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公开(公告)号：US5372337A
公开(公告)日：1994-12-13
申请号：US877210
申请日：1992-05-01
Applicant: Robert W. Kress , Joseph W. Stump
Inventor： Robert W. Kress , Joseph W. Stump
CPC classification number: B64C29/005 , B64C15/12 , B64C39/024 , B64C2201/048 , B64C2201/088 , B64C2201/104 , B64C2201/167
Abstract: An unmanned aerial vehicle incorporates a single engine with bifurcated exhausts which are coupled to side mounted rotating nozzles through a swivel joint. Jet deflection means are mounted to the end of the rotating nozzles to achieve additional degrees of freedom for the aircraft.
Abstract translation: 无人驾驶飞行器包括具有分叉排气的单个发动机，其通过旋转接头联接到侧面安装的旋转喷嘴。 喷射偏转装置安装到旋转喷嘴的端部以实现飞行器的额外的自由度。
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公开(公告)号：US4198779A
公开(公告)日：1980-04-22
申请号：US916343
申请日：1978-06-19
Applicant: Robert W. Kress
Inventor： Robert W. Kress
Abstract: A multi-propeller propulsion system for model aircraft having a single engine and positive driving connections between the engine and each of the multiplicity of propellers. The positive drive may include toothed pulleys and serrated belts and gearing for example.
Abstract translation: 用于模型飞机的多推进器推进系统具有单个发动机，并且在发动机和多个螺旋桨中的每一个之间具有正的驱动连接。 正向驱动器可以包括例如齿形皮带轮和锯齿形皮带以及传动装置。
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公开(公告)号：US5308023A
公开(公告)日：1994-05-03
申请号：US14760
申请日：1993-02-08
Applicant: Robert W. Kress
Inventor： Robert W. Kress
IPC: B64C25/10
CPC classification number: B64C25/10
Abstract: A control member is rotatably mounted on the fuselage or on the wing of a model aircraft in spaced relation with a supporting surface of the fuselage. A gear leg is supported at one end by the control member and supports a landing wheel at its spaced opposite end. The gear leg extends radially of the control member. A torsion spring is coaxially mounted with the control member for storing energy when the control member is in a position whereby the gear leg is fully extended for ground operations and for releasing stored energy to rotate the control member in a manner whereby the gear leg is retracted for flying operations. A gear retracting initiator coupled to the torsion spring initiates gear retraction. An extend lock locks the gear leg in its fully extended position. A retract lock locks the gear leg in its retracted position. An actuator in operative proximity with the extend lock and the retract lock assists in locking the gear leg in its fully extended position and assists in locking the gear leg in its retracted position.
Abstract translation: 控制构件可旋转地安装在与机身的支撑表面间隔开的模型飞机的机身上或机翼上。 齿轮在一端由控制构件支撑，并在其隔开的相对端处支撑着陆车轮。 齿轮支脚沿控制构件的径向延伸。 扭转弹簧与控制构件同轴地安装，当控制构件处于一个位置时，用于存储能量，由此齿轮腿完全延伸用于地面操作并释放存储的能量以使齿轮支腿缩回的方式旋转控制构件 用于飞行操作。 联接到扭转弹簧的齿轮回缩起动器启动齿轮收回。 延伸锁将齿轮支脚锁定在其完全伸出位置。 缩回锁将齿轮锁定在缩回位置。 与延伸锁和缩回锁可操作地邻近的致动器有助于将齿轮锁定在其完全伸出位置，并有助于将齿轮锁定在其缩回位置。
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公开(公告)号：US4726545A
公开(公告)日：1988-02-23
申请号：US936862
申请日：1986-12-02
Applicant: Robert W. Kress
Inventor： Robert W. Kress
CPC classification number: B64C29/005
Abstract: By mounting a lift engine and a lift/cruise engine closely to the center of gravity of an aircraft and by orienting the respective engines such that the thrust axes thereof are arranged for ensuring that the vector sum of the lift engine thrust and the lift/cruise engine thrust pass through the center of gravity at all times, a fuel efficient aircraft can controllably takeoff and land vertically. To provide for vectoring the thrust of the respective engines, different nozzles are provided. Further, to provide for pitch, roll and yaw control, a vane assembly is coupled to the aircraft in such a way that it remains in alignment to the jet stream of the lift engine.
Abstract translation: 通过将提升发动机和升降机/巡航发动机紧密地安装在飞行器的重心上，并且通过使相应的发动机定向，使得它们的推力轴被布置成确保提升发动机推力和升力/巡航的矢量和 发动机推力始终通过重心，燃油效率高的飞机可以可控地起飞和垂直着陆。 为了提供对各个发动机的推力的矢量化，提供了不同的喷嘴。 此外，为了提供俯仰，滚转和偏航控制，叶片组件以这样的方式联接到飞行器，使得其保持与升降机发动机的喷流对准。
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公开(公告)号：US4443014A
公开(公告)日：1984-04-17
申请号：US287365
申请日：1981-07-27
Applicant: Bernard Kovit , Richard G. Koenig , Robert W. Kress
Inventor： Bernard Kovit , Richard G. Koenig , Robert W. Kress
Abstract: A device adaptable to inexpensive models to operate either in a mode of being attacked or an attack mode that permits sequential shooting of energy within a predetermined angle profile and, within range limits, the receipt of such energy whereupon visual indication of a successful attack can be indicated.
Abstract translation: 适于廉价模型的装置可以以被攻击的模式或允许在预定角度轮廓内顺序拍摄能量并且在范围限制内接收这种能量的攻击模式来操作，于是成功攻击的视觉指示可以是 指出。
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Patent Agency Ranking
公开(公告)号：US4296896A
公开(公告)日：1981-10-27
申请号：US70260
申请日：1979-08-27
Applicant: Robert W. Kress , Anthony C. Bacchi
Inventor： Robert W. Kress , Anthony C. Bacchi
CPC classification number: B64C29/0075
Abstract: A VTOL airplane having a stub wing integrating a powerplant to either side of an airplane fuselage to rotatably relate the powerplant means to the airplane fuselage for uniform rotation, allow for flexible interconnecting design and lower the use of gravitational and aerodynamic moments in assistance of rotation of this powerplant/stub wing assembly.
Abstract translation: 垂直起降飞机具有将动力装置整合到飞机机身的任一侧的短叉翼，以将动力装置装置可旋转地联接到飞机机身以进行均匀旋转，允许灵活的互连设计，并降低重力和空气动力矩的使用以协助旋转 这个动力装置/桩架组件。
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公开(公告)号：US5131605A
公开(公告)日：1992-07-21
申请号：US713504
申请日：1991-06-12
Applicant: Robert W. Kress
Inventor： Robert W. Kress
CPC classification number: B64C29/0075 , B64C15/12
Abstract: A VTOL aircraft has a first engine nacelle mounted under the wing on one side of the fuselage and houses two of the aircraft engines. The first engine nacelle is mounted in close proximity with the fuselage. A second engine nacelle is mounted under the wing on the opposite side of the fuselage from the first nacelle and houses the remaining two engines. The second engine nacelle is mounted in close proximity with the fuselage. The first and second nacelles are movable from positions parallel to the wing for normal flight to positions perpendicular to the wing for vertical flight. Each of the first and second engine nacelles has inlets and nozzles and each of the first and second nacelles is angled in a manner whereby its nozzles are closer to the fuselage than its inlets. First control vanes extend aft of the nozzles of, and are movable with, the first engine nacelle and second control vanes extend aft of the nozzles of, and are movable with, the second engine nacelle. Each of the first and second vanes include vertical vanes normally aligned with the thrust vector centerlines.
Abstract translation: 一架VTOL飞机有一个第一发动机舱，安装在机身的一侧，位于机身的一侧，并装有两架飞机发动机。 第一台发动机舱安装在机身附近。 第二发动机舱安装在机翼的机翼的下方，与机身的第一机舱相反，并容纳剩下的两台发动机。 第二台发动机舱安装在机身附近。 第一和第二机舱可从平行于机翼的位置移动，以便正常飞行，垂直于机翼垂直飞行。 第一和第二发动机舱中的每个具有入口和喷嘴，并且第一和第二发动机舱中的每一个以其入口比其入口更靠近机身的方式成角度。 第一控制叶片延伸在第一发动机舱的喷嘴的后面并且可移动，并且第二控制叶片延伸在第二发动机舱的喷嘴的后面并且可与第二发动机机舱移动。 第一和第二叶片中的每一个包括通常与推力矢量中心线对齐的垂直叶片。
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公开(公告)号：US5119935A
公开(公告)日：1992-06-09
申请号：US647347
申请日：1991-01-29
Applicant: Joseph W. Stump , Robert W. Kress , Robert C. Powers
Inventor： Joseph W. Stump , Robert W. Kress , Robert C. Powers
CPC classification number: B64F5/0036 , B64F1/22 , B64F1/36
Abstract: A metal container stores a VTOL aircraft during shipment to a sea vessel or large vehicle where it then functions as a portable weather-tight hangar which can be secured in available deck space. When on board a ship's deck, the walls of the container unfold so that the structure may be converted to a take-off and landing pad that provides an exhaust system for the hot lift engine gases that eliminates the hazard to ship's crew, prevents heat damage to the deck and eliminates "suck down" effects characteristic of certain VTOL aircraft configurations. Triangular panels are removably secured together to form the cover of the container; and when unfolded and flattened, these panels are inserted in the corners of the unfolded structure so as to extend the heat shield.
Abstract translation: 金属集装箱在运输到海运船只或大型车辆期间存放垂直起降飞机，然后起作为便携式防风雨机库的作用，可以将其固定在可用的甲板空间。 当在船的甲板上时，容器的壁展开，使得结构可以转换成起飞和着陆垫，其为热提升发动机气体提供排气系统，消除对船员的危害，防止热损伤 并消除了某些“垂直起降”飞机配置特征的“吸”效应。 三角板可拆卸地固定在一起以形成容器的盖子; 并且当展开和展平时，将这些面板插入展开结构的角部以便延伸隔热板。
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公开(公告)号：US3966142A
公开(公告)日：1976-06-29
申请号：US556095
申请日：1975-03-06
Applicant: Marshall J. Corbett , Robert W. Kress
Inventor： Marshall J. Corbett , Robert W. Kress
CPC classification number: B64C1/30 , B64C29/0075
Abstract: A Vertical Takeoff and Landing (VTOL) aircraft that has a small stowage envelope made possible by articulation of the aircraft empennage and fuselage, the aircraft having propulsion units capable of providing in all attitudes of the empennage with respect to said fuselage engine wash of the empennage thereby insuring aircraft control without additional reaction stabilizing units.
Abstract translation: 具有小载重信号的垂直起飞和着陆（垂直起降）飞机使飞机尾翼和机身成为可能，具有推进装置的飞机能够在尾翼的所有姿态中提供尾翼的机身引擎清洗 从而保证飞机的控制无需额外的反应稳定装置。
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公开(公告)号：US3949095A
公开(公告)日：1976-04-06
申请号：US487047
申请日：1974-07-10
Applicant: Michael Pelehach , Robert W. Kress , Rolf J. Larson
Inventor： Michael Pelehach , Robert W. Kress , Rolf J. Larson
CPC classification number: F24J2/0472 , E04H4/129 , Y02E10/44
Abstract: A solar heating device for swimming pools comprising an inflatable raft having a thermally reflective bottom surface and a thermally transparent top surface, and means for elevating at least a fraction of said reflective surface above the swimming pool surface during periods of diminished solar radiation to reduce heat loss from the water. One raft is generally small enough to be easily handled and a plurality of rafts may be required to cover a substantial part of the water surface. The number of rafts required is variable and provides a measure of flexibility to the rate of heating, i.e., by providing more rafts in spring and fall and perhaps none in mid-summer.
Abstract translation: 一种用于游泳池的太阳能加热装置，包括具有热反射底表面和热透明顶表面的可充气筏，以及用于在太阳辐射减少期间将游泳池表面上方的所述反射表面的至少一部分升高以降低热量的装置 从水中流失 一个木筏通常足够小以容易地处理，并且可能需要多个筏来覆盖水面的大部分。 所需的木筏数量是可变的，并且提供了对加热速率的灵活性的度量，即通过在春季和秋季提供更多的筏子，或者在夏季可能没有。
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