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公开(公告)号:US20080093500A1
公开(公告)日:2008-04-24
申请号:US11662559
申请日:2004-09-28
申请人: Dudley Smith , Walter Joiner , Paul Madej , Charles Hollimon , Daniel Robertson
发明人: Dudley Smith , Walter Joiner , Paul Madej , Charles Hollimon , Daniel Robertson
IPC分类号: B64C27/82
CPC分类号: B64C27/82 , B64C2027/8245
摘要: A rotorcraft having an enhanced configuration in which a simple wing and a propulsive anti-torque system are combined is disclosed. The propulsive anti-torque system includes an anti-torque thruster system in which a variable pitch fan is installed internal to the tail boom of the rotorcraft and an anti-torque thruster nozzle is mounted at the extremity of the tail boom. The fan is driven directly from the main rotor drive. The configuration and location of the fan allows the primary exhaust from the engine to be mixed with the compressed air flow from the fan. The mixed air flow from the fan and the engine passes through the tail boom and out the thruster nozzle.
摘要翻译: 公开了一种具有增强结构的旋翼航空器,其中简单翼和推进式反扭矩系统组合在一起。 推进式反扭矩系统包括抗扭矩推进器系统,其中可变桨距风扇安装在旋翼航空器尾翼的内部,反扭矩推进器喷嘴安装在尾吊臂的末端。 风扇直接从主转子驱动器驱动。 风扇的配置和位置允许来自发动机的主排气与来自风扇的压缩空气流混合。 来自风扇和发动机的混合空气流通过尾部悬臂并从推进器喷嘴出来。
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公开(公告)号:US08939399B2
公开(公告)日:2015-01-27
申请号:US13563086
申请日:2012-07-31
申请人: Areian Kouros , Roger Aubert , Paul Madej
发明人: Areian Kouros , Roger Aubert , Paul Madej
CPC分类号: B64C27/12 , B64D27/24 , B64D2027/026 , Y02T50/64
摘要: The present application relates to a regenerative or hybrid drive system for an aircraft. The drive system includes the use of a power augmentation device to selectively engage the drive system of an aircraft to store power. The power in the power augmentation device being configured to release a power burst to systems within the aircraft to perform critical flight maneuvers.
摘要翻译: 本申请涉及用于飞机的再生或混合驱动系统。 驱动系统包括使用功率增加装置来选择性地接合飞行器的驱动系统以存储动力。 功率增加装置中的功率被配置为向飞行器内的系统释放功率突发以执行关键的飞行操纵。
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公开(公告)号:US20140034781A1
公开(公告)日:2014-02-06
申请号:US13563086
申请日:2012-07-31
申请人: Areian Kouros , Roger Aubert , Paul Madej
发明人: Areian Kouros , Roger Aubert , Paul Madej
IPC分类号: B64D35/08
CPC分类号: B64C27/12 , B64D27/24 , B64D2027/026 , Y02T50/64
摘要: The present application relates to a regenerative or hybrid drive system for an aircraft. The drive system includes the use of a power augmentation device to selectively engage the drive system of an aircraft to store power. The power in the power augmentation device being configured to release a power burst to systems within the aircraft to perform critical flight maneuvers.
摘要翻译: 本申请涉及用于飞机的再生或混合驱动系统。 驱动系统包括使用功率增加装置来选择性地接合飞行器的驱动系统以存储动力。 功率增加装置中的功率被配置为向飞行器内的系统释放功率突发以执行关键的飞行操纵。
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