CN102700719A - 飞机减速发电机 - Google Patents

飞机减速发电机 Download PDF

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CN102700719A
CN102700719A CN2012101757325A CN201210175732A CN102700719A CN 102700719 A CN102700719 A CN 102700719A CN 2012101757325 A CN2012101757325 A CN 2012101757325A CN 201210175732 A CN201210175732 A CN 201210175732A CN 102700719 A CN102700719 A CN 102700719A
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aircraft
belt
airplane
electrical generator
deceleration
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田太康
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Abstract

目前国内外的军民两用机场飞机着陆都是在跑道上滑行、刹车和空气阻力来消耗飞机着陆时的强大惯性。本发明用飞机减速发电机来达到以下目的:1、可发电节能;2、可大幅度缩短机场驱道,节约机场造价和成本。飞机减发电机。原理同“跑步机”只是因飞机较重,在皮带下须设密集的轴承阵列,以能担负飞机的重量和冲击力,飞机着陆后滑行到减速发电机皮带上,飞机轮子与皮带的摩擦力较大,由此带动皮带高速反向转动发电,而飞机在皮带上对跑道相对静止不动。与发明“飞机永磁悬浮电磁弹射平台”结合,解决一切机场的飞机起降问题,可极大地缩短机场跑道,给机场设施带来革命性的改进。技术成熟后可用于我国南海小岛军用机场的建设或用于“航母”。

Description

飞机减速发电机
技术领域:
本发明属飞机着陆着舰系统,它的原理是将飞机着陆着舰时的强大惯性通过飞机减速发电机转换为电能,在短距离、短时间内使飞机安全着陆着舰,又能发电。 
背景技术:
目前世界各国的军民用机场飞机降落都在机场跑道滑行,利用空气阻力刹车和飞机轮胎对跑道的摩擦力来逐步消耗飞机着陆时的强大惯性。本发明用飞机减速发电机来消耗飞机着陆着舰时的强大惯性。将飞机着陆着舰时的强大惯性利用飞机减速发电机转换成电能。又能缩短机场跑道,提高飞机进场的安全性,决不会出现飞机冲出跑道的事故。为达以上目的,发明内容如下: 
发明内容:
飞机从机场迎风着陆后,在它的前方,机场跑道三分之一处,与跑道水平一致,做一长50米宽12米的皮带轮,皮带下设密集的轴承及轴承座,下设承重梁。飞机着陆成功后,通过一段较短的滑行到达“减速发电机”上,因“减速发电机”的皮带与飞机轮胎的摩擦力大,皮带与轴承的摩擦力小,飞机轮胎虽在高速运转,但飞机确纹丝不动,这种惯性力完全消耗在“减速发电机”上,对飞机不产生一切破坏力。“减速发电机”皮带高速运转而发电,给飞机留下一点惯性时停止。让飞机自动离开减速发电机和归位。在三分钟左右的时间内迎接下一架次各种类型飞机的降落。对飞机“减速发电机”不会有太多特殊的要求。只是皮带的速度快,在皮带的下段回程处,须设几处降温设施。皮带的磨损较大,设计时须考虑便于更换和维护。飞机轮胎在“减速发电机”上高速转动,而减速发电机的皮带高速反向运动。这好比汽车打滑一样,以此来消耗它的惯性,完全可用这种强力发电,以减少机场用电需求,以达节能之目的。 
用此设施可保证飞机不会冲出跑道,确保飞机安全,这项发明在飞机场实用,技术成熟后,能确保两三百米内安全降落飞机,一可缩短机场跑道,二可直接在航母上使用。 
附图说明:
图1机场略图:1机场;2飞机减速发电机;3塔台;4机场跑道。 
图2皮带下轴承,轴承平台的俯视图:1轴承;2轴承平台 
图3飞机减速发电机的剖视图:1轴承;3皮带;4轴承座;5皮带轮;6机场跑道;7发电机;8承重支架;9承重梁;10基础;11制动12水沟;13钢筋混凝土;14散热 
具体实施方式:
飞机减速发电机:在机场三分之一处挖一长53米、宽15米、深6米的沟槽。用钢筋混凝土做好基础,边墙,净空尺寸50.5×12.5×3.5米(长、宽、高)。按图3,做好飞机减速发电机,尺寸50×12×3米(长、宽、高),与跑道水平一致即可。飞机减速发电机按500吨荷载力学设计,模块化由工厂生产、现场组装即可使用。 

Claims (2)

1.目前世界各国的军民用机场飞机降落都在机场跑道滑行,利用空气阻力,刹车和飞机轮胎对跑道的摩擦力来逐步消耗飞机着陆时的强大惯性。本发明用飞机减速发电机来消耗飞机着陆着舰时的强大惯性。将飞机着陆着舰时的强大惯性利用飞机减速发电机转换成电能。又能缩短机场跑道,提高飞机进场的安全性,决不会出现飞机冲出跑道的事故。
2.利用飞机着陆的强大惯性发电,减速的飞机减速发电机。
从属权利:
飞机从机场迎风着陆后,在它的前方,机场跑道三分之一处,与跑道水平一致,做一长50米宽12米的皮带轮,皮带下设密集的轴承及轴承座,下设承重梁。飞机着陆成功后,通过一段较短的滑行到达“减速发电机”上,因“减速发电机”的皮带与飞机轮胎的摩擦力大,皮带与轴承的摩擦力小,飞机轮胎虽在高速运转,但飞机确纹丝不动,这种惯性力完全消耗在“减速发电机”上,对飞机不产生一切破坏力。“减速发电机”皮带高速运转而发电,给飞机留下一点惯性时停止。让飞机自动离开减速发电机和归位。在三分钟左右的时间内迎接下一架次各种类型飞机的降落。对飞机“减速发电机”不会有太多特殊的要求。只是皮带的速度快,在皮带的下段回程处,须设几处降温设施。皮带的磨损较大,设计时须考虑便于更换和维护。飞机轮胎在“减速发电机”上高速转动,而减速发电机的皮带高速反向运动。这好比汽车打滑一样,以此来消耗它的惯性,完全可用这种强力发电,以减少机场用电需求。
CN2012101757325A 2012-05-23 2012-05-23 飞机减速发电机 Pending CN102700719A (zh)

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Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103587711A (zh) * 2013-04-28 2014-02-19 叶元华 一种拦阻器及安装拦阻器的跑道
CN104002983A (zh) * 2014-05-30 2014-08-27 陈亮 一种飞行器起降装置
CN105197250A (zh) * 2015-10-08 2015-12-30 叶元华 一种浮动降落平台

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6969213B2 (en) * 2003-02-24 2005-11-29 Omnitek Partners, Llc Roadway for decelerating and/or accelerating a vehicle including an aircraft
CN101238031A (zh) * 2005-06-13 2008-08-06 波音公司 具有动力装置的前机身航空器轮子系统
US20080258014A1 (en) * 2007-04-20 2008-10-23 The Boeing Company Aircraft kinetic landing energy conversion system
US20090076668A1 (en) * 2007-09-14 2009-03-19 Airbus Uk Limited Method and apparatus for providing power in an aircraft to one or more aircraft systems
GB2460132A (en) * 2008-12-23 2009-11-25 Qingchang Zhong A system and a method for converting the kinetic energy stored in landing aircraft into electricity

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6969213B2 (en) * 2003-02-24 2005-11-29 Omnitek Partners, Llc Roadway for decelerating and/or accelerating a vehicle including an aircraft
CN101238031A (zh) * 2005-06-13 2008-08-06 波音公司 具有动力装置的前机身航空器轮子系统
US20080258014A1 (en) * 2007-04-20 2008-10-23 The Boeing Company Aircraft kinetic landing energy conversion system
US20090076668A1 (en) * 2007-09-14 2009-03-19 Airbus Uk Limited Method and apparatus for providing power in an aircraft to one or more aircraft systems
GB2460132A (en) * 2008-12-23 2009-11-25 Qingchang Zhong A system and a method for converting the kinetic energy stored in landing aircraft into electricity

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103587711A (zh) * 2013-04-28 2014-02-19 叶元华 一种拦阻器及安装拦阻器的跑道
CN104002983A (zh) * 2014-05-30 2014-08-27 陈亮 一种飞行器起降装置
CN105197250A (zh) * 2015-10-08 2015-12-30 叶元华 一种浮动降落平台

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Application publication date: 20121003