公开(公告)号：US20100176242A1

公开(公告)日：2010-07-15

申请号：US12532343

申请日：2008-03-25

申请人： Thomas Bock ,  Michael Auburger ,  Patrique Doemeland ,  Brigitte Gerner ,  Florian Schuephaus ,  Silvan Fiedler

发明人： Thomas Bock ,  Michael Auburger ,  Patrique Doemeland ,  Brigitte Gerner ,  Florian Schuephaus ,  Silvan Fiedler

IPC分类号： B64C99/00

CPC分类号： B64C1/066

摘要： A gap covering device (10) for covering a gap (16) between two mutually adjacent first aircraft interior components (12, 14) comprises a visible portion (18) as well as a retaining portion (20) connected to the visible portion (18) and extending opposite the visible portion (18). A receiving structure is fastened to an inner surface of the visible portion (18) and/or of the retaining portion (20) and has a receiving contour adapted to an edge contour of the first aircraft interior components (12, 14).

摘要翻译： 用于覆盖两个彼此相邻的第一飞行器内部部件（12,14）之间的间隙（16）的间隙覆盖装置（10）包括可见部分（18）以及连接到可见部分（18）的保持部分（20） ）并且与可见部分（18）相对延伸。 接收结构紧固到可见部分（18）和/或保持部分（20）的内表面，并具有适于第一飞行器内部部件（12,14）的边缘轮廓的接收轮廓。

公开(公告)号：US10589861B2

公开(公告)日：2020-03-17

申请号：US16345796

申请日：2016-10-31

申请人： OPTiM Corporation

发明人： Shunji Sugaya

IPC分类号： B64C99/00 ,  B64D47/08 ,  B64D1/18 ,  A01M7/00 ,  B64C39/02 ,  G05D1/00 ,  B64C13/16 ,  B64D1/16

摘要： A drone control system in which a drone can move to a position where a purpose can be achieved and performs an action according to the purpose is provided. The drone control system 1 controls a drone 10 capable of performing a predetermined action on a predetermined object, and includes a state data acquiring module 201 that acquires state data indicating a state of the object, a purpose data acquiring module 202 that acquires purpose data which is a purpose of moving the drone, and a detecting module 203 that detects an action point, which is position information at which an action for the purpose is executed, based on the acquired state data and purpose data.

公开(公告)号：US20100059627A1

公开(公告)日：2010-03-11

申请号：US11794487

申请日：2005-12-29

申请人： Cesar Bautista De La Llave ,  Bernardo Lopez Romano ,  Angel Postigo Rodriguez ,  Jose Sanchez Gomez

发明人： Cesar Bautista De La Llave ,  Bernardo Lopez Romano ,  Angel Postigo Rodriguez ,  Jose Sanchez Gomez

IPC分类号： B64C1/00 ,  B64C99/00 ,  B64C25/32

CPC分类号： B64C1/068 ,  B64C1/061 ,  B64C1/062 ,  B64C25/001 ,  B64C2001/0072 ,  Y02T50/43

摘要： The invention relates to an aircraft with a protection shield for the rear composite material, fuselage 25) for conducting tail impact tests, in addition to a tail absorber, the shield (11) being formed by a plurality of pieces (21) joined to supports (23) fixed to the rear fuselage (25) behind the tail absorber (1), said pieces (21) having a laminar structure with an outer steel sheet (13), an inner composite sheet (17) and an intermediate high resistance silicon sheet (15).

摘要翻译： 本发明涉及一种具有用于后部复合材料的保护罩的飞行器，用于进行尾部撞击试验的机身25），除了尾部吸收器之外，所述屏蔽件（11）由接合到支撑件的多个部件（21）形成 （23），固定到尾部吸收体（1）后面的后机身（25），所述片（21）具有层状结构，具有外钢板（13），内复合片（17）和中间高电阻硅 片（15）。

公开(公告)号：US12116129B2

公开(公告)日：2024-10-15

申请号：US18331960

申请日：2023-06-09

申请人： SOFTBANK CORP.

发明人： Noritomo Yanagimoto

IPC分类号： B64C39/10 ,  B64C3/48 ,  B64C11/46 ,  B64C99/00 ,  B64D27/24 ,  B64D27/31 ,  B64D27/357 ,  B64D33/10

CPC分类号： B64C39/10 ,  B64C3/48 ,  B64C11/46 ,  B64C99/00 ,  B64D27/24 ,  B64D27/31 ,  B64D27/357 ,  B64D33/10

摘要： There is provided a flight vehicle including: a wing unit; a battery that is arranged in the wing unit; an air intake unit that is formed at a position corresponding to the battery on a front side of the wing unit; a heat sink unit that is arranged for the battery and cools the battery by air which flows in from the air intake unit and that includes a ventilation unit having a shape widening from the front side toward a rear side; and an exhaust unit that is formed at a position corresponding to the battery on the rear side of the wing unit and that exhausts air which flows out from the heat sink unit.

公开(公告)号：US20230322383A1

公开(公告)日：2023-10-12

申请号：US18331960

申请日：2023-06-09

申请人： HAPSMobile Inc.

发明人： Noritomo YANAGIMOTO

IPC分类号： B64C39/10 ,  B64D27/24 ,  B64D33/10 ,  B64C11/46 ,  B64C3/48 ,  B64C99/00

CPC分类号： B64C39/10 ,  B64D27/24 ,  B64D33/10 ,  B64C11/46 ,  B64C3/48 ,  B64C99/00

摘要： There is provided a flight vehicle including: a wing unit; a battery that is arranged in the wing unit; an air intake unit that is formed at a position corresponding to the battery on a front side of the wing unit; a heat sink unit that is arranged for the battery and cools the battery by air which flows in from the air intake unit and that includes a ventilation unit having a shape widening from the front side toward a rear side; and an exhaust unit that is formed at a position corresponding to the battery on the rear side of the wing unit and that exhausts air which flows out from the heat sink unit.

公开(公告)号：US08162613B2

公开(公告)日：2012-04-24

申请号：US12038873

申请日：2008-02-28

申请人： Richard A. Oleson ,  Richard M. Aynsley ,  Dale R. Jury

发明人： Richard A. Oleson ,  Richard M. Aynsley ,  Dale R. Jury

IPC分类号： B64C99/00

CPC分类号： F04D25/088 ,  F04D29/384 ,  F04D29/681 ,  F05D2240/307

摘要： An angled fan blade extension includes an attachment portion and an angled portion. The attachment portion is configured to facilitate securing the angled fan blade extension to the distal end of a fan blade. The angled portion is configured to extend from the distal end of the attachment portion, creating an angled extension relative to the fan blade. Adding angular fan blade extensions to fan blades may improve the airflow control, and thereby increase the utility and efficiencies of a fan.

摘要翻译： 倾斜的风扇叶片延伸部包括附接部分和倾斜部分。 附接部分构造成便于将倾斜的风扇叶片延伸部固定到风扇叶片的远端。 成角度部分被构造成从附接部分的远端延伸，相对于风扇叶片产生成角度的延伸。 将风扇叶片延伸部分加入风扇叶片可以改善气流控制，从而提高风扇的效用和效率。

公开(公告)号：US20120175071A1

公开(公告)日：2012-07-12

申请号：US13419496

申请日：2012-03-14

申请人： Ingo WUGGETZER ,  Stefan LIST ,  Nicolas TSCHECHNE ,  Tobias MAYER

发明人： Ingo WUGGETZER ,  Stefan LIST ,  Nicolas TSCHECHNE ,  Tobias MAYER

IPC分类号： B64C99/00

CPC分类号： B64C1/066 ,  B64D11/00

摘要： A cladding apparatus is provided for the interior of an aircraft that includes, but is not limited to at least one two-dimensional fabric sheet, at least one guide device, and at least one tensioning element. The guide device is configured to be attached in the interior along a direction of extension of the interior, and slidably guide the fabric sheet at least in a first section of the interior along the direction of extension. The tensioning element is, furthermore, configured to be attached in the interior, and by producing a tensile force that acts on the front edge and/or the rear edge of the fabric sheet to stretch taut the fabric sheet along the direction of extension of the interior.

摘要翻译： 为飞行器的内部设置包层设备，其包括但不限于至少一个二维织物片，至少一个引导装置和至少一个张紧元件。 引导装置构造成沿着内部的延伸方向在内部附接，并且沿着延伸方向至少在内部的第一部分中可滑动地引导织物片。 此外，张紧元件被构造成附接在内部，并且通过产生作用在织物片的前边缘和/或后边缘上的张力，以沿着织物片的延伸方向拉伸织物片 室内。

公开(公告)号：US20120138741A1

公开(公告)日：2012-06-07

申请号：US13310873

申请日：2011-12-05

申请人： Christian Fabre ,  Alain Bignolais

发明人： Christian Fabre ,  Alain Bignolais

IPC分类号： B64C99/00

CPC分类号： B64D25/20 ,  A62B33/00 ,  B64D2045/0065 ,  G01S5/0231

摘要： Method and device for aiding the localization of an aircraft wreck submerged in a sea.The device includes at least a beacon (2a, 2b) which is automatically ejected out of the fuselage of the aircraft (AC), when this latter is submerged in a sea (M).

摘要翻译： 帮助淹没在海上的飞机残骸的本地化的方法和装置。 该装置至少包括一个信标（2a，2b），当它们被淹没在海中时，该信标（2a，2b）被自动地弹出飞机（AC）的机身（M）。

公开(公告)号：US20110309197A1

公开(公告)日：2011-12-22

申请号：US13165461

申请日：2011-06-21

申请人： Julie Holvoet ,  Matthieu De Kergommeaux ,  Jean-Claude Briois ,  Luc Michelet

发明人： Julie Holvoet ,  Matthieu De Kergommeaux ,  Jean-Claude Briois ,  Luc Michelet

IPC分类号： F16M13/02 ,  B64C99/00

CPC分类号： B64C1/406 ,  B64C1/40 ,  F16L3/24 ,  H02G3/32 ,  Y02T50/46

摘要： This device is intended for an aircraft comprising frames, a skin and connecting pieces between the skin and the frames, referred to as clips.It comprises: two brackets (30), each bracket having a first branch (32) intended to be fastened to a clip of the aircraft and a second branch (34) provided with a slot (36), a stirrup-shaped clip (1) comprising a base (2) and two arms (4, 6), each arm (4, 6) having at its free end a securing lug (17) adapted for being able to be inserted in the slot (36) of one of the said brackets with a flange (19) that forms a stop countering displacement of the securing lug once the latter is inserted into the said slot, each arm (4, 6) further comprising at least one support (14, 22) for accommodating a system.

摘要翻译： 该装置适用于包括框架，皮肤以及皮肤和框架之间的连接件（称为夹子）的飞行器。 它包括：两个支架（30），每个支架具有一个第一分支（32），用于固定到飞行器的一个夹子上;第二分支（34）设置有一个槽（36），一个镫形的夹子 ），其包括基部（2）和两个臂（4,6），每个臂（4,6）在其自由端处具有固定凸耳（17），该固定凸耳适于能够插入到 所述支架具有凸缘（19），所述凸缘（19）在所述凸缘插入所述槽中时形成所述固定凸耳的止动对抗位移，每个臂（4,6）还包括至少一个支撑件（14,22） 系统。

公开(公告)号：US20110187182A1

公开(公告)日：2011-08-04

申请号：US13008938

申请日：2011-01-19

申请人： Howard Austerlitz ,  Ron Bueter ,  John O'Brien

发明人： Howard Austerlitz ,  Ron Bueter ,  John O'Brien

IPC分类号： B64C99/00 ,  G05F3/02

CPC分类号： H02H9/008 ,  Y10T307/492 ,  Y10T307/505 ,  Y10T307/516 ,  Y10T307/62

摘要： A method and system for limiting energy to a sensor and/or an environment in which the sensor is located. A high current sensor driver is powered through a resistance-capacitance (RC) circuit. In a failure mode, the RC circuit constrains output of a sensor driver to the sensor in order to limit average current applied to the sensor. In one embodiment, the capacitor is chosen so that it can provide adequate current to the sensor driver for a short period of time. The value of the resistor may be chosen to ensure that under short circuit conditions direct current (DC) is limited to a safe value. The combined values of the resistor and capacitor may be adjusted such that the capacitor can charge to a prescribed level during the interval between active pulses.

摘要翻译： 一种用于将能量限制到传感器和/或传感器所位于的环境中的方法和系统。 高电流传感器驱动器通过电阻电容（RC）电路供电。 在故障模式下，RC电路将传感器驱动器的输出限制到传感器，以限制施加到传感器的平均电流。 在一个实施例中，选择电容器使得其可以在短时间段内向传感器驱动器提供足够的电流。 可以选择电阻的值，以确保在短路条件下，直流（DC）被限制在一个安全值。 可以调节电阻器和电容器的组合值，使得电容器可以在有效脉冲之间的间隔期间将电荷充电到规定的电平。