方式解释为限定或限制下文阐述的发明。
    • 5. 发明授权
    • Control and power mechanism for model aircraft
    • 模型飞机的控制和动力机制
    • US5709580A
    • 1998-01-20
    • US654300
    • 1996-05-28
    • Victor Stanzel
    • Victor Stanzel
    • A63H27/04
    • A63H27/04
    • An electrically powered model aircraft is disclosed in which an on-board electric motor is powered from a ground based electric storage battery. Flight attitude of the aircraft is controlled by torsion control system in which a torsion member is attached at one end to the aircraft and a tubular shaft is disposed about the torsion member, with one end of the tubular shaft being nonrotatably attached to the torsion member at a point spaced from the aircraft and the other end of the tubular shaft being nonrotatably attached to a control device on the aircraft adapted to be operated by rotation of the tubular shaft, to control operation of a control surface of the aircraft. A combination electrical connector and torsion control line extends between, and is releasably mechanically and electrically connected to, the aircraft and to a control handle carried by the airplane operator. Operation of the control handle by the aircraft operator exerts torsional forces on the control line which are transmitted to the torsion member on the aircraft, thereby causing rotation of the tubular shaft and control device, to control operation of the aircraft control surface. This abstract is not to be construed in any way to define or limit the invention set forth below.
    • 公开了一种电动型飞机,其中车载电动机由地基蓄电池供电。 飞机的飞行姿态由扭转控制系统控制,其中扭转构件的一端连接到飞行器,并且管状轴围绕扭转构件设置,管状轴的一端不可旋转地附接到扭转构件 与飞行器间隔开的点和管状轴的另一端不可转动地连接到飞机上的控制装置,其适于通过管状轴的旋转来操作,以控制飞行器的控制表面的操作。 组合电连接器和扭转控制线在飞行器之间延伸并且可释放地机械地和电气地连接到飞行器以及由飞机操作者携带的控制手柄。 由飞机操作者对操纵手柄的操作在控制线上施加扭转力,该扭力传递到飞行器上的扭转构件,从而引起管状轴和控制装置的旋转,以控制飞行器控制表面的操作。 本摘要不得以任何方式解释为限定或限制下文阐述的发明。
    • 6. 发明授权
    • Model aircraft
    • 模型飞机
    • US3991512A
    • 1976-11-16
    • US563673
    • 1975-03-31
    • Victor Stanzel
    • Victor Stanzel
    • A63H27/04A63H27/00
    • A63H27/04
    • A remotely powered and controlled aircraft is provided of the type wherein the propeller is driven from a remote drive unit by an elongated flexible cable confined within a flexible tube. The aircraft of the invention includes a secondary control knob slidably and rotatably mounted about the flexible tube for selectively controlling the effective length of the tube and cable to thereby control the radius of flight of the aircraft. In a preferred embodiment, the aircraft is a biplane with a unique wing support construction, including eyelets in the wings and flexible struts having wing engaging hooks thereon which may be selectively inserted through the eyelets for engagement with the wings. This abstract is not to be construed in any way to define or limit the invention set forth below.
    • 提供了一种远程供电和受控的飞机,其中螺旋桨由远程驱动单元由限制在柔性管内的细长柔性电缆驱动。 本发明的飞行器包括可旋转地安装在柔性管周围的次级控制旋钮,用于选择性地控制管和电缆的有效长度,从而控制飞行器的飞行半径。 在优选实施例中,飞行器是具有独特的翼支撑结构的双平面,其包括翅膀中的孔眼和在其上具有翼接合钩的柔性支柱,其可以选择性地插入通过孔眼以与翼接合。 本摘要不得以任何方式解释为限定或限制下文阐述的发明。