CN107472549A - A kind of aircraft carrier alighting deck and its application method - Google Patents
A kind of aircraft carrier alighting deck and its application method Download PDFInfo
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- CN107472549A CN107472549A CN201710684142.8A CN201710684142A CN107472549A CN 107472549 A CN107472549 A CN 107472549A CN 201710684142 A CN201710684142 A CN 201710684142A CN 107472549 A CN107472549 A CN 107472549A
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- alighting deck
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- 238000000034 method Methods 0.000 title claims abstract description 11
- 230000001360 synchronised effect Effects 0.000 claims description 7
- 230000009471 action Effects 0.000 claims description 2
- 230000007246 mechanism Effects 0.000 description 4
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 4
- 238000010586 diagram Methods 0.000 description 2
- 239000000463 material Substances 0.000 description 2
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- 235000007164 Oryza sativa Nutrition 0.000 description 1
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- 230000034994 death Effects 0.000 description 1
- 231100000517 death Toxicity 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 230000002085 persistent effect Effects 0.000 description 1
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- 235000009566 rice Nutrition 0.000 description 1
- 230000006641 stabilisation Effects 0.000 description 1
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
- B64F1/02—Ground or aircraft-carrier-deck installations for arresting aircraft, e.g. nets or cables
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
- B64F1/002—Taxiing aids
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Abstract
The invention provides a kind of aircraft carrier alighting deck and its application method, is related to aircraft-carrier-deck facility technology field, solves the technical problems such as aircraft carrier landing runway in the prior art is too short, landing difficulty is larger, security incident is multiple.The device includes main alighting deck, and airstrips are provided with main alighting deck；Telescopic service deck is provided with main alighting deck airstrips direction, drive device is provided between the main alighting deck and the service deck, for driving the service deck to be stretched out along landing runway direction, aids in carrier-borne aircraft safe falling.The present invention can effectively reduce the landing difficulty of carrier-borne aircraft, due to extending flight landing runway, abundant landing time has been won for pilot, has effectively avoided failure of landing caused by drop point judges to lose and known, and then the interception success rate for intercepting rope is improved, increase security.
Description
Technical field
The present invention relates to aircraft-carrier-deck facility technology field, is dropped more particularly, to a kind of aircraft carrier alighting deck and aircraft carrier
Fall deck application method.
Background technology
Aircraft carrier is aircraft carrier, is a kind of large-scale water surface naval vessels using carrier-borne aircraft as main operational weapon, alighting deck is just
It is for carrier-borne aircraft landing and the upper deck parked on aircraft carrier warship face.Carrier-borne aircraft land in mode be：Aircraft carrier barrier cable, it is used for
Carrier-borne aircraft is blocked at a high speed and stopped, is that carrier-borne aircraft is qualified " lifeline ".Can slowly slow down flat fly greatly when being landed with shore-based aircraft
Mutually very unlike, carrier-borne aircraft, which lands, must accelerate to land, once arrester wires pintle fails to tangle carrier-borne aircraft, it is necessary to and energy quick lift is answered
Fly.Generally, intercept rope and be arranged in alighting deck rear portion, share four interception ropes, the pilot of landing must allow arresting hook to hang up
Wherein one.He should hang up Article 3 (counting from back to front) under the best circumstances, if he hangs up first two, then under him
It is peaceful that angle drops, if he hangs up the last item, then and his angle downwards are too steep.When landing, pilot must be by aircraft
Force down completely, so he can ensure to hook an interception rope.Engine must be reached maximum by him simultaneously, if it is so carrier-borne
Machine can also be realized within the most short time if not hanging up interception rope and gone around, and come back to landing course line.
Land on aircraft carrier, be most difficult flight skill especially at night or in the case of bad weather
, the example for failure of landing on aircraft carrier be can be found everywhere, and casualties and huge property loss can be caused when serious.By
In intercepting rope stopped under carrier-borne aircraft fast state, considerably increase and intercept rope leakage extension, disconnected rope risk, these all make carrier-borne
Operation when machine lands is extremely difficult, turns into most dangerous, accident rate highest node on warship.Therefore, if aircraft carrier can be real
Existing sufficiently long runway declines for carrier-borne aircraft, slowed down, then can effectively improve landing security.But because aircraft carrier is by globality
With the limitation of the other conditions such as tonnage, sufficiently long runway can not be solely made.
Applicants have discovered that at least there is following technical problem in prior art：Landing runway is too short, carrier-borne aircraft landing difficulty
Larger, the carrier-borne aircraft pilot exercisable time is too short during land, landing security incident takes place frequently.
The content of the invention
It is existing to solve it is an object of the invention to provide a kind of deck for aiding in carrier-borne aircraft stable landing and its application method
There is landing runway present in technology too short, cause the technical problems such as ship-board aircraft landing difficulty is larger, security incident takes place frequently.This
Invent many technique effects elaboration as detailed below that the optimal technical scheme in many technical schemes provided can be generated.
To achieve the above object, the invention provides following technical scheme：
A kind of aircraft carrier alighting deck, including main alighting deck, airstrips are provided with main alighting deck；In main landing first
Plate is provided with telescopic service deck along airstrips direction, for extending the airstrips；The main alighting deck
Drive device is provided between the service deck, for driving the service deck to be stretched out along airstrips direction or receiving
Return.
Preferably, the service deck includes warship panel and the horizontal support bar being set in parallel in below the warship panel,
The horizontal support bar end is connected with the warship panel and stretching synchronous with the warship panel or withdrawal, the driving dress
Put and act on the horizontal support bar, the horizontal support bar is protruded horizontally up or is withdrawn；The horizontal support bar has bar
Set, it is arranged at below the main alighting deck, the horizontal support bar is placed in the rod set when withdrawing.
Preferably, in addition to telescopic first support column and telescopic second support column；First support column two
End is fixedly installed on the warship panel and horizontal support bar respectively, and the second support column both ends are fixedly installed on the warship respectively
Between panel and the rod set, first support column and the second support column synchronization action, the warship panel and water are kept
Flat support bar is parallel.
Preferably, the second support top end is provided with support wheel, and the warship panel lower surface is provided with rectilinear orbit,
The support wheel is located in the rectilinear orbit, and the support wheel turns in the rectilinear orbit when warship panel-level moves
It is dynamic.
Preferably, in addition to skewed horizontal load bar, there is oblique rod set and flexible rod end, the oblique rod set is fixed on aircraft carrier
On hull or main alighting deck, the drive end end is connected to the horizontal support bar end, when the drive end extends,
The horizontal support bar is supported upwards.
Preferably, the horizontal support bar is arranged to several, is be arranged in parallel with the airstrips, the support wheel,
The rectilinear orbit and hydraulic-driven bar setting corresponding with the quantity of the horizontal support bar and position.
Preferably, the warship panel bottom surface is provided with some row's rollers, is arranged at intervals with the rectilinear orbit；The roller
The warship panel is supported to be relatively moved with the main alighting deck.
Preferably, the warship panel lower surface is set fluted, and the roller can be folded up to the groove.
Preferably, the main alighting deck end is provided with step, when the warship panel stretches out with the main alighting deck
Overlapping at the step, the shoulder height is identical with the warship plate thickness.
The present invention also provides a kind of application method of aircraft carrier alighting deck, and the aircraft carrier alighting deck includes telescopic auxiliary
Deck is helped, application method includes the operation for controlling the service deck to rise vertically and the behaviour for moving horizontally the service deck
Make.
Aircraft carrier alighting deck provided by the invention, service deck, Ke Yishi are installed along in runway heading in main alighting deck
When stretch out, to extend airstrips；Or withdraw, it is overlapping with main alighting deck, main alighting deck is not influenceed to be used.Carrier-borne aircraft
Before landing, service deck is released using drive device, slowly declines to service deck during main alighting deck edge, makes its upper table
Face and main alighting deck upper surface in the same plane, to keep the flatness of airstrips and continuity.When carrier-borne aircraft lands,
Landing attempt is carried out by standard of main alighting deck runway, if can not accurately drop on main alighting deck, can also be dropped in advance
On service deck, landing is avoided unsuccessfully to fall into sea；Can also be using service deck runway as standard landing attempt, equivalent to extending master
Alighting deck runway, it can be ensured that carrier-borne aircraft pintle reach intercept rope position when more accurately hook arrester wires, make carrier-borne aircraft into
Work(lands, and farthest avoids injures and deaths；When landing without carrier-borne aircraft, service deck is withdrawn to main alighting deck direction, with main drop
Fall that deck is overlapping, service deck plane now can equally play the function of covered portionss main deck, not influence main landing
The normal use on deck.
The present invention can effectively lower the landing difficulty of carrier-borne aircraft, due to extending airstrips, can greatly reduce by
Landing failure caused by judging to lose and know in drop point, can also increase the interception success rate for intercepting rope, increase security.
Brief description of the drawings
In order to illustrate more clearly about the embodiment of the present invention or technical scheme of the prior art, below will be to embodiment or existing
There is the required accompanying drawing used in technology description to be briefly described, it should be apparent that, drawings in the following description are only this
Some embodiments of invention, for those of ordinary skill in the art, on the premise of not paying creative work, can be with
Other accompanying drawings are obtained according to these accompanying drawings.
Fig. 1 is the top view of aircraft carrier involved in the present invention；
Fig. 2 is state when service deck of the present invention stretches out；
Fig. 3 is state when service deck of the present invention prepares to withdraw；
Fig. 4 is state when service deck of the present invention is withdrawn；
Fig. 5 is warship panel bottom surface structure schematic diagram of the present invention.
1 in figure, main alighting deck；11st, step；2nd, rope is intercepted；3rd, airstrips；4th, service deck；41st, warship panel；
411st, rectilinear orbit；42nd, horizontal support bar；421st, horizontal rod set；43rd, the first support column；44th, the second support column；441st, support
Wheel；45th, skewed horizontal load bar；451st, oblique rod set；452nd, expansion link；46th, roller；5th, aircraft carrier hull.
Embodiment
To make the object, technical solutions and advantages of the present invention clearer, technical scheme will be carried out below
Detailed description.Obviously, described embodiment is only part of the embodiment of the present invention, rather than whole embodiments.Base
Embodiment in the present invention, those of ordinary skill in the art are not making creativeness in the description of the invention, it is necessary to say
It is bright, the orientation or position relationship of the instruction such as term " on ", " under ", "left", "right", " vertical ", " level ", " interior ", " outer "
Based on orientation shown in the drawings or position relationship, to be for only for ease of the description present invention and simplifying description, rather than instruction or
Imply that signified device or element there must be specific orientation, with specific azimuth configuration and operation, therefore it is not intended that
Limitation of the present invention.In addition, term " first ", " second " are only used for describing purpose, and it is not intended that instruction or hint phase
To importance.
In the description of the invention, it is necessary to illustrate, unless otherwise clearly defined and limited, term " installation ", " phase
Even ", " connection " should be interpreted broadly, for example, it may be being fixedly connected or being detachably connected, or be integrally connected；Can
To be mechanical connection or electrical connection；Can be joined directly together, can also be indirectly connected by intermediary, Ke Yishi
The connection of two element internals.For the ordinary skill in the art, with concrete condition above-mentioned term can be understood at this
Concrete meaning in invention.
The invention provides a kind of aircraft carrier alighting deck, as shown in figure 1, including main alighting deck 1, set on main alighting deck
It is equipped with and intercepts rope 2 and airstrips 3；When carrier-borne aircraft lands from main alighting deck 1 above as far as possible low height close to main landing first
Intercepted rope 2 stops when plate 1 intercepts rope 2, until stopping.The present invention sets the auxiliary that can be extended at the main rear portion of alighting deck 1
Deck 4, drive device is provided between the main alighting deck 1 or aircraft carrier hull 5 and service deck 4, enables service deck 4
It is enough to extend or shorten along the direction of airstrips 3, main alighting deck 1 is lengthened, for aiding in carrier-borne aircraft safe falling.
Fig. 2 is state when service deck of the present invention stretches out, and Fig. 3 is that service deck of the present invention prepares to receive
State when returning, Fig. 4 are states when service deck of the present invention is withdrawn, lower Fig. 2-4 pairs of present invention boats of mask body combination
Female alighting deck is described in detail.
Service deck 4 includes warship panel 41 and horizontal support bar 42, the width of warship panel 41 and the main width phase of alighting deck 1
Together, upper surface is maintained at the same horizontal plane with the main upper surface of alighting deck 1 when warship panel 41 stretches out, so that airstrips are kept
Good planarization and persistent.Specifically, the main tail end of alighting deck 1 is provided with the step for coordinating with warship panel 41
11, its front end is located exactly in step 11 after making the stretching of warship panel 41, warship panel 41 and main alighting deck 1 is had certain weight
Folded, the height of step 11 is identical with the thickness of warship panel 41, to keep warship panel 41 with the main upper surface of alighting deck 1 in same level
On.The choice of material of warship panel 41 and the similar material of main alighting deck 1, but can be slightly lighter than main alighting deck 1, with full
The flexibility that foot stretches out and withdrawn.Warship panel 41 is overlapping with main alighting deck 1 in a non-operative state, such as is recovered to main landing
The bottom of deck 1, the inside of aircraft carrier hull 5 are placed in the main top of alighting deck 1, and warship panel 41 is designed according to being actually needed
Placement location.
In order to keep stabilization when warship panel 41 stretches out, horizontal support bar 42 is provided with below warship panel 41.Level branch
Strut 42 is identical with the length of warship panel 41, synchronous with warship panel 41 can stretch out, synchronous to withdraw, and keeps warship panel 41 in vertical side
Upward firmness degree, while help warship panel 41 to resist issuable impulsive force when carrier-borne aircraft landing fails.Specifically, water
Flat support bar 42 is fixedly connected with the end of warship panel 41, and horizontal support bar 42, which is provided with, is fixed on the main lower section of alighting deck 1, hull
Horizontal rod set 421 inside 5.In being provided with the drive device for driving horizontal support bar 42 on aircraft carrier hull, water can be made
Flat support bar 42 stretches out or withdrawn.When horizontal support bar 42 is withdrawn, it is retracted into horizontal rod set 421, on the one hand makes horizontal branch
Strut 42 is smoothly withdrawn, and on the other hand can play a part of support level support bar 42.
The first support column 43 and the second support column 44 are provided between horizontal support bar 42 and warship panel 41.Wherein first
Dagger 43 is vertically installed in warship panel 41 and the end of horizontal support bar 42, and the first support column 43 is arranged to Collapsible structure, both ends
The lower surface of warship panel 41 and the upper surface of horizontal support bar 42 are individually fixed in, the first support column 43 can be by warship panel by elongation
41 jack up；Second support column 44 is arranged between horizontal rod set 421 and warship panel 41, and the second support column 44 is arranged to scalable knot
Structure, the second support column 44 and the first support column 43 keep synchronous, can make between warship panel 41 and horizontal support bar 42
Vertical distance increases or reduced.
Wherein, the lower end of the second support column 44 is fixed in horizontal rod set 421, and upper end is provided with support wheel 441, the support
Wheel 441 is supported in the lower surface of warship panel 41, is particularly located in the rectilinear orbit 411 of the lower surface of warship panel 41 setting, when warship face
Plate 41 to main alighting deck 1 bounce back when, support wheel 441 supports and promotes warship panel 41 to be moved to main alighting deck 1, to reduce
Friction between two support columns 44 and warship panel 41.Wherein support wheel 441 is it can also be provided that active drive wheel.Under warship panel 41
Surface is provided with some rectilinear orbits 411, corresponding with the position of support wheel 441, and rectilinear orbit 411 withdraws luck with warship panel 41
Dynamic direction is identical, the friction between guiding and reduction warship panel 41 and the second support column 44 when being withdrawn for warship panel 41.
The lower section of service deck 4 is provided with skewed horizontal load bar 45, for supporting service deck 4.Specifically, skewed horizontal load bar 45
Be arranged to Collapsible structure, can extend and shorten in its axial direction, could be arranged to such as hydraulic drive mechanism or
Air pressure drive mechanism, it has oblique rod set 451 and expansion link 452, wherein oblique rod set 451 be fixed on aircraft carrier hull 5 or
On main alighting deck 1, the end of horizontal support bar 42 is fixed in the end of expansion link 452, can be set at oblique rod set 451 oblique
Drive device, when making horizontal support bar 42 and the synchronization elongation of skewed horizontal load bar 45, warship panel 41 is promoted to the main rear portion of alighting deck 1
Stretch out, while the upward support level support bar 42 of skewed horizontal load bar 45 and warship panel 41；When horizontal extension bar 42 and skewed horizontal load
When bar 45 is synchronously withdrawn, warship panel 41 is promoted to be withdrawn to the main direction of alighting deck 1.
In addition, Fig. 5 is warship panel bottom surface structure schematic diagram of the present invention.The bottom of warship panel 41 is additionally provided with roller
46, the roller 46 is during warship panel 41 is retracted on main alighting deck 1, and support warship panel 41 is in main alighting deck 1
Friction of the upper slip to reduce between warship panel 41 and main alighting deck 1, makes warship panel 41 smoothly withdraw.If roller 46 can be
Dry be arranged in parallel, as Fig. 5 is arranged to three rows, be arranged in parallel and is arranged at intervals with rectilinear orbit 411.
Warship panel 41 can set 30-50 rice along airstrips direction length in the present invention, can effectively alleviate carrier-borne aircraft
Because landing failure caused by landing place is inaccurate during landing.It is also possible in the front portion of main alighting deck and afterbody difference
The service deck is set, makes the flexible utilization of aircraft carrier alighting deck of the present invention.
The aircraft carrier alighting deck working method of the present invention is as follows：
When needing landing without carrier-borne aircraft, warship panel 41 is located at initial position, and main 1 overlapping placement of alighting deck, not shadow
The normal use of main alighting deck 1 is rung, warship panel 41 is placed on main alighting deck, and horizontal support bar 42 is located at horizontal rod set
In 421.
When carrier-borne aircraft needs landing, wherein the first support column 43 works with the second support column 44 simultaneously, make warship panel 41
It is raised above in a manner of parallel to main alighting deck 1, then roller 46 is fallen, and warship panel 41 is supported in into main alighting deck 1
On；Warship panel 41 is risen to after predetermined altitude, and horizontal support bar 42 stretches out out of horizontal rod set 421, while skewed horizontal load bar
452 stretch out out of oblique rod set 451, because the end of horizontal support bar 42 is connected with warship panel 41 by the first support column 43, warship
Panel 41 also stretches out backward therewith, the support wheel 441 on the second support column 44 in the rectilinear orbit 411 of the bottom surface of warship panel 41,
Reduce friction when warship panel 41 stretches out；After warship panel 41 reaches precalculated position, the income of roller 46 arrives the bottom of warship panel 41
Portion, while the first support column 43 and the second support column 44 start slowly to shorten, and make warship panel 41 parallel under horizontal support bar 42
Drop, until engaging the edge of warship panel 41 and the step 11 at the main rear portion of alighting deck 1.Skewed horizontal load bar 45 is locked to prop up upwards
Support warship panel 41.After completing above step, all movable mechanisms all lock in service deck, wait carrier-borne aircraft landing.
After carrier-borne aircraft completes landing, first by the latch-release of movable mechanism.First support column 43 and second
Dagger 44 is synchronous to be stretched out upwards, warship panel 41 is increased, and to predetermined altitude, roller 46 stretches out from the bottom surface of warship panel 41, simultaneously
Horizontal support bar 42 and skewed horizontal load bar 45 are retracted into horizontal rod set 421 and oblique rod set 451 respectively, so as to drive warship panel
41 move to the main direction of alighting deck 1.When roller 46 is located at main 1 top of alighting deck, the first support column 43 and the second support
The synchronous appropriate retraction of post 44, makes warship panel 41 be continued to move under the support of roller 46, until warship panel 41 returns to initial position.
In such scheme, the first support column 43 and the second support column 44 can use same drive device, for example, air pressure or
Person's hydraulic drive source, or the first support column 43 and the second support column 44 can also be with skewed horizontal load bars 45 and horizontal support bar 42
Using same air pressure or hydraulic drive source, the original power source for intercepting rope of aircraft carrier is utilized.
The foregoing is only a specific embodiment of the invention, but protection scope of the present invention is not limited thereto, any
Those familiar with the art the invention discloses technical scope in, change or replacement can be readily occurred in, should all be contained
Cover within protection scope of the present invention.Therefore, protection scope of the present invention should be based on the protection scope of the described claims.
Claims (10)
1. a kind of aircraft carrier alighting deck, it is characterised in that including main alighting deck (1), flight is provided with main alighting deck (1)
Runway (3)；Telescopic service deck (4) is provided with along airstrips (3) direction in main alighting deck, it is described for extending
Airstrips (3)；Drive device is provided between the main alighting deck (1) and the service deck (4), it is described for driving
Service deck (4) stretches out or withdrawn along airstrips (5) direction.
2. aircraft carrier alighting deck according to claim 1, it is characterised in that the service deck (4) includes warship panel
And the horizontal support bar (42) that is set in parallel in below the warship panel, horizontal support bar (42) end and the warship (41)
Panel (41) connects and stretching synchronous with the warship panel (41) or withdrawal, and the drive device acts on the horizontal branch
Strut (42), the horizontal support bar (42) is set to protrude horizontally up or withdraw；The horizontal support bar (42) has rod set
(421), it is arranged at below the main alighting deck (1), the horizontal support bar (42) is placed in the rod set (421) when withdrawing
It is interior.
3. aircraft carrier alighting deck according to claim 2, it is characterised in that also including telescopic first support column (43)
With telescopic second support column (44)；First support column (43) both ends be fixedly installed on respectively the warship panel (41) and
Horizontal support bar (42), the second support column (44) both ends are fixedly installed on the warship panel (41) and the rod set respectively
(421) between, first support column (43) and second support column (44) synchronization action, keep the warship panel (41) and
Horizontal support bar (42) is parallel.
4. aircraft carrier alighting deck according to claim 3, it is characterised in that the second support column (44) top is provided with
Support wheel (441), warship panel (41) lower surface are provided with rectilinear orbit (411), and the support wheel (441) is positioned at described straight
In trajectory (411), the warship panel (41) when moving horizontally the support wheel (441) turn in the rectilinear orbit (411)
It is dynamic.
5. aircraft carrier alighting deck according to claim 4, it is characterised in that also including skewed horizontal load bar (45), have oblique
To rod set (451) and flexible rod end (452), the oblique rod set (451) is fixed on aircraft carrier hull (5) or main alighting deck
(1) on, drive end (452) end is connected to the horizontal support bar (42) end, when the drive end (452) extends,
The horizontal support bar (42) is supported upwards.
6. aircraft carrier alighting deck according to claim 5, it is characterised in that the horizontal support bar (42) is arranged to some
It is individual, it is be arranged in parallel with the airstrips (3), the support wheel (441), the rectilinear orbit (411) and the hydraulic-driven
Bar (45) setting corresponding with the quantity of the horizontal support bar (42) and position.
7. aircraft carrier alighting deck according to claim 4, it is characterised in that warship panel (41) bottom surface is provided with some
Roller (46) is arranged, is arranged at intervals with the rectilinear orbit (411)；The roller (46) supports the warship panel (41) and the master
Alighting deck (1) relatively moves.
8. aircraft carrier alighting deck according to claim 7, it is characterised in that warship panel (41) lower surface is provided with recessed
Groove, the roller (46) can be folded up to the groove.
9. aircraft carrier alighting deck according to claim 2, it is characterised in that main alighting deck (1) end is provided with
Step (11), when the warship panel (41) is stretched out with the main alighting deck (1) at the step (11) place overlapping, the step
(11) it is highly identical with warship panel (41) thickness.
10. a kind of aircraft carrier alighting deck application method, the aircraft carrier alighting deck includes telescopic service deck, and its feature exists
In application method includes the operation for controlling the service deck to rise vertically and the operation for moving horizontally the service deck.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710684142.8A CN107472549A (en) | 2017-08-09 | 2017-08-09 | A kind of aircraft carrier alighting deck and its application method |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710684142.8A CN107472549A (en) | 2017-08-09 | 2017-08-09 | A kind of aircraft carrier alighting deck and its application method |
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| Publication Number | Publication Date |
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| CN107472549A true CN107472549A (en) | 2017-12-15 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201710684142.8A Pending CN107472549A (en) | 2017-08-09 | 2017-08-09 | A kind of aircraft carrier alighting deck and its application method |
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Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108408072A (en) * | 2018-05-08 | 2018-08-17 | 西北工业大学 | A kind of carrier-borne recovery method of fixed-wing UAV and system |
| CN108945286A (en) * | 2018-07-04 | 2018-12-07 | 中国船舶工业集团公司第七0八研究所 | Active extendible helicopter platform device |
| CN111470015A (en) * | 2020-05-19 | 2020-07-31 | 济南环太机电技术有限公司 | Lifting deck type aircraft carrier |
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| CN102548838A (en) * | 2009-07-28 | 2012-07-04 | Tts海运公司 | variable length boat ramp |
| CN103043220A (en) * | 2011-10-13 | 2013-04-17 | 王力丰 | Taking-off and landing system of shipboard aircraft of aircraft carrier and taking-off and landing method thereof |
| CN104002980A (en) * | 2013-02-21 | 2014-08-27 | 上海市南洋模范中学 | Carrier-based aircraft landing assist device |
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| CN108408072A (en) * | 2018-05-08 | 2018-08-17 | 西北工业大学 | A kind of carrier-borne recovery method of fixed-wing UAV and system |
| CN108408072B (en) * | 2018-05-08 | 2021-08-06 | 西北工业大学 | Method and system for shipboard recovery of fixed-wing unmanned aircraft |
| CN108945286A (en) * | 2018-07-04 | 2018-12-07 | 中国船舶工业集团公司第七0八研究所 | Active extendible helicopter platform device |
| CN111470015A (en) * | 2020-05-19 | 2020-07-31 | 济南环太机电技术有限公司 | Lifting deck type aircraft carrier |
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