CN102765468A - Novel design scheme for aircraft carrier runways - Google Patents
Novel design scheme for aircraft carrier runways Download PDFInfo
- Publication number
- CN102765468A CN102765468A CN2012102341001A CN201210234100A CN102765468A CN 102765468 A CN102765468 A CN 102765468A CN 2012102341001 A CN2012102341001 A CN 2012102341001A CN 201210234100 A CN201210234100 A CN 201210234100A CN 102765468 A CN102765468 A CN 102765468A
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- runway
- aircraft
- aircraft carrier
- carrier
- slope type
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Abstract
The invention provides a novel design scheme for aircraft carrier runways, and relates a design scheme for all-weather aircraft carriers, which is energy-saving, safe and environment-friendly and shortens the lengths of taking-off and landing runways. A runway on the deck of an aircraft carrier is designed to be a slope type runway. when an aircraft lands, the aircraft climbs up along the slope type runway E; after arriving the top end, the aircraft is landed on the ground by a lifter C; and during the landing, power is generated by a power generation system arranged in the lifter C and is fed back to a battery in the aircraft carrier. A hyperbolic notch G is formed in the beginning end of the slope type runway E of the aircraft carrier, so that when the tail of the aircraft B lands on the runway, a draw hook stretching downwards hooks the notch easily rather than fails to hook the pull rope of a damping piece. When the slope type runway E is paved, a plurality of bar reinforcements are pre-buried side by side at certain width intervals along the trend of the runway in advance, so that the bar reinforcements can be applied with a certain voltage to generate heat in virtue of iron resistance to melt snow flakes falling from the sky, and all melted snow water can be discharged downwards along the slope type runway E.
Description
Technical field
The new design plan of patent aircraft carrier runway of the present invention, the battleship that relates to a kind of military field is technological.
Background technology
Since over half a century; The military design engineers of developed country; On the problem of development aircraft carrier runway, pace up and down and when a carrier-borne aviator is maked a return voyage, the safety problem of warship, come but fail to find out an economy, safety and rational solution all the time; Causing the failure that causes repeatedly, is that large quantities of carrier-borne aviators die young because of warship defeats and get what come in return.
Summary of the invention
The new design plan of patent aircraft carrier runway of the present invention is to be a kind of new departure that main objective is taked with improving safety factor, and it not only can make the carrier-borne aircraft B on the deck of flying back can safe falling, guarantees no longer to take place any accident; Can also shorten the length of runway when taking off, be that carrier-borne aircraft warship safety and the undying nightmare that adds long runway to finish aircraft carrier.Particularly estimable is, the runway that after this new departure was implemented, the runway of aircraft carrier just can become " round-the-clock ", fall, be " killing three birds with one stone ".
Its concrete way is:
1, avoid carrier-borne aircraft B when landing; The drag hook of its afterbody is not hung the steel wire rope of sandbag damping piece; Can be with the initial landing point place on deck, open a hyp big gap G; So that pintle can be stretched lower deck, this just can guarantee that drag hook can " not brush past " with the steel wire rope of sandbag damping piece again.Again runway E is built into sloping type runway, after carrier-borne aircraft B drops on the deck, will make its kinetic energy that carries, change into a part of potential energy at once and lower its speed rapidly along sloping type runway E upwards " spurt is slided "; Also allow the aviator to step on " machine of stopping " at this moment simultaneously and brake, its speed is further lowered rapidly.Step on " machine of stopping " owing to allow chaufeur; So can in wheel, install the motor of a cover " electric-generating "; In order to when stepping on " machine of stopping " at chaufeur; Utilize the kinetic energy of aircraft B and generate electricity, produce electric energy and feed back to again in the battery in the carrier-borne aircraft B, make the energy recycle to reach.(concrete grammar is referring to " round-the-clock environmental protection airport " patent, and the patent No. is: 201210042637.8)
2, owing to built sloping type runway E above deck, just can utilize this ramp to be used as takeoff runway, when carrier-borne aircraft B takes off; Because be in a high position; After the starting, utilize potential energy, can quicken the takeoff speed of aircraft; Power up, drive wheel for simultaneously the motor in the wheel, carrier-borne aircraft B just can go up to the air in limited distance again.For the carrier-borne aircraft B that is more convenient for immediately goes up to the air, the initiating terminal of runway can be designed to " type warps ".
3, companion ladder C also is designed to power generation type, utilizes the potential energy after the carrier-borne aircraft B that returns warship climbs, and generates electricity during decline, feeds back in the battery on the warship.
4, when building sloping type runway E, in advance along the trend of runway, side by side, certain width ground, pre-buried several reinforcing bars at interval; When running into snowy day, leading to certain voltage on the reinforcing bar, utilize the iron resistance heating effect of reinforcing bar; To melt the snowflake that fall the sky; This part snowflake will be with falling with changing into water, and it can let out light downwards along the ramp of runway, and is unlikely to ponding.
5, when carrier-borne aircraft B takes off, trailing wheel is absorbed in the G groove of aircraft carrier runway E initiating terminal, cause the unbalance for the moment and mis-use breakdown of carrier-borne aircraft B; Can be under the G on deck groove; Pre-install two movable pad H; When carrier-borne aircraft B took off, these two movable pad H drew in, and deck " pad " put down and unlikely generation accident.
Description of drawings
Fig. 1: the lateral plan that is aircraft carrier.
A---guardrail
B---carrier-borne aircraft
C---companion ladder
D---direct tower
E---sloping type runway
F---warship body
Fig. 2: the birds-eye view that is aircraft carrier.
G---gap
Fig. 3: be the scheme drawing that increases movable pad
H---two movable pads
The specific embodiment
When 1, making aircraft carrier,, open the gap G of a hyperbola at the initiating terminal of runway; In order to the tail of carrier-borne aircraft B when " warship "; The drag hook of stretching down is " recognizing groove " easily, and be unlikely to miss the steel wire rope that hangs up the damping rope, (the steel wire rope of damping piece this moment; Should paste the deck fully and put, and the aircraft that need not to be suspended in midair again, to take off with obstruction free flies away from the deck)
2, in the high-end end of sloping type runway E, solid, elastic protecting wire net A must be installed one again, break through runway and crash into marine to prevent contingency carrier-borne aircraft B.
3, when laying sloping type runway E, in advance along the trend of runway, side by side, pre-buried several reinforcing bars in certain width ground at interval; When running into snowy day, leading to certain voltage on the reinforcing bar, utilize the iron resistance heating of reinforcing bar; To melt the snowflake that fall the sky; This part snowflake will be with falling with changing into water, and it can let out light downwards along the ramp of runway, is unlikely to ponding.
Claims (4)
1. the new design plan of patent aircraft carrier runway of the present invention, the aircraft carrier runway that it is characterized in that having a plurality of advantages such as energy-conservation, safe and reliable, environmental protection and shortening landing airdrome length.
2. according to claim 1, the runway on the aircraft carrier deck is designed to the ramp pattern.
3. according to claim 1, at aircraft carrier runway initiating terminal, open a hyperbola gap G.
4. according to claim 1, when laying sloping type runway, in advance along the trend of runway, side by side, pre-buried several reinforcing bars equal in certain width ground at interval with the runway face.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2012102341001A CN102765468A (en) | 2012-06-29 | 2012-06-29 | Novel design scheme for aircraft carrier runways |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2012102341001A CN102765468A (en) | 2012-06-29 | 2012-06-29 | Novel design scheme for aircraft carrier runways |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN102765468A true CN102765468A (en) | 2012-11-07 |
Family
ID=47093100
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2012102341001A Pending CN102765468A (en) | 2012-06-29 | 2012-06-29 | Novel design scheme for aircraft carrier runways |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN102765468A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103863537A (en) * | 2012-12-12 | 2014-06-18 | 芦正安 | Aircraft carrier hull with double-deck flight deck |
| CN105752303A (en) * | 2015-12-29 | 2016-07-13 | 深圳前海联合邮轮有限公司 | Method for assisting short takeoff of fixed wing aircraft and ship form |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4209768A (en) * | 1974-10-22 | 1980-06-24 | Basov Nikolai G | Aircraft take-off and landing system and method for using same |
| US5218921A (en) * | 1989-02-13 | 1993-06-15 | Anthony Malcolm | Aircraft carrier |
| CN1804220A (en) * | 2005-11-03 | 2006-07-19 | 王敏华 | Slope-shaped airplane runway covering small area and use method thereof |
| CN2816127Y (en) * | 2004-12-26 | 2006-09-13 | 朱炎炎 | Fully-automatic ice-snow removing system |
| CN1955071A (en) * | 2005-10-30 | 2007-05-02 | 梁嘉麟 | Slope aircraft landing taxi-track on aircraft-carrier deck and its using method |
| CN101513936A (en) * | 2009-03-31 | 2009-08-26 | 王力丰 | Taking off device and taking off method for carrier-based aircraft |
| CN102358432A (en) * | 2011-09-07 | 2012-02-22 | 刘建平 | Assisted takeoff system of airplane |
-
2012
- 2012-06-29 CN CN2012102341001A patent/CN102765468A/en active Pending
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4209768A (en) * | 1974-10-22 | 1980-06-24 | Basov Nikolai G | Aircraft take-off and landing system and method for using same |
| US5218921A (en) * | 1989-02-13 | 1993-06-15 | Anthony Malcolm | Aircraft carrier |
| CN2816127Y (en) * | 2004-12-26 | 2006-09-13 | 朱炎炎 | Fully-automatic ice-snow removing system |
| CN1955071A (en) * | 2005-10-30 | 2007-05-02 | 梁嘉麟 | Slope aircraft landing taxi-track on aircraft-carrier deck and its using method |
| CN1804220A (en) * | 2005-11-03 | 2006-07-19 | 王敏华 | Slope-shaped airplane runway covering small area and use method thereof |
| CN101513936A (en) * | 2009-03-31 | 2009-08-26 | 王力丰 | Taking off device and taking off method for carrier-based aircraft |
| CN102358432A (en) * | 2011-09-07 | 2012-02-22 | 刘建平 | Assisted takeoff system of airplane |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103863537A (en) * | 2012-12-12 | 2014-06-18 | 芦正安 | Aircraft carrier hull with double-deck flight deck |
| CN105752303A (en) * | 2015-12-29 | 2016-07-13 | 深圳前海联合邮轮有限公司 | Method for assisting short takeoff of fixed wing aircraft and ship form |
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|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C02 | Deemed withdrawal of patent application after publication (patent law 2001) | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20121107 |