公开(公告)号：EP3107807A1

公开(公告)日：2016-12-28

申请号：EP15704564.2

申请日：2015-02-17

Applicant: IAT 21 Innovative Aeronautics Technologies GmbH

Inventor： SCHWAIGER, Meinhard

IPC: B64C3/38 ,  B64C3/56 ,  B64C29/00 ,  B64C39/00 ,  B64C39/02

CPC classification number: B64C29/0033 ,  B64C3/385 ,  B64C3/56 ,  B64C27/026 ,  B64C27/20 ,  B64C39/024 ,  B64C2201/027 ,  B64C2201/042 ,  B64C2201/044 ,  B64C2201/102 ,  B64C2201/108 ,  B64C2201/162 ,  B64D27/04 ,  B64D27/24 ,  B64D2027/026 ,  B64D2211/00

Abstract: The invention relates to an aircraft comprising a fuselage (1), a plurality of propeller units (3) that can pivot in relation to the fuselage (1), and wings (5) that can pivot at least partially in relation to the fuselage (1) and independently of the propeller units (3).

Abstract translation: 本发明涉及一种飞机，其包括机身（1），可相对于机身（1）枢转的多个螺旋桨单元（3）和能够相对于机身至少部分地枢转的翼（5） 1）并且独立于螺旋桨单元（3）。

公开(公告)号：EP2234876B1

公开(公告)日：2016-05-25

申请号：EP08768886.7

申请日：2008-01-31

Applicant: Raytheon Company

Inventor： SANDERSON, Terry, M. ,  CLARK, Jamie, W.

IPC: B64C3/38 ,  B64C3/54 ,  B64C3/56 ,  F42B10/14 ,  F42B10/20

CPC classification number: B64C3/54 ,  B64C3/56 ,  B64C2201/102 ,  F42B10/14 ,  F42B10/143 ,  F42B10/20 ,  Y02T50/14

Abstract: Methods and apparatus for systems having deployable elements according to various aspects of the present invention comprise a system including a deployable surface and an adaptive actuator including a polymer foam. In one embodiment, the system comprises a vehicle including a deployable wing comprising an exterior surface. The exterior surface may be adjusted by adjusting the shape, size, position, and/or orientation of the adaptive actuator.

公开(公告)号：EP2233393B1

公开(公告)日：2016-01-06

申请号：EP10157279.0

申请日：2010-03-23

Applicant: Schnoell, Gregor

Inventor： Schnoell, Gregor

IPC: B64C1/30 ,  B64C27/08 ,  B64C39/02 ,  A63H27/00

CPC classification number: B64C1/30 ,  A63H27/12 ,  B64C27/08 ,  B64C39/024 ,  B64C2201/027 ,  B64C2201/102 ,  B64C2201/108

公开(公告)号：EP2849996A4

公开(公告)日：2015-07-29

申请号：EP13790867

申请日：2013-04-04

Applicant: TEXTRON SYSTEMS CORP

Inventor： GUPTAA SUNEAL ,  BLEY JEREMY

IPC: B64C3/56

CPC classification number: B64C3/56 ,  B64C39/024 ,  B64C2201/102 ,  F42B10/16 ,  Y02T50/145

Abstract: An air vehicle, as well as a method for folding an air vehicle for storage, may include a fuselage and a wing connected to the fuselage. The wing may include two ends positioned opposite from each other, and the wing may be substantially perpendicular to the fuselage. At least one of the ends may define a space therebetween the fuselage and the wing. The space may be sized to receive a potion of the wing when the wing is wrapped around the fuselage.

Abstract translation: 一种空中飞行器以及用于折叠用于存储的空中车辆的方法可以包括机身和连接到机身的机翼。 机翼可以包括彼此相对定位的两个端部，并且机翼可以基本上垂直于机身。 端部中的至少一个可以在机身和机翼之间限定它们之间的空间。 当机翼围绕机身缠绕时，该空间的大小可以容纳翼的一部分。

公开(公告)号：EP2475575A4

公开(公告)日：2015-07-08

申请号：EP10833732

申请日：2010-09-09

Applicant: AEROVIRONMENT INC

Inventor： MIRALLES CARLOS THOMAS ,  PLUMB NICK ,  TAO TONY SHUO ,  OLSEN NATHAN

IPC: F42B15/01 ,  F41G7/00 ,  F41G7/22 ,  F41G9/00

CPC classification number: B64C13/28 ,  B64C3/44 ,  B64C3/50 ,  B64C3/56 ,  B64C5/12 ,  B64C9/02 ,  B64C9/08 ,  B64C9/18 ,  B64C11/00 ,  B64C13/18 ,  B64C39/024 ,  B64C2009/005 ,  B64C2201/021 ,  B64C2201/08 ,  B64C2201/102 ,  B64C2201/121 ,  B64C2201/14 ,  B64C2201/145 ,  B64C2201/146

Abstract: A system comprising an aerial vehicle or an unmanned aerial vehicle (UAV) (100, 400, 1000, 1500) configured to control pitch, roll, and/or yaw via airfoils (141, 142, 1345, 1346) having resiliently mounted trailing edges opposed by fuselage-house deflecting actuator horns (621, 622). Embodiments include one or more rudder elements (1045, 1046, 1145, 1146, 1245, 1345, 1346, 1445, 1446, 1545, 1546) which may be rotatably attached and actuated by an effector member (1049, 1149, 1249, 1349) disposed within the fuselage housing (1001) and extendible in part to engage the one or more rudder elements.

Abstract translation: 一种包括飞行器或无人驾驶飞行器（UAV）的系统，其被配置为经由具有弹性安装的后缘的机翼来控制俯仰，滚动和/或偏航，所述后翼与机身偏转致动器喇叭相对。 实施例包括一个或多个方向舵元件，其可以由设置在机身壳体内的效应器构件可旋转地附接和致动，并且部分地可部分地接合一个或多个舵元件。

公开(公告)号：EP2849996A1

公开(公告)日：2015-03-25

申请号：EP13790867.9

申请日：2013-04-04

Applicant: Textron Systems Corporation

Inventor： GUPTAA, Suneal ,  BLEY, Jeremy

IPC: B64C3/56

CPC classification number: B64C3/56 ,  B64C39/024 ,  B64C2201/102 ,  F42B10/16 ,  Y02T50/14

Abstract: An air vehicle, as well as a method for folding an air vehicle for storage, may include a fuselage and a wing connected to the fuselage. The wing may include two ends positioned opposite from each other, and the wing may be substantially perpendicular to the fuselage. At least one of the ends may define a space therebetween the fuselage and the wing. The space may be sized to receive a potion of the wing when the wing is wrapped around the fuselage.

Abstract translation: 飞行器以及用于折叠飞行器以进行存储的方法可以包括机身和连接到机身的机翼。 机翼可以包括彼此相对定位的两个端部，并且机翼可以基本垂直于机身。 至少一个端部可以在机身和机翼之间限定空间。 当机翼围绕机身缠绕时，该空间可以被设定尺寸以容纳机翼的一部分。

公开(公告)号：EP2814734A1

公开(公告)日：2014-12-24

申请号：EP13709050.2

申请日：2013-02-13

Applicant: Reiter, Johannes

Inventor： Reiter, Johannes

IPC: B64C29/02 ,  B64C39/02 ,  B64C29/00 ,  B64C39/00 ,  B64C27/16 ,  B64C27/18

CPC classification number: B64C27/00 ,  B64C3/385 ,  B64C27/001 ,  B64C27/16 ,  B64C27/18 ,  B64C29/00 ,  B64C29/0033 ,  B64C29/0075 ,  B64C29/02 ,  B64C39/008 ,  B64C39/024 ,  B64C2201/088 ,  B64C2201/102 ,  B64C2201/104 ,  B64C2201/108 ,  B64C2201/165

Abstract: The present invention relates to a device for generating aerodynamic lift and in particular an aircraft (100) for vertical take-off and landing. A wing arrangement (110) comprises at least one propulsion unit (111), wherein the propulsion unit (111) comprises a rotating mass which is rotatable around a rotary axis (117). The wing arrangement (110) is mounted to a fuselage (101) such that the wing arrangement (110) is tiltable around a longitudinal wing axis (112) of the wing arrangement (110) and such that the wing arrangement (110) is rotatable with respect to the fuselage (101) around a further rotary axis that differs to the longitudinal wing axis (112). An adjusting mechanism adjusts a tilting angle of the wing arrangement (110) around the longitudinal wing axis (112) under influence of a precession force (Fp) which forces the wing arrangement (110) to tilt around the longitudinal wing axis (112).

Abstract translation: 用于产生气动升力的装置技术领域本发明涉及一种用于产生气动升力的装置，尤其涉及一种用于垂直起飞和着陆的飞机（100）。 机翼装置（110）包括至少一个推进单元（111），其中推进单元（111）包括可围绕旋转轴线（117）旋转的旋转质量。 机翼装置（110）安装到机身（101），使得机翼装置（110）可围绕机翼装置（110）的纵向机翼轴线（112）倾斜并且使得机翼装置（110）可旋转 相对于机身（101）绕与纵向机翼轴线（112）不同的另一旋转轴线旋转。 调节机构在迫使机翼布置（110）围绕纵向机翼轴线（112）倾斜的进动力（Fp）的影响下调节机翼布置（110）围绕纵向机翼轴线（112）的倾斜角度。

公开(公告)号：EP2799332A2

公开(公告)日：2014-11-05

申请号：EP14002518.0

申请日：2005-04-14

Applicant: Arlton, Paul E. ,  Arlton, David J.

Inventor： Arlton, Paul E. ,  Arlton, David J.

IPC: B64C27/10 ,  B64C27/22 ,  B64C39/02

CPC classification number: B64C27/10 ,  B64C27/22 ,  B64C39/024 ,  B64C2201/027 ,  B64C2201/042 ,  B64C2201/082 ,  B64C2201/102 ,  B64C2201/108 ,  B64C2201/141 ,  B64C2201/146 ,  B64C2201/165 ,  B64C2201/201 ,  B64C2201/203 ,  B64C2201/205

Abstract: A rotary wing vehicle (1) includes a body structure having an elongated tubular backbone or core (40), and a counter-rotating coaxial rotor system (3, 5) having rotors with each rotor having a separate motor (54, 61) to drive the rotors about a common rotor axis of rotation (7), The rotor system is used to move the rotary wing vehicle (1) in directional flight.

Abstract translation: 旋翼机（1）包括具有细长管状骨架或芯（40）的本体结构和具有转子的反向旋转同轴转子系统（3,5），每个转子具有单独的电机（54,61） 驱动转子围绕共同的转子旋转轴（7）。转子系统用于在定向飞行中移动旋翼机（1）。

公开(公告)号：EP1594736A4

公开(公告)日：2010-02-24

申请号：EP04809283

申请日：2004-02-19

Applicant: AAI CORP

Inventor： MILLER STEPHEN W ,  VELAZQUEZ MATTHEW T

IPC: B64B20060101 ,  B64B1/00 ,  B64C3/56 ,  B64C39/02 ,  B64F1/04 ,  B64F1/06

CPC classification number: B64C39/024 ,  B64C2201/021 ,  B64C2201/042 ,  B64C2201/084 ,  B64C2201/102 ,  B64C2201/165 ,  B64C2201/201 ,  B64C2201/203 ,  B64F1/06

公开(公告)号：EP1687200A2

公开(公告)日：2006-08-09

申请号：EP04810203.2

申请日：2004-11-01

Applicant: The Insitu Group, Inc.

Inventor： SLIWA, Steven, M. ,  VON FLOTOW, Andreas, H. ,  DENNIS, Brian, D.

IPC: B63H1/00

CPC classification number: B64C11/003 ,  A63H27/02 ,  B64C11/04 ,  B64C11/14 ,  B64C11/28 ,  B64C39/024 ,  B64C2201/044 ,  B64C2201/082 ,  B64C2201/102 ,  B64C2201/165 ,  B64C2201/182 ,  B64C2201/201 ,  B64C2201/206 ,  B64D41/007 ,  F02K5/023 ,  F05D2260/85 ,  Y02T50/44 ,  Y02T50/672

Abstract: Methods and systems for starting propeller driven aircraft and other devices are disclosed. A system in accordance with one embodiment of the invention includes a removable fixture that is coupled to the propeller and has at least one portion exposed to a flowstream to rotate the propeller during engine start-up. The fixture is configured to separate from the propeller after the engine begins to turn over (e.g., after the engine starts and/or rotates above a threshold rate). Accordingly, the system can include a releasable link between the fixture and the propeller.