| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 61 | STABLE OFFSHORE FLOATING DEPOT | EP12822127 | 2012-02-09 | EP2741955A4 | 2016-01-13 | VANDENWORM NICOLAAS |
| An offshore depot having a vertically symmetric hull, an upper inwardly-tapered wall and a lower outwardly-tapered wall that produce significant heave damping in response to heavy wave action. Ballast is added to the lower and outermost portions of the hull to lower the center of gravity below the center of buoyancy. The offshore depot includes a tunnel formed within or through the hull at the waterline that provides a sheltered area inside the hull for safe and easy launching/docking of boats and embarkation/debarkation of personnel. When the watertight tunnel doors are all shut, the tunnel may be drained to create a dry dock environment within the hull. The offshore depot includes berthing and dinning accommodations, medical facilities, workshops, machine shops, a heliport, and the like. | ||||||
| 62 | LIFT ARRANGEMENTS | EP99913465.3 | 1999-03-26 | EP1066193A1 | 2001-01-10 | SEYFANG, George R.,British Aerospace; HUNTER, Christopher J.,British Aerospace |
| A lift arrangement for conveying a load between two levels in a lift shaft (14), said lift arrangement comprising two platform (16, 18) means each mounted for movement within said lift shaft (14) between one level (10) and the other (12), each platform means being changeable between a load-carrying configuration in which it extends across a substantial extent of the lift shaft (14), and a bypass configuration in which it allows the other floor means to pass it when in a load carrying configuration. | ||||||
| 63 | Aircraft handling and/or storage apparatus | EP96302855.0 | 1996-04-24 | EP0739813A1 | 1996-10-30 | Drinkwater, Paul Jefferson, British Aero. Def. Ltd; Whaites, Colin, British Aerospace Defence Limited |
Aircraft lift apparatus (12) for an aircraft-carrying vessel, for transferring an aircraft between the flight deck and a storage area below said flight deck, said apparatus including means for tilting the aircraft (14) about an axis (16) thereby to reduce the effective width of the aircraft (22), and lift means (10) for moving the aircraft between said flight deck and said storage area. |
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| 64 | Dynamic load compensating apparatus | EP86307268.2 | 1986-09-22 | EP0218405A2 | 1987-04-15 | Cherbonnier, T. Dave |
A dynamic load compensation system comprises:
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| 65 | Aircraft stores handling apparatus and system | EP80304426.2 | 1980-12-08 | EP0031212B1 | 1984-10-17 | Deady, Martin Albert |
| 66 | Landing pad and hangar structure for vertical take-off and landing aircraft | EP80304482.5 | 1980-12-11 | EP0030849B1 | 1984-04-04 | Akerman, Moshe; Saly, Amnon |
| 67 | DEVICE FOR PROPELLING AND TURNING HULL | PCT/KR2013005635 | 2013-06-26 | WO2014003427A1 | 2014-01-03 | SONG GYUNG JIN; SONG YOUNG SICK; SONG WON GI; SONG WON CHAN; SONG JUNG SIK; SONG IN JUNG; CHAE JE WAN; CHAE HEON |
| The present invention relates to a device for propelling and turning a hull, wherein the resistance acting on the stem of the hull is converted and the hull can be moved not only in the forward and backward directions but also in the left and right directions so as to improve the mobility and evasion capacity of the hull. The device for propelling and turning a hull comprises: a manifold arranged in the lengthwise direction in the lower portion of the hull so as to discharge the water introduced at the stem side toward the stern side; a propelling means, the top of which is rotatably connected to the stern side end of the manifold, the propelling means being arranged so as to jet water in a lateral direction; and a steering means, which is rotatably coupled to the stern side end of the propelling means such that the steering means rotates the propelling means in a given direction by means of rotating force applied from an external source. | ||||||
| 68 | A CARRIER-BORNE AIRCRAFT TAKEOFF/LANDING SYSTEM AND METHODS OF USING THE SAME | PCT/IB2010000886 | 2010-03-10 | WO2010113030A3 | 2011-05-12 | WANG LIFENG |
| The present invention provides a carrier-borne aircraft takeoff/landing system comprising a takeoff auxiliary mechanism and/or an integrated runway which are/is positioned on the aircraft carrier. The takeoff auxiliary mechanism can be a sliding vehicle or a simple pendulum type projectile mechanism, the integrated runway is a carrier-borne aircraft runway which can be extended out of the aircraft carrier. The carrier-borne aircraft takeoff/landing system of the present invention concentrates the advantages of current ways of catapult launch and ski-jump takeoff and abandons the faults existed, which can reduce the difficulties and risks involved during the traditional landing. The takeoff/landing system which is outstanding for its simple structure, significantly reduced research cost and energy consumption, with improved efficiency, easy operation and maintenance, high reliability, which are applicable to various carrier-borne aircraft for take off and/or landing. | ||||||
| 69 | 双层飞行甲板概念的航空母舰 | CN200920149309.1 | 2009-04-08 | CN201437404U | 2010-04-14 | 王石诚 |
| 本实用新型是一种双层飞行甲板概念的航空母舰，其主要是在航空母舰原飞行甲板上，加盖第二层飞行甲板，进而形成具双层飞行甲板的设计，飞机的起飞降落可以分开在不同层的甲板上作业，起飞降落不会互相干扰，任务单纯的多也安全的多，并在增加少许建造费用即可使航空母舰增加将近2倍的操作空间和容量，并在飞行甲板上，设有跑道缓冲装置，以用来减少飞机降落时所需要的跑道滑行长度以及减缓飞机冲行的速度，可增加安全性和人员操作上的容易度，同时在原飞行甲板以及第二层飞行甲板一侧，设有向外延伸凸出于甲板外的升降机平台，以做为两层飞行甲板以及最下层停机棚间飞机运送移动的目的。 | ||||||
| 70 | 可伸出航母舰体外的舰载机跑道 | CN200920148915.1 | 2009-04-03 | CN201385772Y | 2010-01-20 | 王力丰 |
| 本实用新型是一种可伸出航母舰体外的舰载机跑道，在航母的甲板上设有整体式舰载机跑道，在航母舰体内设有驱动机构驱动该跑道滑动，使该跑道的一部分伸出到舰体外；在该跑道的下面设有升降式甲板，该甲板用于填补该跑道一部分伸出舰外后舰上留下的空缺，该跑道与该甲板相互配合拼接后，形成一条平坦的加长的舰载机跑道；该跑道伸出舰外悬于海面部分由浮船及若干个临时漂浮物支撑，该跑道的伸出或收回是依靠驱动机构的驱动和/或由浮船的辅助推拉。一种可伸出航母舰体外的舰载机跑道，可降低了航母舰载机起飞和降落的难度和风险。 | ||||||
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