CN103863537A - Aircraft carrier hull with double-deck flight deck - Google Patents
Aircraft carrier hull with double-deck flight deck Download PDFInfo
- Publication number
- CN103863537A CN103863537A CN201210531863.2A CN201210531863A CN103863537A CN 103863537 A CN103863537 A CN 103863537A CN 201210531863 A CN201210531863 A CN 201210531863A CN 103863537 A CN103863537 A CN 103863537A
- Authority
- CN
- China
- Prior art keywords
- deck
- flight deck
- cabin
- double
- hatch door
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
Images
Landscapes
- Cage And Drive Apparatuses For Elevators (AREA)
Abstract
The invention discloses an aircraft carrier hull with a double-deck flight deck. The aircraft carrier hull with the double-deck flight deck comprises an upper main flight deck (2) and a lower assistant flight deck cabin (6), and a cabin door (3) device is mounted at the front end. A layer under the lower assistant flight deck cabin comprises a plane warehouse (12) and four elevator entrances (5). Above the cabin door (3), an iron and steel hinge (11) is fixed at the front end of the main flight deck (2) through screws, recess (10) components with holes are welded at each of two sides of the cabin door and are connected with bumps with holes at two ends of a hydraulic telescopic rod (9) by iron pins, and the other ends are in lock connection with a recess (10) of the assistant flight deck cabin (6) by iron pins, and the recess is provided with holes. By means of said structure, the double-deck flight deck is capable of working simultaneously to enable a shipboard aircraft to take off, and the fighting capacity is formed quickly.
Description
Technical field
The invention relates to a kind of double-deck flight deck aircraft carrier hull, its objective is the novel aircraft carrier of making an independent creation of orthodox school.
Background technology
Aircraft carrier and carrier-borne aircraft portion fly with two kinds of catapult-assisted take-offs as main flow take sliding jumping up in the world at present, existing short distance vertical takeoff and landing deck aircraft carrier and oblique landing deck is housed drives the aircraft carrier of taking off by catapult-launching gear, current powerful 100,000 tons of atomic aircrafts of U.S.'s Nimitz level that belong to.
Along with national economic strength increases, government has a mind to develop aircraft carrier and strengthens national defence.And national military equipment is mainly with Su Shiwei master, comprise watt good lattice number old aircraft carrier hull buying.Therefore, as a demobilized old soldier's patriotic thought, resolve to want independent innovation, invent a kind of double-deck flight deck aircraft carrier hull, be used for becoming and establish Chinese and can independently establish an image.It is than other many one decks of aircraft carrier flight deck that the present invention innovates aircraft carrier feature, if and partly hereby level aircraft carrier comparison of the Buddhist nun of the U.S., equal or be less than this tonnage at displacement tonnage, the invention aircraft carrier quantitatively obviously wants many at carrier-borne aircraft, if same development adopts nuclear power source and catapult-launching gear technology, its fighting capacity Superiority Promoting will be more outstanding than it.
Summary of the invention
The invention is a kind of double-deck flight deck aircraft carrier hull, it is characterized in that the secondary flight deck cabin of the main flight deck in upper strata and lower floor, and front end is all connected with hatch door, by hydraulic efficiency gear by hatch door opening and closing.Lower floor is aircraft warehouse again, and ship-board aircraft can be by four elevators in and out of upper strata cabin and the main flight deck of top layer.
The main flight deck in described upper strata, is characterized in that: the past to afterbody is full through type landing aircraft platform.Front end is connected with hatch door, opens with main flight deck and lifts and form 15 ° of angles when hatch door, and aircraft can be slided to jump up in the above and fly, or utilizes ejector power to take off.Be positioned at board and have island shape bridge and direct tower.Deck topside can be installed quadruplet elevator altogether, for aircraft provides deliver from vault and recovery operation condition.Deck afterbody can be installed multiple tracks and block steel cable, specially for aircraft provides landing platform.
The lower floor of the main flight deck in described upper strata is the cabin of secondary flight deck cabin sealing, can serve as at ordinary times hangar and use.Front end exit is mounted with hatch door, can be by hydraulic efficiency gear by hatch door opening and closing.Two cover catapult-launching gears can be installed in front portion, deck, can utilize to launch to exit and take off, or do not use catapult-launching gear at hatch door unlatching aircraft, and short distance vertical take-off and landing aircraft (VTOL aircraft) also can be exported and be taken off by hatch door.There is the outlet of four elevators on both sides, cabin deck, and aircraft can fall the machine lower deck on hand of coming in and going out by length.
The main flight deck in described upper strata and lower floor's flight deck cabin, front end is all connected with hatch door.The main flight deck front end in upper strata is provided with the iron and steel hinge interlinkage being screwed and connects, and iron and steel hinge interlinkage another side is to be screwed hatch door top, and hatch door both sides are welded with eyelet dimple parts.Be connected with iron pin with the perforated protuberance in hydraulic rod reducing two, other end and cabin deck are welded perforated concave bottom seat iron lock and are lived together with limit.In hydraulic stem effect, hatch door is opened, lifted and form 15 ° of angles with the main flight deck in upper strata, facilitate aircraft to slide to jump up in the above and fly.
Accompanying drawing explanation
Fig. 1 is front view of the present invention.
Fig. 2 is the main aircraft deck plan sketch in upper strata of the present invention.
Fig. 3 is hatch door structural representation of the present invention.
(1) hull.(2) the main flight deck in upper strata.(3) hatch door.(4) direct tower.(5) lifting and device.(6) the secondary flight deck cabin of lower floor.(7) block steel cable.(8) catapult-launching gear.(9) hydraulically extensible bar.(10) dimple parts.(11) iron and steel hinge interlinkage.(12) hangarage.
The specific embodiment
Press shown in Fig. 1 to Fig. 3, for the specific embodiments of the double-deck flight deck aircraft carrier hull of the invention (1), it comprises the main flight deck in upper strata (2) and the secondary flight deck cabin of lower floor (6), front end at ordinary times hatch door (3) in closing, by hydraulic efficiency gear (9) by hatch door opening and closing.
Send instruction when being positioned at board direct tower (4), aircraft carrier is in the Job readiness that takes off.The main flight deck in upper strata (2) front end hatch door (3) upwardly opens under hydraulically extensible bar (9) thrust, lifts with main flight deck (2) and forms 15 ° of angles.The aircraft of hangar (12) and secondary flight deck cabin (6) the inside rises to main flight deck (2) by elevator (5), and aircraft can be slided to jump up and fly.If utilize catapult-launching gear (8), hatch door is not opened aircraft and can be taken off yet.Rear portion, deck can arrange several roads and block steel cable (7) and provide the platform of landing for aircraft, and when blocking no success, complete straight-through main flight deck (2) also can make aircraft accelerate heavily to fly.
Pass through hydraulic stem (9) under the effect of iron and steel hinge interlinkage (11) and dimple parts (10) when obtaining the secondary flight deck cabin of instruction lower floor (6), hatch door (3) is opened, and aircraft can be taken off to hatch door outlet by ejection machine (8).Short distance vertical take-off and landing aircraft (VTOL aircraft) is not used ejector can take off equally.When aircraft carrier is during in aircraft landing recovery operation, elevator (5) can be sent the aircraft of main upper strata aircraft deck (2) landing back to the secondary flight deck cabin of lower floor (6) and lower floor's hangarage (12) again.The secondary flight deck cabin (6) that occupies aircraft also can serve as hangar and use.Now hatch door (3) is closed under hydraulically extensible bar (9) uses, and aircraft carrier takes off, and landing recovery operation finally completes.
Claims (4)
1. a double-deck flight deck aircraft carrier hull, comprise double-deck flight deck hull (1), the main flight deck in upper strata (2), the secondary flight deck cabin of lower floor (6), front end cabin door device (3), lower floor's hangarage (12) again, both sides, cabin deck are totally four elevator gangways (5).
2. double-deck flight deck aircraft carrier hull according to claim 1, it is characterized in that: the main flight deck in described upper strata (2), it is full through type takeoff and landing platform from tail end to front end, postmedian deck is wider than front end deck, and deck front end equates with the hatch door being connected (3) length and width.Being positioned at board is island formula bridge direct tower (4) on one side, and deck two sides of a ship have four elevator gangways (5).
3. double-deck flight deck aircraft carrier hull according to claim 2, it is characterized in that: the secondary flight deck cabin of the main flight deck in described upper strata (2) lower floor (6), it is the complete straight-through closed cabin of flight deck from tail end to front end, postmedian cabin is wider than front end cabin, front end is connected with hatch door (3) by hydraulically extensible bar (9), and cabin both sides have four elevator gangways (5).
4. according to the described double-deck flight deck side of a ship lash ship body of claim 2 and 3, it is characterized in that: described cabin door device (3).The main flight deck in upper strata (2) front end is screwed iron and steel hinge interlinkage (11) and is connected with being equipped with, iron and steel hinge interlinkage (11) another side is screwed in the top of hatch door (3), there are dimple (10) parts of welding with eyelet on hatch door (3) both sides, live with iron lock with the perforated protuberance in hydraulically extensible bar (9) two, other end and secondary flight deck cabin (6) are welded with eyelet concave bottom seat (10) parts iron lock and live.Under hatch door (3) hydraulically extensible bar (9) thrust, open, lift and form 15 ° of angles with the main flight deck in upper strata (2), withdrawal can be closed hatch door.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201210531863.2A CN103863537A (en) | 2012-12-12 | 2012-12-12 | Aircraft carrier hull with double-deck flight deck |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201210531863.2A CN103863537A (en) | 2012-12-12 | 2012-12-12 | Aircraft carrier hull with double-deck flight deck |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN103863537A true CN103863537A (en) | 2014-06-18 |
Family
ID=50902679
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201210531863.2A Pending CN103863537A (en) | 2012-12-12 | 2012-12-12 | Aircraft carrier hull with double-deck flight deck |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN103863537A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107539491A (en) * | 2017-06-09 | 2018-01-05 | 石福军 | A kind of aircraft carrier main body and its auxiliary device |
| CN107554809A (en) * | 2017-09-11 | 2018-01-09 | 荆门创佳机械科技有限公司 | Aircraft carrier hoistable platform based on linear electric motors driving |
| CN107685844A (en) * | 2017-07-11 | 2018-02-13 | 丁乃祥 | Multi-functional aircraft carrier |
Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2146430Y (en) * | 1990-11-19 | 1993-11-17 | 唐全国 | Aircraft-carrier flight deck |
| CN201437404U (en) * | 2009-04-08 | 2010-04-14 | 王石诚 | Aircraft carrier with dual-layer flight deck concept |
| RU2390462C1 (en) * | 2009-03-13 | 2010-05-27 | Эдуард Дмитриевич Житников | Small two-deck aircraft carrier |
| CN102079380A (en) * | 2010-09-17 | 2011-06-01 | 朱惠芬 | Navigation submarine ship with hydrofoil power cabins |
| CN102139752A (en) * | 2010-02-03 | 2011-08-03 | 陈世文 | Novel aircraft carrier |
| CN201989937U (en) * | 2011-01-06 | 2011-09-28 | 吕宝林 | Miniature aircraft carrier |
| CN202439835U (en) * | 2012-01-18 | 2012-09-19 | 郝安阶 | Aircraft carrier |
| CN102730174A (en) * | 2011-04-07 | 2012-10-17 | 上海市枫泾中学 | Carbon fiber disk-shaped attack-type aircraft carrier |
| CN102765468A (en) * | 2012-06-29 | 2012-11-07 | 北京科实医学图像技术研究所 | Novel design scheme for aircraft carrier runways |
-
2012
- 2012-12-12 CN CN201210531863.2A patent/CN103863537A/en active Pending
Patent Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2146430Y (en) * | 1990-11-19 | 1993-11-17 | 唐全国 | Aircraft-carrier flight deck |
| RU2390462C1 (en) * | 2009-03-13 | 2010-05-27 | Эдуард Дмитриевич Житников | Small two-deck aircraft carrier |
| CN201437404U (en) * | 2009-04-08 | 2010-04-14 | 王石诚 | Aircraft carrier with dual-layer flight deck concept |
| CN102139752A (en) * | 2010-02-03 | 2011-08-03 | 陈世文 | Novel aircraft carrier |
| CN102079380A (en) * | 2010-09-17 | 2011-06-01 | 朱惠芬 | Navigation submarine ship with hydrofoil power cabins |
| CN201989937U (en) * | 2011-01-06 | 2011-09-28 | 吕宝林 | Miniature aircraft carrier |
| CN102730174A (en) * | 2011-04-07 | 2012-10-17 | 上海市枫泾中学 | Carbon fiber disk-shaped attack-type aircraft carrier |
| CN202439835U (en) * | 2012-01-18 | 2012-09-19 | 郝安阶 | Aircraft carrier |
| CN102765468A (en) * | 2012-06-29 | 2012-11-07 | 北京科实医学图像技术研究所 | Novel design scheme for aircraft carrier runways |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107539491A (en) * | 2017-06-09 | 2018-01-05 | 石福军 | A kind of aircraft carrier main body and its auxiliary device |
| CN107685844A (en) * | 2017-07-11 | 2018-02-13 | 丁乃祥 | Multi-functional aircraft carrier |
| CN107685844B (en) * | 2017-07-11 | 2019-03-19 | 丁乃祥 | Multi-functional aircraft carrier |
| CN107554809A (en) * | 2017-09-11 | 2018-01-09 | 荆门创佳机械科技有限公司 | Aircraft carrier hoistable platform based on linear electric motors driving |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US8453963B2 (en) | Amphibious large aircraft without airstairs | |
| CN103863537A (en) | Aircraft carrier hull with double-deck flight deck | |
| CN201437404U (en) | Aircraft carrier with dual-layer flight deck concept | |
| CN102826231A (en) | Slope downward-sliding takeoff platform for carrier-based aircraft, application aircraft carrier and realization method | |
| CN104760705A (en) | Vehicle-mounted aircraft taking-off and landing device | |
| CN107985506A (en) | A kind of total arrangement suitable for 10,000 tons bulk freighter | |
| US3361274A (en) | Lighter lifting and stacking devices | |
| CN107487424A (en) | A kind of spacecraft sea recovery method and equipment | |
| CN104828257A (en) | Layout scheme for carrier-based aircraft hangars of aircraft carrier | |
| CN203047533U (en) | Slope-gliding launching platform for shipboard aircraft, and application aircraft carrier | |
| CN208102251U (en) | A kind of total arrangement suitable for 10,000 tons bulk freighter | |
| US2425972A (en) | Aircraft construction for handling cargo | |
| DE3011542A1 (en) | Hatch covers for container ship - has support beams bridging hatch for over-deck loading | |
| CN104085538B (en) | A kind of sea, common naval vessel unmanned aerial vehicle closely landing gear | |
| CN205061263U (en) | Lift cage | |
| US1896546A (en) | Floating airport | |
| CN211918935U (en) | Container ship based on anti-collision wall cabin front mooring equipment sinking type design | |
| EP1955943B1 (en) | Transport ship, in particular cargo ship | |
| DE69924405T2 (en) | LIFEBOAT SYSTEM | |
| CN106741624B (en) | Bulk cargo ship hatch coaming and ship opening longitudinal girder with total strength being completely taken into account | |
| CN202953144U (en) | Ocean engineering ship | |
| CN106476985B (en) | Bulk cargo ship hatch coaming with partial total strength and ship opening longitudinal girder | |
| CN209305804U (en) | Lander is laid and recovery system | |
| CN207141421U (en) | A kind of aircraft carrier main body provided with auxiliary device | |
| CN207374616U (en) | A kind of spacecraft sea recovery gear |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| DD01 | Delivery of document by public notice |
Addressee: Lu Zhengan Document name: the First Notification of an Office Action |
|
| DD01 | Delivery of document by public notice |
Addressee: Lu Zhengan Document name: Notification that Application Deemed to be Withdrawn |
|
| WD01 | Invention patent application deemed withdrawn after publication | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20140618 |