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1. 发明专利

JP5787468B2 芝生保全車用万能ヨークアセンブリ有权
标题翻译：用于草皮维修车辆普遍轭组件
公开(公告)号：JP5787468B2
公开(公告)日：2015-09-30
申请号：JP2009037174
申请日：2009-02-19
申请人：テキストロンイノヴェーションズインコーポレイテッド , Textron Innovations Inc.
发明人：ウィルソン,ケニスアール.
IPC分类号： A01D34/64 , A01D34/82
CPC分类号： A01D67/005 , A01D34/44

2. 发明专利

JP2012235689A Ac drive system for electrically operated vehicle 审中-公开
标题翻译：用于电动车辆的交流驱动系统
公开(公告)号：JP2012235689A
公开(公告)日：2012-11-29
申请号：JP2012156833
申请日：2012-07-12
申请人： Textron Innovations Inc , テキストロンイノベーションズインコーポレイテッド
发明人： CLARK WARREN , BELL OLIVER A JR
IPC分类号： B60L7/00 , B60L11/18 , B60L15/20 , B60T7/02 , B60T7/12 , B60T8/17 , B60T8/171
CPC分类号： B60L3/108 , B60L3/12 , B60L7/14 , B60L7/26 , B60L11/1803 , B60L11/1816 , B60L11/1861 , B60L15/10 , B60L15/20 , B60L2200/22 , B60L2210/20 , B60L2220/30 , B60L2250/26 , B60L2260/28 , B60T13/586 , B60W10/08 , B60W10/18 , H04L2012/40215 , H04L2012/40273 , Y02T10/644 , Y02T10/645 , Y02T10/7005 , Y02T10/7044 , Y02T10/705 , Y02T10/7072 , Y02T10/725 , Y02T10/7275 , Y02T90/127 , Y02T90/14
摘要： PROBLEM TO BE SOLVED: To provide a drive system for a utility vehicle.SOLUTION: The drive system includes an alternating-current (AC) motor for providing a drive torque. The AC motor controller receives a power source voltage signal, a throttle pedal position signal, a brake pedal position signal, a key switch signal, a forward/neutral/reverse (FNR) signal, and a run/tow signal indicative of the utility vehicle being configured to be driven and being configured to be towed. The AC motor controller generates an AC drive signal for the AC motor, wherein the AC drive signal is based on the power source voltage signal, throttle pedal position signal, brake pedal position signal, key switch signal, FNR signal, and run/tow signal.
摘要翻译：要解决的问题：提供一种用于多用途车辆的驱动系统。解决方案：驱动系统包括用于提供驱动扭矩的交流（AC）电机。交流电动机控制器接收电源电压信号，节气门踏板位置信号，制动踏板位置信号，钥匙开关信号，前进/中立/反向（FNR）信号和指示多功能车辆的行驶/牵引信号被配置为被驱动并被构造成被牵引。交流电动机控制器产生用于交流电动机的交流驱动信号，其中交流驱动信号基于电源电压信号，油门踏板位置信号，制动踏板位置信号，钥匙开关信号，FNR信号和运行/牵引信号。版权所有（C）2013，JPO＆INPIT

3. 发明公开

US20240017823A1 OPTIMIZING USAGE OF SUPPLEMENTAL ENGINE POWER 审中-公开
公开(公告)号：US20240017823A1
公开(公告)日：2024-01-18
申请号：US17867231
申请日：2022-07-18
申请人： Textron Innovations Inc.
发明人： Thomas Dewey PARSONS , Charles Eric COVINGTON , Kent E. DONALDSON , Andrew Thomas CARTER
IPC分类号： B64C27/12 , B64D31/06
CPC分类号： B64C27/12 , B64D31/06
摘要： In an embodiment, an aircraft includes a drive system, a main engine coupled to the drive system to provide first power, and a supplemental engine coupled to the drive system to provide second power additive to the first power. The aircraft also includes a control system to control the main engine and the supplemental engine to optimize usage of the supplemental engine. The control system is operable to maintain the supplemental engine in a reduced power state at least until a determination is made that supplemental power is needed to satisfy a total power demand of the drive system. The control system is also operable to determine that supplemental power is needed to satisfy the total power demand of the drive system. The control system is further operable to increase a power level of the supplemental engine in response to the determination that supplemental power is needed.

4. 发明公开

US20230327292A1 Modular Battery Systems for Aircraft 审中-公开
公开(公告)号：US20230327292A1
公开(公告)日：2023-10-12
申请号：US18206610
申请日：2023-06-06
申请人： Textron Innovations Inc.
发明人： Michael Raymond Hull , Steven Loveland , Yue Fan
IPC分类号： H01M50/512 , B64D27/24 , B60L50/64 , B64C29/00 , B60L58/10 , H01M10/42 , H01M50/249 , H01M50/209
CPC分类号： H01M50/512 , B64D27/24 , B60L50/64 , B64C29/00 , B60L58/10 , H01M10/425 , H01M50/249 , H01M10/4207 , H01M50/209 , H01M2010/4271 , B64D2221/00 , B60L2200/10 , H01M2220/20
摘要： A modular battery system includes an array of battery modules arranged in at least one stack. Each battery module includes a plurality of battery cells, a first side having positive and negative receptacles and a second side, that is opposite of the first side, having positive and negative plugs. The receptacles and plugs are configured such that adjacent battery modules in a side-by-side relationship are electrically coupled together via plug and receptacle connections and such that the battery modules are electrically coupled together in parallel. An interconnection electrically couples each stack of battery modules together via plug and receptacle connections with one of the battery modules in each stack such that the stacks of battery modules are electrically coupled together in parallel. Each of the battery modules includes a thermal conditioning system configured to thermally isolate the battery module from the other battery modules.

5. 发明申请

WO2015081198A1 PROPELLER WITH LIGHTNING STRIKE PROTECTION 审中-公开
标题翻译：螺旋桨带防雷保护
公开(公告)号：WO2015081198A1
公开(公告)日：2015-06-04
申请号：PCT/US2014/067623
申请日：2014-11-26
申请人： TEXTRON INNOVATIONS, INC.
发明人： MARTIN, Billy, M. , DAVIS, Kevin, A.
IPC分类号： B64C11/20 , B64D45/02
CPC分类号： F01D5/147 , B64C11/26 , B64D45/02 , Y10T29/49332
摘要： A propeller blade assembly including a propeller blade having a leading edge, and a trailing edge extending between a tip and a hub, and an electrically conductive band extending longitudinally on either or both of the leading edge and trailing edge. The electrically conductive band secured to the leading edge of the propeller serves as an entry point on the aircraft and conductive channel into the airframe thereby avoiding the potentially damaging effect of the lightening on the carbon fiber composite propeller.
摘要翻译：包括具有前缘的螺旋桨叶片和在尖端和轮毂之间延伸的后缘的螺旋桨叶片组件以及在前缘和后缘中的任一个或两者上纵向延伸的导电带。固定到螺旋桨前缘的导电带作为飞机上的入口点和导电通道进入机身，从而避免了对碳纤维复合材料螺旋桨的减轻的潜在的破坏性影响。

6. 发明申请

WO2015023870A1 SYSTEM AND METHOD FOR REDUCED FLAMMABILITY OF AN AIRCRAFT FUEL SYSTEM 审中-公开
标题翻译：用于降低飞机燃料系统易燃性的系统和方法
公开(公告)号：WO2015023870A1
公开(公告)日：2015-02-19
申请号：PCT/US2014/051107
申请日：2014-08-14
申请人： TEXTRON INNOVATIONS, INC.
发明人： MONTGOMER, Michael, Scott
IPC分类号： B64D37/34 , B64D37/32 , F02M99/00
CPC分类号： B64D37/32 , B64D37/04
摘要： Disclosed is a method for controlling the flammability of fuel vapors in an aircraft main fuel tank that is located in whole or in part in the fuselage contour. The method comprises a fuel system architecture and fuel consumption sequencing maintaining liquid fuel in said main tanks during all normal operations. Ceasing the withdrawal of fuel from the main tank when the fuel reaches a predetermined level thereby limiting the volume and flammability exposure time of the fuel vapor ullage. Once the predetermined level is met the fuel is supplied from wing tanks throughout the remainder of the mission. The predetermined main tank fuel level at which wing tank fuel begins to be consumed is determined by the aircraft flight reserves fuel volume stored in the main tank as well as the amount necessary to continuously submerge the main tank fuel pumps during the entire mission.
摘要翻译：公开了一种控制整个或部分位于机身轮廓中的飞行器主燃料箱中的燃料蒸汽的可燃性的方法。该方法包括在所有正常操作期间在所述主油箱中保持液体燃料的燃料系统结构和燃料消耗顺序。当燃料达到预定水平时，停止燃油从主油箱的撤出，从而限制燃油蒸汽消耗的体积和可燃性暴露时间。一旦满足预定水平，燃油就从任务的其余部分的翼舱提供。机舱油箱燃料开始消耗的预定主油箱燃料油位由存储在主油箱中的飞机储备燃料量以及整个任务期间连续淹没主油箱燃油泵所需的量决定。

7. 发明申请

WO2013033585A3 AIRCRAFT SIDE- LEDGE CONSOLE 审中-公开
标题翻译：飞机侧面控制台
公开(公告)号：WO2013033585A3
公开(公告)日：2013-04-25
申请号：PCT/US2012053424
申请日：2012-08-31
申请人： TEXTRON INNOVATIONS INC , HEADRICK JONATHAN , THISIUS TODD , KUHN DAVE , CILLESEN CRAIG , DAVIS DAVE
发明人： HEADRICK JONATHAN , THISIUS TODD , KUHN DAVE , CILLESEN CRAIG , DAVIS DAVE
IPC分类号： B64D11/00 , B64D11/06 , F21V8/00
CPC分类号： B64D11/00 , B64D11/0638
摘要： A console for aircraft that is located between two seats which face each other. The console includes an open ledge with a cup holder arrangement. The cup holder arrangement includes two removable holder dividers which can be flipped up or down and held into position by a spring-loaded cam arrangement. The console also includes two inwardly facing surfaces which provide connectors for electronic devices resting on the ledge. A light-emitting face is provided on a back wall of the ledge so that any articles resting on the ledge can be seen in dark environments.
摘要翻译：位于两个彼此面对的座位之间的飞机控制台。控制台包括带杯架布置的开放式凸缘。杯架装置包括两个可拆卸的保持器分隔件，其可以被向上或向下翻转并通过弹簧加载的凸轮装置保持在适当位置。控制台还包括两个面向内的表面，其提供搁置在凸缘上的电子设备的连接器。在壁架的后壁上设置发光面，使得在黑暗环境中可以看到搁置在凸缘上的任何物品。

8. 发明申请

WO2013033585A2 AIRCRAFT SIDE- LEDGE CONSOLE 审中-公开
标题翻译：飞机侧面LEDGE控制台
公开(公告)号：WO2013033585A2
公开(公告)日：2013-03-07
申请号：PCT/US2012/053424
申请日：2012-08-31
申请人： TEXTRON INNOVATIONS INC. , HEADRICK, Jonathan , THISIUS, Todd , KUHN, Dave , CILLESEN, Craig , DAVIS, Dave
发明人： HEADRICK, Jonathan , THISIUS, Todd , KUHN, Dave , CILLESEN, Craig , DAVIS, Dave
IPC分类号： B64D11/00 , B64D11/06 , F21V8/00
CPC分类号： B64D11/00 , B64D11/0638
摘要： A console for aircraft that is located between two seats which face each other. The console includes an open ledge with a cup holder arrangement. The cup holder arrangement includes two removable holder dividers which can be flipped up or down and held into position by a spring-loaded cam arrangement. The console also includes two inwardly facing surfaces which provide connectors for electronic devices resting on the ledge. A light-emitting face is provided on a back wall of the ledge so that any articles resting on the ledge can be seen in dark environments.
摘要翻译：
位于彼此相对的两个座椅之间的飞机的控制台。控制台包括一个带杯架布置的开放式壁架。杯架装置包括两个可拆卸的保持架分隔件，其可通过弹簧加载凸轮装置向上或向下翻转并保持就位。控制台还包括两个面向内的表面，这些表面为搁置在壁架上的电子设备提供连接器。在壁架的后壁上提供发光面，以便在黑暗环境中可以看到搁在壁架上的任何物品。

9. 发明专利

CA3061109A1 AUTONOMOUS THRUST VECTORING RING WING POD 未知
公开(公告)号：CA3061109A1
公开(公告)日：2020-05-08
申请号：CA3061109
申请日：2019-11-07
申请人： TEXTRON INNOVATIONS INC
发明人： MORRIS KEVIN , BRODEUR NICHOLAS , FENNY CARLOS
IPC分类号： B64C27/28 , B64C27/20 , B64C27/26 , B64C29/00
摘要： An autonomous thrust vectoring ring wing pod is disclosed. A plurality of distributed propulsion element (thruster) layout within a self-articulating ring wing pod allows the pod to selectively control its thrust vector by controlling each propulsion element in the pod. This arrangement allows autonomous and independent control of the tilting of the ring wing relative to the aircraft. The ring wing pod acts as both a nacelle to house the propulsion elements as well as a lifting surface when in wing-borne flight. The autonomous thrust vectoring ring wing pod also provides superior aircraft attitude control in wing-borne flight, thus negating the need for conventional surface controls.

10. 发明专利

CA2710639C TEST INSTRUMENT FOR PULSE TDR, STEP TDR AND TRANSMISSION ANALYSIS 未知
公开(公告)号：CA2710639C
公开(公告)日：2017-08-22
申请号：CA2710639
申请日：2010-07-21
申请人： TEXTRON INNOVATIONS INC
发明人： DURSTON THOMAS W
IPC分类号： G01R31/02 , G01R31/11 , H04B3/46 , H04M1/24
摘要： The test instrument is used to perform both time domain reflectometry (TDR) and analysis of transmission signals on a line under test. Further, the test instrument provides for both pulse TDR and step TDR. A coupling transformer having an enhanced low frequency response provides for coupling of the test instrument to the line under test. Isolation circuits between the coupling transformer and the line under test to prevent damage to the test instrument due to voltages on the line under test allow the test instrument to be used in connection with an active line under test. Two isolation circuits are utilized to maintain longitudinal balance of the circuit. During step TDR, the positive and negative transmitter circuits provide step-- shaped impulse signals. The enhanced low frequency response of the coupling transformer allows for transmission of step-shaped impulses, including the DC components of those signals, to the line under test and allows for transmission of reflected signals, including the DC components of those signals to the receivers. The test instrument provides selectable impedance matching and provides for selectable attenuation levels.

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