公开(公告)号：WO2014053057A1

公开(公告)日：2014-04-10

申请号：PCT/CA2013/000846

申请日：2013-10-04

Applicant: SKYKAR INC. ,  LENG, Marcus

Inventor： LENG, Marcus

IPC: B64D27/24 ,  B64C27/22 ,  B64C27/28 ,  B64C29/00 ,  B64C39/08

CPC classification number: B64C27/26 ,  B60L11/1805 ,  B60L11/1859 ,  B60L11/1861 ,  B64C1/26 ,  B64C11/46 ,  B64C15/02 ,  B64C29/00 ,  B64C29/0025 ,  B64C29/02 ,  B64C39/026 ,  B64D17/00 ,  B64D27/24 ,  B64D31/12 ,  B64D33/08

Abstract: An aerial vehicle includes at least one wing, a plurality of thrust producing elements on the at least one wing, a plurality of electric motors equal to the number of thrust producing elements for individually driving each of the thrust producing elements, at least one battery for providing power to the motors, and a flight control system to control the operation of the vehicle. The aerial vehicle may include a fuselage configuration to facilitate takeoffs and landings in horizontal, vertical and transient orientations, redundant control and thrust elements to improve reliability and means of controlling the orientation stability of the vehicle in low power and multiple loss of propulsion system situations. Method of flying an aerial vehicle includes the variation of the rotational speed of the thrust producing elements to achieve active vehicle control.

Abstract translation: 飞行器包括至少一个机翼，在所述至少一个机翼上的多个推力产生元件，多个电动马达等于用于单独驱动每个所述推力产生元件的推力产生元件的数量，至少一个用于 向电动机供电，以及用于控制车辆操作的飞行控制系统。 飞行器可以包括机身配置，以便于在水平，垂直和瞬态取向中的起飞和着陆，冗余控制和推力元件以提高可靠性，并且在低功率和多功率推进系统情况下，控制车辆的定向稳定性。 飞行器的飞行方法包括推力产生元件的旋转速度的变化，以实现主动的车辆控制。

公开(公告)号：WO2010138229A3

公开(公告)日：2011-02-17

申请号：PCT/US2010026465

申请日：2010-03-08

Applicant: SIKORSKY AIRCRAFT CORP ,  TONI DARRYL M ,  MCCARTHY MARY ,  BARR BRUCE H ,  STOBIECKI ANTHONY Z ,  SWIFT THOMAS ,  DZIEKONSKI THOMAS

Inventor： TONI DARRYL M ,  MCCARTHY MARY ,  BARR BRUCE H ,  STOBIECKI ANTHONY Z ,  SWIFT THOMAS ,  DZIEKONSKI THOMAS

IPC: B64D1/22 ,  B64C1/20 ,  B64C27/22 ,  B64D9/00

CPC classification number: B64C27/14 ,  B64C1/061 ,  B64C27/06 ,  B64D1/22

Abstract: An external hook system for a rotary-wing aircraft includes a lower frame interface which accommodates longitudinal and lateral loads and an upper frame interface. A tension member is mountable between the lower frame interface and the upper frame interface to transfer tension loads between the lower frame interface and the upper frame interface.

Abstract translation: 用于旋转翼飞行器的外部钩系统包括容纳纵向和横向载荷的下部框架接口以及上部框架接口。 张紧构件可安装在下框架接口和上框架接口之间，以在下框架接口和上框架接口之间传递张力负荷。

公开(公告)号：WO2010104509A1

公开(公告)日：2010-09-16

申请号：PCT/US2009/036889

申请日：2009-03-12

Applicant: BELL HELICOPTER TEXTRON INC. ,  COLLINS, Bob ,  STAMPS, Frank, B. ,  CORRINGAN, John, J. III ,  DREIER, Mark, E.

Inventor： COLLINS, Bob ,  STAMPS, Frank, B. ,  CORRINGAN, John, J. III ,  DREIER, Mark, E.

IPC: B64C27/22

CPC classification number: B64C29/0033

Abstract: A tiltrotor aircraft includes a rotatable nacelle that supports a rotor assembly and is pivotally attached to the aircraft's fuselage. A wing extension attaches to an outboard section of the nacelle. The wing extension provides additional yaw control during helicopter mode and additional lift during airplane mode. A method for controlling at least a portion of yaw movement includes positioning the rotor assembly in helicopter mode, creating rotor wash with the rotor assembly, and pivotally rotating the wing extension in the rotor wash.

Abstract translation: 倾斜旋转飞机包括支撑转子组件并可枢转地附接到飞机机身的可旋转机舱。 机翼延伸部连接到机舱的外侧部分。 机翼延伸在直升机模式下提供额外的偏航控制，并在飞机模式期间提供额外的提升。 用于控制偏转运动的至少一部分的方法包括将转子组件定位成直升机模式，与转子组件一起产生转子清洗，以及在转子清洗器中枢转地旋转机翼延伸部。

公开(公告)号：WO2008045011A3

公开(公告)日：2009-03-12

申请号：PCT/US2006019388

申请日：2006-05-19

Applicant: BELL HELICOPTER TEXTRON INC ,  RAUBER RICHARD ,  STAMPS FRANK B ,  BRASWELL JAMES LEE JR

Inventor： RAUBER RICHARD ,  STAMPS FRANK B ,  BRASWELL JAMES LEE JR

IPC: B64C27/22

CPC classification number: B64C27/41 ,  B64C27/52 ,  B64C29/0033 ,  F16C1/04

Abstract: A constant-velocity drive system for a rotary-wing aircraft rotor comprising a differential torque-splitting mechanism and a gimbal mechanism is disclosed. A rotary-wing aircraft having a rotary-wing aircraft rotor comprising a differential torque- splitting mechanism and a gimbal mechanism is disclosed.

Abstract translation: 公开了一种用于包括差动扭矩分离机构和万向节机构的旋翼飞机转子的恒速驱动系统。 公开了一种旋转翼飞行器，其具有包括差动扭矩分离机构和万向节机构的旋翼飞行器转子。

公开(公告)号：WO2008147451A2

公开(公告)日：2008-12-04

申请号：PCT/US2007/084397

申请日：2007-11-12

Applicant: SIKORSKY AIRCRAFT CORPORATION ,  COTTON, Bryan S. ,  ARIFIAN, Kenneth C. ,  SCHWEIZER, Leslie ,  CEVETTE, Jeffrey L.

Inventor： COTTON, Bryan S. ,  ARIFIAN, Kenneth C. ,  SCHWEIZER, Leslie ,  CEVETTE, Jeffrey L.

IPC: B64C27/22 ,  B64C27/12 ,  B64C11/38

CPC classification number: B64C27/10 ,  B64C11/38 ,  B64C27/14 ,  B64C2027/8236 ,  B64C2027/8254

Abstract: A translational thrust system for a high speed rotary-wing aircraft includes a propeller system driven by a propeller gearbox, a hydraulic system, and a mechanical-hydraulic control system. The mechanical-hydraulic control system utilizes a hydraulic fluid which travels to and from a propeller dome via an oil transfer/position feedback tube which translates with a propeller pitch change piston. Translation of the oil transfer/position feedback tube and the propeller pitch change piston pitches the blades between high (coarse) and low (fine) pitch positions.

Abstract translation: 用于高速旋翼飞机的平移推力系统包括由螺旋桨变速箱，液压系统和机械液压控制系统驱动的螺旋桨系统。 机械液压控制系统利用一个液压流体，该液压流体经由与螺旋桨变桨活塞平移的油传递/位置反馈管行进和往返于螺旋桨穹顶。 油传递/位置反馈管和螺旋桨螺距改变活塞的转换在高（粗）和低（精细）间距位置之间调节叶片。

公开(公告)号：WO2008118131A1

公开(公告)日：2008-10-02

申请号：PCT/US2007/018108

申请日：2007-08-14

Applicant: KAREM, Abe

Inventor： KAREM, Abe

IPC: B64C27/22

CPC classification number: B64C29/0033 ,  B64C27/08 ,  B64C27/26

Abstract: A rotorcraft having multiple rotors, and wings that provide lift in forward flight, has mechanical coupling between rotors that can be disengaged and optionally reengaged, during flight. The coupling can, which can prevent a failure of one rotor from interfering with rotation of the other rotor(s), can be accomplished using many different types of devices, including for example, dog clutches and friction clutches, and collapsible clutches. Disengagement can range from being completely under control of an operator, to partially under operator control, to completely automatic. Among many other benefits, designing, manufacturing, fitting, retrofitting or in some other manner providing an aircraft with a device that can disengage rotation of one of the rotors from that of another one of the rotors during flight can be used to improving survivability in an emergency situation.

Abstract translation: 具有多个转子的旋翼飞行器以及在向前飞行中提供升力的机翼具有转子之间的机械耦合，该转子在飞行期间可以分离并且可选地重新啮合。 可以使用许多不同类型的装置（包括例如爪形离合器和摩擦离合器以及可折叠的离合器）来实现能够防止一个转子干扰另一个（多个）转子旋转的联接。 脱离范围可以从完全在操作员的控制下，部分在操作员控制下，到完全自动化。 在许多其他优点中，设计，制造，安装，改装或以某种其他方式为飞机提供能够在飞行期间使转子中的一个与另一个转子的旋转脱离的装置可用于提高飞行器中的生存性 紧急情况。

公开(公告)号：WO2007130109A2

公开(公告)日：2007-11-15

申请号：PCT/US2006/030806

申请日：2006-08-07

Applicant: RAYTHEON COMPANY ,  MEREMS, Paul, A. ,  HILL, Randy, W.

Inventor： MEREMS, Paul, A. ,  HILL, Randy, W.

IPC: B64C27/22

CPC classification number: B64D1/02 ,  B64D19/02

Abstract: In various representative aspects, an airborne delivery system according to various aspects of the present invention comprises a container and an autorotating rotor system. The container may contain contents, and the rotor system facilitates control of at least a portion of the flight of the airborne system and the descent. Exemplary features may include a guidance system, for example to guide and control the airborne system, and a wing for gliding.

Abstract translation: 在各种代表性方面，根据本发明的各个方面的机载传送系统包括容器和自转转子系统。 容器可以包含内容物，并且转子系统便于控制机载系统和下降的至少一部分飞行。 示例性特征可以包括引导系统，例如引导和控制机载系统，以及用于滑行的机翼。

公开(公告)号：WO2007108794A1

公开(公告)日：2007-09-27

申请号：PCT/US2006/009965

申请日：2006-03-20

Applicant: BOSTAN, Nicolae

Inventor： BOSTAN, Nicolae

IPC: B64C27/22

CPC classification number: B64C39/024

Abstract: A vertical takeoff and landing (VTOL) air vehicle disclosed. The air vehicle can be manned or unmanned. In one embodiment, the air vehicle includes two shrouded propellers (202), a fuselage (201) and a gyroscopic stabilization disk installed in the fuselage. The gyroscopic stabilization disk can be configured to provide sufficient angular momentum, by sufficient mass and/or sufficient angular velocity, such that the air vehicle is gyroscopically stabilized during various phases of flight. In one embodiment the fuselage is fixedly attached to the shrouded propellers. In another embodiment, the shrouded propellers are pivotably mounted to the fuselage.

Abstract translation: 一架垂直起降（VTOL）的空中客车。 机动车可以载人或无人驾驶。 在一个实施例中，空中交通工具包括安装在机身中的两个被覆盖的螺旋桨（202），机身（201）和陀螺仪稳定盘。 陀螺稳定盘可以被配置成通过足够的质量和/或足够的角速度来提供足够的角动量，使得在飞行的各个阶段期间航空器的陀螺仪稳定。 在一个实施例中，机身固定地附接到被覆盖的螺旋桨。 在另一个实施例中，被覆盖的螺旋桨可枢转地安装在机身上。

公开(公告)号：WO2007106137A1

公开(公告)日：2007-09-20

申请号：PCT/US2006/037440

申请日：2006-09-26

Applicant: INFORMATION SYSTEMS LABORATORIES, INC.

Inventor： SULLIVAN, Callum, R.

IPC: B64C27/22

CPC classification number: B64C39/005

Abstract: A cycloidal propulsion unit for controlling a thrust vector includes a hub that rotates about a hub axis. Further, the unit includes an airfoil blade pivotally mounted on the hub along a blade axis parallel to the hub axis. As a result, the blade may pivot about the blade axis while traveling along a blade path during rotation of the hub. The unit further includes a ring that rotates around a ring axis parallel to the hub axis. The ring is interconnected with the blade via a control rod. Also, a device is engaged with the ring to selectively position the ring axis relative to the hub axis. As a result of these structures, selective positioning of the ring axis provides control of the rotation of the blade about the blade axis as the blade travels along the blade path.

Abstract translation: 用于控制推力矢量的摆线推进单元包括围绕轮毂轴线旋转的轮毂。 此外，该单元包括沿着平行于轮毂轴线的叶片轴线枢转地安装在轮毂上的翼型叶片。 结果，当轮毂旋转期间，叶片可绕刀片轴线枢转，同时沿叶片路径行进。 该单元还包括围绕平行于轮毂轴线的环轴线旋转的环。 环通过控制杆与刀片相互连接。 此外，装置与环接合以选择性地相对于轮毂轴线定位环轴线。 作为这些结构的结果，当叶片沿着叶片路径行进时，环轴的选择性定位提供叶片围绕叶片轴线的旋转的控制。

公开(公告)号：WO2005014391A8

公开(公告)日：2005-04-14

申请号：PCT/RU2004000250

申请日：2004-06-29

Applicant: DEMIN ALEXSANDR PAVLOVICH ,  DEMIN SERGEI ALEXANDROVICH

Inventor： DEMIN ALEXSANDR PAVLOVICH ,  DEMIN SERGEI ALEXANDROVICH

IPC: B64C27/22 ,  B64C27/28 ,  B64C29/00 ,  B64C31/024 ,  B64D27/06

CPC classification number: B64C27/28 ,  B64C29/0033 ,  B64C31/024 ,  B64D27/06

Abstract: The invention relates to multipurpose heavier-than-air aircrafts which can be used in the form of an airplane, helicopter or a sailplane. The inventive multipurpose heavier-than-air aircraft consists of a body comprising a tail assembly which is provided with a rudder, a pitch control surface and a chassis. A lifting forwardswept wing is fixed to the centre wing section of the body. A slotted opening closed with shutters is embodied in the top section of the body, wherein a driving engine used for sailplane mode and provided with a thrust propeller fixed to the shaft thereof is arranged. Said driving engine is cinematically connected to a carriage displacement drive by means of a main strut displacing mechanism. The carriage is provided with the position lock thereof corresponding to airplane, helicopter and sailplane flight modes. The carriage displacement drive is connected to an asymmetrical lever displacement mechanism. The major arm of said asymmetrical lever and an auxiliary strut are pivotally connected to the driving engine. Said auxiliary strut is pivotally connected to the rockshaft of the asymmetrical lever my means of a mechanism.

Abstract translation: 本发明涉及可以以飞机，直升机或滑翔机的形式使用的多用途重型飞机。 本发明的多用途重型飞机由包括尾部组件的主体组成，尾部组件设置有方向舵，俯仰控制表面和底盘。 抬起的前卫翼固定在身体的中心翼部分。 具有快门的开槽开口体现在主体的顶部，其中设置有用于帆板模式的驱动引擎，并且设置有固定在其轴上的推力推进器。 所述驱动发动机通过主支柱移位机构电动连接到滑架移动驱动装置。 滑架具有对应于飞机，直升机和帆板飞行模式的位置锁定。 滑架位移驱动器连接到不对称的杠杆位移机构。 所述不对称杆和辅助支柱的主臂枢转地连接到驱动发动机。 所述辅助支柱枢转地连接到不对称杠杆的轴心，其机构的装置。