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1. 发明申请

WO2017011075A1 CONTROL NORMALIZATION FOR UNMANNED AUTONOMOUS SYSTEMS 审中-公开
标题翻译：控制不规范自动系统的正常化
公开(公告)号：WO2017011075A1
公开(公告)日：2017-01-19
申请号：PCT/US2016/033764
申请日：2016-05-23
申请人： QUALCOMM INCORPORATED
发明人： CHAU, Kiet Tuan , CANOY, Michael-David Nakayoshi , DEVICO, Michael Orlando , SPRIGG, Stephen Alton
IPC分类号： G05D1/00
CPC分类号： B64C13/06 , B64C39/024 , B64C2201/141 , B64C2201/146 , G05B13/04 , G05D1/0022
摘要： Methods, systems, and process-readable media include an autonomous vehicle override control system that receives override commands from a pilot qualified on a first type of unmanned autonomous vehicle (UAV) and translates the inputs into suitable commands transmitted to a target UAV of a second UAV type. A pilot's certification for a first UAV type may be determined from the pilot's login credentials. The system may obtain a first control model for the first UAV type and a second control model for the target UAV. Pilot input commands processed through the first control model may be used to calculate movements of a virtual UAV of the type. The system may estimate physical movement of the target UAV similar to the first physical movement, and generate an override command for the target UAV using the second control model and the second physical movement. Control models may accommodate current conditions and pilot experience.
摘要翻译：方法，系统和过程可读介质包括自动车辆覆盖控制系统，其从在第一类型的无人自主车辆（UAV）上限定的飞行器接收超控命令，并且将输入转换为传输到第二类型的目标UAV的合适命令无人机类型。飞行员的第一个UAV类型的认证可以从飞行员的登录凭据确定。该系统可以获得用于第一UAV类型的第一控制模型和用于目标UAV的第二控制模型。可以使用通过第一控制模型处理的导频输入命令来计算该类型的虚拟UAV的移动。系统可以估计目标UAV的物理运动，类似于第一物理运动，并且使用第二控制模型和第二物理运动生成针对目标UAV的覆盖命令。控制模型可以适应当前条件和飞行员体验。

2. 发明申请

WO2008061110A2 CUSTOMIZABLE PEDAL SYSTEM 审中-公开
标题翻译：可自定义的踏板系统
公开(公告)号：WO2008061110A2
公开(公告)日：2008-05-22
申请号：PCT/US2007084606
申请日：2007-11-14
申请人： BELL HELICOPTER TEXTRON INC , SPINA PASQUALE , LINTON BRAD
发明人： SPINA PASQUALE , LINTON BRAD
IPC分类号： B62M1/36 , G05G1/38
CPC分类号： B64C13/06 , G05G1/40 , G05G1/44 , G05G1/46 , G05G11/00 , Y10T74/2039 , Y10T74/20528
摘要： A pedal system comprising a support base; a first lever comprising a root portion and a terminal portion formed such that the terminal portion interfaces with the root portion at a bend in the first lever of a first predetermined angle, the root portion of the first lever being pivotally mounted to the support base such that the first lever is rotatable in a first plane of rotation about an axis of rotation at or near the support base; a second lever comprising a root portion and a terminal portion formed such that the terminal portion interfaces with the root portion at a bend in the second lever of a second predetermined angle, the root portion of the second lever being pivotally mounted to the support base such that the second lever is rotatable in a second plane of rotation about the axis of rotation, wherein the second plane of rotation is substantially parallel to the first plane of rotation; a first pedal configured to be engaged by a foot of a user to rotate the first lever about the axis of rotation, the first pedal being attached to the first lever to extend therefrom in a direction that is (i) away from the second lever, and (ii) roughly parallel to the axis of rotation, the first pedal being attached to the first lever such that the position of the first pedal is adjustable along the terminal portion of the first lever; a second pedal configured to be engaged by a foot of the user to rotate the second lever about the axis of rotation, the second pedal being attached to the second lever to extend therefrom in a direction that is (i) away from the first lever, and (ii) roughly parallel to the axis of rotation, the second pedal being attached to the second lever such that the position of the second pedal is adjustable along the terminal portion of the second lever separate from the adjustment of the first pedal along the terminal portion of the first lever.
摘要翻译：一种踏板系统，包括支撑基座; 第一杠杆，包括根部部分和端部部分，其形成为使得端子部分在第一杠杆的弯曲处以第一预定角度与根部部分接合，第一杠杆的根部可枢转地安装到支撑基座，所述第一杠杆能够在围绕所述支撑基座处或附近的旋转轴线的第一旋转平面中旋转; 第二杆，包括根部和终端部，其形成为使得端子部分在第二杆的弯曲处以第二预定角度与根部部分接合，第二杆的根部可枢转地安装到支撑基座，所述第二杠杆可围绕所述旋转轴线在第二旋转平面中旋转，其中所述第二旋转平面基本上平行于所述第一旋转平面; 第一踏板被构造成由使用者的脚接合以围绕旋转轴线旋转第一杆，第一踏板附接到第一杆以在其上延伸，其方向为（i）远离第二杆，和（ii）大致平行于所述旋转轴线，所述第一踏板附接到所述第一杆，使得所述第一踏板的位置沿着所述第一杆的端子部分可调节; 第二踏板，其构造成被使用者的脚接合以围绕旋转轴线旋转第二杆，第二踏板附接到第二杆，以在其方向上延伸，其方向是（i）远离第一杆，和（ii）大致平行于旋转轴线，第二踏板附接到第二控制杆，使得第二踏板的位置沿第二操纵杆的端子部分可调节，与第一踏板沿着终端的调节分开第一杆的一部分。

3. 发明申请

WO2016191071A1 BARREL CAM RUDDER PEDAL ASSEMBLY 审中-公开
公开(公告)号：WO2016191071A1
公开(公告)日：2016-12-01
申请号：PCT/US2016/031199
申请日：2016-05-06
申请人： WOODWARD MPC, INC. , PETROU, Anton , PIOTROWSKI, Maciej
发明人： PETROU, Anton , PIOTROWSKI, Maciej
IPC分类号： B64C13/06 , B64C13/04 , B64C27/56
CPC分类号： F16H25/12 , B64C13/04 , B64C13/06 , B64C27/56 , Y02T50/44
摘要： A barrel cam rudder pedal system is provided. The system includes an outer housing (24) with a chassis assembly (40) carried by the outer housing (24). A barrel cam arrangement (26) is rotationally mounted within an interior space of the chassis assembly (40). A pair of pedal assemblies (22) is mechanically coupled to the barrel cam arrangement (26) such that linear movement of either of the pair of pedal assemblies (22) results in a rotation of the barrel cam arrangement (26) about a central longitudinal axis defined by the barrel cam arrangement (26).
摘要翻译：提供桶式舵舵踏板系统。该系统包括具有由外壳（24）承载的底盘组件（40）的外壳（24）。桶形凸轮装置（26）旋转地安装在底盘组件（40）的内部空间内。一对踏板组件（22）机械地联接到所述滚筒凸轮装置（26），使得所述一对踏板组件（22）中的任何一个的直线运动导致所述滚筒凸轮装置（26）绕中心纵向轴由筒状凸轮装置（26）限定。

4. 发明申请

WO2014075023A1 MODULAR, ABOVE-THE-FLOOR RUDDER AND BRAKE CONTROL SYSTEM 审中-公开
标题翻译：模块化，上面的地面和制动控制系统
公开(公告)号：WO2014075023A1
公开(公告)日：2014-05-15
申请号：PCT/US2013/069509
申请日：2013-11-11
申请人： MASON ELECTRIC CO.
发明人： CARNER, Fred , SALAMAT, Bijan
IPC分类号： B64C13/04 , B64C13/06 , B64C13/50
CPC分类号： B64C13/06 , B64C13/04 , B64C13/503
摘要： A modular brake and rudder control system usable in an aircraft. The modular system mounts atop the flight deck floor (16) without penetrating through the floor when the system is operatively connected to the aircraft's fly-by-wire brake and rudder systems. Pedal assemblies (66) extending from the housing (40) are rotatable and longitudinally moveable relative to the housing. A brake control system fully contained in the housing is connected to the pedal assemblies and provides a signal via an electrical connector (28) to the fly-by-wire brake system upon rotation of the pedals. A rudder control system is fully contained in the housing and is operable independent of the brake control system. The rudder control system detects longitudinal motion of the pedal assemblies and provides a signal via an electrical connector (28) to the fly-by-wire rudder system. The housing, the electrical connectors, the pedal assemblies, the brake control system and the rudder control system define a modular component installable and removable from the cockpit as a unit.
摘要翻译：一种可用于飞机的模块式制动和方向舵控制系统。当系统可操作地连接到飞行器的线控制动器和方向舵系统时，模块化系统安装在飞行甲板地板（16）的顶部，而不会穿透地板。从壳体（40）延伸的踏板组件（66）可相对于壳体旋转并纵向移动。完全容纳在壳体中的制动控制系统连接到踏板组件，并且在踏板旋转时通过电连接器（28）向线绕制动系统提供信号。舵控制系统完全包含在壳体中，并且独立于制动控制系统可操作。方向舵控制系统检测踏板组件的纵向运动，并通过电连接器（28）向线控舵系统提供信号。壳体，电连接器，踏板组件，制动控制系统和方向舵控制系统定义了作为一个单元可从驾驶舱安装和拆卸的模块化部件。

5. 发明申请

WO2016200601A1 EFFICIENT POWER AND THERMAL MANAGEMENT SYSTEM FOR HIGH PERFORMANCE AIRCRAFT 审中-公开
标题翻译：高性能飞机的有效功率和热管理系统
公开(公告)号：WO2016200601A1
公开(公告)日：2016-12-15
申请号：PCT/US2016/033907
申请日：2016-05-24
申请人： NORTHROP GRUMMAN SYSTEMS CORPORATION
发明人： HO, Yuhang
IPC分类号： B64D41/00 , B64C13/06 , B64D13/06
CPC分类号： F01D19/00 , B60R16/03 , B64C13/06 , B64D13/06 , B64D41/00 , B64D2013/0611 , B64D2013/0614 , B64D2013/0644 , B64D2013/0696 , B64D2221/00 , F01D5/02 , F01D15/10 , F02C7/12 , F02C7/268 , F04D29/321 , F05D2240/24 , F05D2240/60 , F05D2260/20 , Y02T50/56
摘要： A system and method for improved efficiency of an integrated power and cooling unit, IPCU (100), of an aircraft is disclosed. The IPCU (100) comprises a compressor (104), a starter/generator (106) and at least a cooling turbine (102), all coupled to a common shaft (110). The system (300) uses an open-loop cooling system and turbo machine power-matching to provide wide operation range without over-sizing. In order to reduce the temperature of the air flow through a cooling heat exchanger (116), the cooling turbine (102) needs to expand further, at the same time generating power to the shaft (110). To avoid the power being higher than the compressor (104) could absorb, the starter/generator (106) is used to convert the power into electrical power supplied to loads on the aircraft, to arrive at a more efficient system. Power sum control (302,304) via distribution control units is used to couple a bus (115) receiving power from the IPCU (100) starter/generator (106), with buses (128,132) receiving power from generators (124,126) of the aircraft engine (122).
摘要翻译：公开了一种用于提高飞机综合功率和冷却单元（IPCU（100））效率的系统和方法。 IPCU（100）包括压缩机（104），起动器/发电机（106）和至少一个冷却涡轮机（102），其全部联接到公共轴（110）。系统（300）使用开环冷却系统和涡轮机功率匹配来提供广泛的操作范围，而不会过大。为了降低通过冷却热交换器（116）的空气流的温度，冷却涡轮（102）需要进一步膨胀，同时向轴（110）产生动力。为了避免功率高于压缩机（104）吸收的功率，起动器/发电机（106）用于将功率转换成供应给飞机上的负载的电力，以获得更有效的系统。通过分配控制单元的功率和控制（302,304）用于将从IPCU（100）启动器/发电机（106）接收电力的总线（115）与从飞行器引擎的发电机（124,126）接收功率的总线（128,132）（122）。

6. 发明申请

WO2016082014A1 SYSTEM AND METHOD TO INTERCHANGE FLIGHT CONTROL INCEPTORS IN AN AIRCRAFT FLIGHT CONTROL SYSTEM AND COCKPIT 审中-公开
标题翻译：在航空器飞行控制系统和机组中交换飞行控制受害者的系统和方法
公开(公告)号：WO2016082014A1
公开(公告)日：2016-06-02
申请号：PCT/BR2015/000178
申请日：2015-11-25
申请人： EMBRAER S.A.
发明人： DE MIRANDA CARÁ, Guilherme , CHAVES, Nilson Emanuel Bezerra , FONSECA, Celso Jose Amaral , CAMPOS, Marcos Vinícus
IPC分类号： B64C13/04 , B64C27/56
CPC分类号： B64C13/04 , B64C13/06 , B64C27/56 , B64D11/0689 , Y02T50/44
摘要： A flexible flight control system enables conversion from one architecture using one type of inceptor to another architecture using another type of inceptor, through the usage of modular software and hardware pieces with common interfaces among the different types of inceptors. Longitudinal and lateral directional control laws are adapted to be compatible with the specific aspects of the operation of each configuration/architecture, giving the option to the aircraft operator to choose any one of a number of inceptor architectures at time of manufacture.
摘要翻译：灵活的飞行控制系统通过使用具有不同类型的接收器之间的通用接口的模块化软件和硬件部件，使用一种类型的受体到另一种架构，使用另一种类型的受体来实现转换。纵向和横向方向控制规则适用于与每个配置/架构的操作的具体方面相一致，为飞行员提供在制造时选择多个受体架构中的任何一个的选项。

7. 发明申请

WO2014138014A1 MULTIPLE DEGREES OF TRANSLATIONAL ADJUSTMENT PEDALS 审中-公开
标题翻译：多层次的翻译调整方案
公开(公告)号：WO2014138014A1
公开(公告)日：2014-09-12
申请号：PCT/US2014/020201
申请日：2014-03-04
申请人： WOODWARD, INC. , STACHNIAK, Darryl S.
发明人： STACHNIAK, Darryl S.
IPC分类号： B64C13/04 , F02D11/02
CPC分类号： G05G1/405 , B64C13/06 , Y10T74/20528
摘要： A pedal system for an aircraft comprising a pedal and a pedal mounting mechanism is provided. The pedal is configured for manipulation through at least one operational degree of freedom by a pilot to provide control inputs to the aircraft. The pedal mounting mechanism is configured for supporting the pedal within a cockpit of the aircraft for manipulation by the pilot. The pedal mounting mechanism provides at least two adjustment degrees of freedom for adjusting the position of the pedal within the cockpit.
摘要翻译：提供了一种用于包括踏板和踏板安装机构的飞机的踏板系统。踏板被配置成通过飞行员通过至少一个操作自由度进行操纵以向飞行器提供控制输入。踏板安装机构被配置为将踏板支撑在飞行器的驾驶舱内，以由飞行员操纵。踏板安装机构提供至少两个调整自由度以调节驾驶舱内踏板的位置。

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