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51. 发明授权

US5033010A Turbine engine monitoring system 失效
标题翻译：涡轮发动机监控系统
公开(公告)号：US5033010A
公开(公告)日：1991-07-16
申请号：US277099
申请日：1988-11-29
申请人： Trevor Lawrence , Edward N. Denaci , William H. Conn
发明人： Trevor Lawrence , Edward N. Denaci , William H. Conn
IPC分类号： G05B23/02
CPC分类号： G05B23/0264 , F05B2220/50
摘要： A turbine engine monitoring system is provided which disposes a data storage device in permanent association with an engine being monitored. The data storage device comprises an electrically erasable programmable read-only memory which is contained in an enclosure and permanently attached to the engine. A connection link is provided to connect the memory device in signal communication with an external device, such as an engine control unit. The engine control unit is connected in signal communication with a plurality of transducers that enable the engine control unit to monitor the operational status of a plurality of parameters relating to the turbine engine. By permanently attaching the data storage device to the turbine engine, a lifetime information of the turbine engine can be maintained in permanent association with the turbine engine regardless of replacement of the turbine engine or its related engine control unit.
摘要翻译：提供了一种涡轮发动机监控系统，其配置与正在监测的发动机永久关联的数据存储装置。数据存储设备包括电可擦除可编程只读存储器，其被包含在外壳中并且永久地附接到发动机。提供连接链路以将存储器设备与诸如发动机控制单元的外部设备进行信号通信。发动机控制单元与多个换能器进行信号通信连接，使得发动机控制单元能够监视与涡轮发动机相关的多个参数的操作状态。通过将数据存储装置永久地附接到涡轮发动机，无论涡轮发动机或其相关的发动机控制单元的更换，涡轮发动机的寿命信息都可以与涡轮发动机永久地相关联。

52. 发明授权

US4914910A Emergency power unit oxidizing gas bottle heating apparatus 失效
标题翻译：应急动力装置氧化气瓶加热装置
公开(公告)号：US4914910A
公开(公告)日：1990-04-10
申请号：US218875
申请日：1988-07-14
申请人： Malcolm J. McArthur
发明人： Malcolm J. McArthur
IPC分类号： B64D41/00
CPC分类号： B64D41/00 , F05B2220/50
摘要： An emergency power unit for providing emergency on board power to an aircraft having apparatus for heating the oxidizing gas contained in the oxidizing gas bottle includes a fuel supply source (14) for supplying fuel, and oxidizing gas bottle (12) containing pressurized oxidizing gas, an oxidizing gas heating device (18) and (20) for heating the pressurized oxidizing gas within the oxidizing gas bottle (12) by using heat energy generated by a combustor (16) wherein the combustor (16) causes combustion of a mixture of fuel and oxidizing gas heated by the oxidizing gas heating device (18) and (20). Hot gases resulting from the combustion of the mixture of fuel and heated oxidizing gas drive the blades of a turbine (32) thereby producing emergency on board power to the aircraft.
摘要翻译：一种用于向具有用于加热氧化气体瓶中所含的氧化气体的装置的飞行器提供紧急电力的应急动力单元包括用于供应燃料的燃料供应源（14）和包含加压氧化气体的氧化气瓶（12）氧化气体加热装置（18）和（20），用于通过使用由燃烧器（16）产生的热能来加热氧化气体瓶（12）内的加压氧化气体，其中燃烧器（16）引起燃料混合物燃烧和由氧化气体加热装置（18）和（20）加热的氧化气体。由燃料和加热的氧化气体的混合物的燃烧产生的热气体驱动涡轮机（32）的叶片，由此产生飞机上的紧急电力。

53. 发明授权

US4786852A Inverter operated turbine engine starting system 失效
标题翻译：变频器运行的涡轮发动机启动系统
公开(公告)号：US4786852A
公开(公告)日：1988-11-22
申请号：US169141
申请日：1988-03-10
申请人： Alexander Cook
发明人： Alexander Cook
IPC分类号： F02N11/04 , F02N11/00
CPC分类号： F02N11/04 , F05B2220/50
摘要： Engine start capability may be added to an aircraft generating system including a variable speed, constant frequency inverter 34 by placing transistors 48 in shunt relation to diodes 22 forming part of a full wave rectifier for rectifying A.C. power from a brushless generator output winding 10 which is normally supplied to the inverter 34 for conversion to constant frequency A.C. power. A source of D.C. power 60 may be connected to the diodes 22 and transistors 48 and the latter are operated by an inverter controller 52 to convert the D.C. power so provided to alternating current to be fed to the brushless generator output windings 10 and cause the brushless generator to operate as an A.C. motor for the starting of a turbine engine 18 or the like.
摘要翻译：发动机启动能力可以通过将晶体管48分配到与形成全波整流器的一部分的二极管22分流的方式添加到包括可变速恒定变频器34的飞机发电系统中，用于整流来自无刷发电机输出绕组10的交流电力，通常提供给逆变器34以转换成恒定的交流电力。 DC电源60的源可以连接到二极管22和晶体管48，并且后者由逆变器控制器52操作以将所提供的DC电力转换成交流电流以供给无刷发电机输出绕组10并使无刷发电机作为用于启动涡轮发动机18等的AC电动机。

54. 发明授权

US4769051A Filtered environmental control system 失效
标题翻译：过滤后的环境控制系统
公开(公告)号：US4769051A
公开(公告)日：1988-09-06
申请号：US109634
申请日：1987-10-19
申请人： Gregory L. Defrancesco
发明人： Gregory L. Defrancesco
IPC分类号： B64D13/06 , F24F3/16 , B01D53/04
CPC分类号： F24F3/1603 , B64D13/06 , B64D2013/0651 , F05B2220/50
摘要： An air conditioning system, being powered by a supply of compressed air, has an air cycle machine which incorporates a regenerable filter. The filter receives pressurized air for filtration from the air cycle machine compressor, and receives purge air from the air cycle machine turbine downstream of a load heat exchanger. The air cools the load before purging the filter thereby minimizing system power requirements.

55. 发明授权

US4456830A AC Motor-starting for aircraft engines using APU free turbine driven generators 失效
标题翻译：交流电机启动使用APU自由涡轮驱动发电机的飞机发动机
公开(公告)号：US4456830A
公开(公告)日：1984-06-26
申请号：US370760
申请日：1982-04-22
申请人： Michael J. Cronin
发明人： Michael J. Cronin
IPC分类号： F02N11/04 , F02N11/14 , F02N7/08 , F02N17/00
CPC分类号： F02N11/04 , F02N11/14 , F05B2220/50
摘要： The invention is an electric starting system for starting aircraft jet engines (32), (34) and (36) using an APU (10) free turbine driven generator (12). The operating power factor of the starter-generator (12) is controlled during start mode operation of the APU (10) by monitoring the line current via a current transformer (58). Contactors (14) and (16) connect the generator (12) into the aircraft's ac power system and ac starting system, respectively. A master start relay (22) is provided, and is closed in the `start` mode such that a power electronics inverter (24) may be powered from external power via contactors (18). The variable-voltage/variable-frequency output of inverter (24) is controlled via a logic controller (26) and can be applied sequentially to the three engine driven generators (32), (34) and (36) via start relays (42), (44) and (46) to start the engines (32), (34) and (36) respectively. An alternative embodiment of the APU generator/power electronics/starter-generator start system is the utilization of a separate induction motor starter than can operate with or without the use of power electronics.
摘要翻译：本发明是一种用于使用APU（10）的涡轮机驱动发电机（12）启动飞机喷气发动机（32），（34）和（36）的电启动系统。通过经由电流互感器（58）监视线路电流，在APU（10）的启动模式操作期间控制起动器 - 发电机（12）的工作功率因数。接触器（14）和（16）将发电机（12）分别连接到飞机的交流电源系统和交流启动系统中。提供主启动继电器（22），并且以“起动”模式闭合，使得电力电子逆变器（24）可以通过接触器（18）从外部电源供电。逆变器（24）的可变电压/可变频率输出通过逻辑控制器（26）进行控制，并且可以通过启动继电器（42）依次施加到三个发动机驱动发电机（32），（34）和（36）），（44）和（46）分别启动发动机（32），（34）和（36）。 APU发电机/电力电子/起动器起动系统的另一实施例是使用独立的感应电动机起动器，而不是使用或不使用电力电子设备。

56. 发明授权

US3928971A Internal combustion engine 失效
标题翻译：内燃机
公开(公告)号：US3928971A
公开(公告)日：1975-12-30
申请号：US45005174
申请日：1974-03-11
申请人： SPATH TOMMY W
发明人： SPATH TOMMY W
IPC分类号： F02G3/02 , F02G3/00
CPC分类号： F02G3/02 , F05B2220/50
摘要： An internal combustion engine of the usual piston type in combination with a gas turbine operable to assist in powering the output drive shaft of said engine, the exhaust gases and the crankcase vapors of the piston engine, which contain combustible unburned hydrocarbons, being collected, compressed and supplied to the turbine to provide fuel therefor, whereby both to increase the proportion of the available energy extracted from the basic fuel, for greater economy of fuel usage, and also to reduce the amount of atmosphere polluting emissions contained in the ultimate exhaust gases.
摘要翻译：通常的活塞式的内燃机与燃气轮机组合起来，该燃气轮机可操作以帮助驱动所述发动机的输出驱动轴，含有可燃的未燃碳氢化合物的活塞发动机的废气和曲轴箱蒸气被收集，压缩并提供给涡轮机以提供燃料，从而增加从基本燃料中提取的可用能量的比例，以增加燃料使用的经济性，并且还减少最终废气中所含的大气污染排放物的量。

57. 发明授权

US3380564A Accessory drive for single turbine helicopter 失效
标题翻译：单涡轮直升机配件驱动
公开(公告)号：US3380564A
公开(公告)日：1968-04-30
申请号：US54058666
申请日：1966-04-06
申请人： UNITED AIRCRAFT CORP
发明人： BEURER FREDERICK C
IPC分类号： B64C27/12
CPC分类号： B64C27/12 , F05B2220/50

58. 发明授权

US2798166A Method and apparatus for starting gas turbines 失效
标题翻译：用于启动燃气轮机的方法和装置
公开(公告)号：US2798166A
公开(公告)日：1957-07-02
申请号：US50126255
申请日：1955-04-14
申请人： SOLAR AIRCRAFT CO
发明人： PETER KAREN H
IPC分类号： H02P9/08
CPC分类号： H02P9/08 , F05B2220/50 , H02P2101/30 , Y10T307/305 , Y10T307/50 , Y10T307/62

59. 发明申请

US20120183402A1 SPIRAL BEVEL GEAR SET FOR RAM AIR TURBINE 有权
标题翻译：用于RAM空气涡轮机的螺旋桨齿轮组
公开(公告)号：US20120183402A1
公开(公告)日：2012-07-19
申请号：US13008203
申请日：2011-01-18
申请人： Stephen Michael Bortoli
发明人： Stephen Michael Bortoli
IPC分类号： F03D11/02 , B23P11/00 , F16H1/14
CPC分类号： F03D15/10 , B64D41/007 , F03D9/00 , F03D9/28 , F03D9/32 , F03D15/00 , F03D80/70 , F05B2220/50 , F05B2240/50 , F05B2240/923 , F05B2260/503 , F05B2260/5032 , F05D2260/4031 , F16H1/14 , F16H55/0846 , Y02E10/722 , Y10T29/49229 , Y10T74/19665
摘要： A ram air turbine (RAT) assembly includes a gearbox that supports a gear set with a ring gear that drives a pinion gear. The gear set provides for the transmission of power from the turbine to a generator, pump or other power conversion device. A turbine shaft supports the ring gear and a pinion shaft that rotates about an axis transverse to the turbine shaft supports the pinion gear. A ratio between a face width and a diametrical pitch of the gear set is within a desired ratio that provides sufficient space for supporting bearing assemblies while provide for operation within the physical constraints and desired performance requirements of the RAT.
摘要翻译：冲压空气涡轮机（RAT）组件包括齿轮箱，其支撑具有驱动小齿轮的齿圈的齿轮组。齿轮组提供从涡轮机到发电机，泵或其它电力转换装置的动力传输。涡轮轴支撑环形齿轮，并且小齿轮轴围绕横向于涡轮轴的轴线旋转，支撑小齿轮。齿轮组的面宽度和直径间距之间的比率在所需的比率内，其提供足够的空间用于支撑轴承组件，同时提供在物理约束和RAT的期望性能要求下的操作。

60. 发明授权

US08154148B2 Device and method for emergency electricity supply on board an aircraft 有权
标题翻译：飞机上应急电源的装置和方法
公开(公告)号：US08154148B2
公开(公告)日：2012-04-10
申请号：US12294435
申请日：2007-03-13
申请人： Olivier Langlois , Etienne Foch
发明人： Olivier Langlois , Etienne Foch
IPC分类号： B60L1/00 , B60L3/00 , H02G3/00
CPC分类号： B64D41/00 , B64D41/007 , B64D2041/002 , B64D2221/00 , F03D9/12 , F03D9/25 , F03D9/32 , F05B2220/50 , Y02E10/725 , Y02E60/16 , Y02T50/44 , Y02T50/54
摘要： A device and a method for emergency electricity supply on board an aircraft, able to supply a part of the aircraft's electrical power circuit. The device includes a synchronous machine with separate excitation, associated with a flywheel, and an auxiliary device to set the flywheel in rotation and to maintain rotation of the flywheel.
摘要翻译：一种用于飞机上的紧急电力供应的装置和方法，能够提供飞机电力电路的一部分。该装置包括具有与飞轮相关联的单独激励的同步机，以及用于将飞轮旋转并保持飞轮旋转的辅助装置。

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