CN103723282A - 碟形航空母舰 - Google Patents

碟形航空母舰 Download PDF

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Publication number
CN103723282A
CN103723282A CN201210422514.7A CN201210422514A CN103723282A CN 103723282 A CN103723282 A CN 103723282A CN 201210422514 A CN201210422514 A CN 201210422514A CN 103723282 A CN103723282 A CN 103723282A
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deck
dish
aircraft
take
shipboard
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CN201210422514.7A
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刘君才
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Abstract

本发明是一种碟形航空母舰,其三体式船身上有直径≥400米的圆盘形甲板,其盘缘为环形起飞甲板,其长度近似无限,故可不用弹射器类助飞装置,由系留装置联接舰载机和环形滑轨,以便舰载机在环形起飞甲板上盘绕起飞,待舰载机脱离环形起飞甲板后,系留装置才解锁使舰载机脱缰而去,中小型舰载机只需盘绕一圈即可起飞,重型舰载机盘绕2~3圈即可起飞,且可同时起飞多架同型号舰载机。

Description

碟形航空母舰
技术领域
本发明是一种航空母舰,特指一种碟形航空母舰。 
背景技术
现有的航空母舰因本身结构限制,其飞行甲板很短,使舰载机要借助滑跃甲板或弹射器才能起飞。 
发明内容
本发明是一种采用环形起飞甲板的碟形航空母舰。 
其技术方案是,三体式航空母舰的甲板呈园盘形,盘缘为环形起飞甲板,其内侧有与甲板平齐的环形滑轨,由系留装置联接环形滑轨和舰载机,以防舰载机在环形起飞甲板上盘绕起飞时掉入海中,当舰载机盘绕起飞至机轮脱离环形起飞甲板后,系留装置解锁使舰载机脱缰而去,其优点是,环形起飞甲板长度近似无限,故不用弹射器助飞,结构简单、高效,可一次同时起飞多架相同的航载机。 
具体实施方式
本发明的碟形航空母舰,其三体式船身上有直径≥400米的园盘形甲板,故其周长在1千多米,盘缘为60米宽的环形起飞甲板,其内侧有与甲板平齐的环形滑轨,由高强度钢管做成直径约380米的园环,其表面镀銦铅合金,系留装置由绞车、高强度钢索及爪形电磁 锁和滑块组成,钢索头A接爪形滑块,以沿环形滑轨滑行,钢索头B接爪形电磁锁,以临时固定在起落架上,调节绞车使钢索绷直,舰载机即可准备盘绕起飞了。 
园盘形甲板中间有2条直线形降落甲板,降落甲板长度均在200米以上,并配有多重阻拦索,以便舰载机高低速均可安全降落,如再配上弹射器,且降落甲板亦可起飞舰载机。 

Claims (2)

1.一种碟形航空母舰,由三体式船身、大直径园盘形甲板、环形滑轨及系留装置组成,其特征是:园盘形甲板边缘的环形起飞跑道内侧有环形滑轨。
2.如权利要求1所述的碟形航空母舰,其特征是:可调长度的系留装置由绞车、钢索、爪形电磁锁和爪形滑块组成。
CN201210422514.7A 2012-10-13 2012-10-13 碟形航空母舰 Pending CN103723282A (zh)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201210422514.7A CN103723282A (zh) 2012-10-13 2012-10-13 碟形航空母舰

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201210422514.7A CN103723282A (zh) 2012-10-13 2012-10-13 碟形航空母舰

Publications (1)

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CN103723282A true CN103723282A (zh) 2014-04-16

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Family Applications (1)

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CN201210422514.7A Pending CN103723282A (zh) 2012-10-13 2012-10-13 碟形航空母舰

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CN (1) CN103723282A (zh)

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3325124A (en) * 1966-02-24 1967-06-13 Woldemar A Bary Closed track airport with inlet runways for straight instrument landings
US3877664A (en) * 1972-04-19 1975-04-15 France Etat Mooring device
US3923274A (en) * 1974-03-07 1975-12-02 Dornier Gmbh Device for centering and arresting an aircraft positioned on a take-off and landing platform and starting therefrom and landing thereon
US4709883A (en) * 1985-04-22 1987-12-01 Giuliani Robert L Launch and ascent system
CN202115693U (zh) * 2011-04-07 2012-01-18 上海市枫泾中学 碳纤碟形攻击型航母

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3325124A (en) * 1966-02-24 1967-06-13 Woldemar A Bary Closed track airport with inlet runways for straight instrument landings
US3877664A (en) * 1972-04-19 1975-04-15 France Etat Mooring device
US3923274A (en) * 1974-03-07 1975-12-02 Dornier Gmbh Device for centering and arresting an aircraft positioned on a take-off and landing platform and starting therefrom and landing thereon
US4709883A (en) * 1985-04-22 1987-12-01 Giuliani Robert L Launch and ascent system
CN202115693U (zh) * 2011-04-07 2012-01-18 上海市枫泾中学 碳纤碟形攻击型航母

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Application publication date: 20140416