CN103057717A - Modular deck with power rods - Google Patents
Modular deck with power rods Download PDFInfo
- Publication number
- CN103057717A CN103057717A CN2013100165298A CN201310016529A CN103057717A CN 103057717 A CN103057717 A CN 103057717A CN 2013100165298 A CN2013100165298 A CN 2013100165298A CN 201310016529 A CN201310016529 A CN 201310016529A CN 103057717 A CN103057717 A CN 103057717A
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- CN
- China
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- aircraft carrier
- power
- deck
- modular deck
- power rod
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- 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.)
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Abstract
The invention relates to a modular deck with power rods. The modular deck is used for take-off and landing of an aircraft carrier. The technical scheme includes that a plurality of steel power rods are parallelly fixed to form a square or rectangular modular deck body with the power rods; two modular deck zones with the power rods are formed on an inevitable track of take-off and landing rear load-bearing wheels of the aircraft carrier placed on the deck of the aircraft carrier, the power rods are driven by a motor to synchronously and constantly rotate towards a bow, and accordingly the modular deck zones with kinetic power are formed; when the aircraft carrier lands on the bow, set-forward power of the aircraft carrier can be reduced to zero and the aircraft carrier can be decelerated and stop at the moment when the two rear load-bearing wheels of the aircraft carrier are in contact with the modular deck with the power rods; and reversely, when the aircraft carrier takes off via the modular deck with the power rods, the aircraft carrier can be boosted by multiplied-speed ahead power at the moment when constant power in the horizontal rotation direction of the modular deck with the power rods is transmitted to the two rear load-bearing wheels of the aircraft carrier, the exit take-off set-forward speed of the aircraft carrier is greatly increased, take-off force is increased, and take-off action is completed.
Description
Technical field
The invention belongs to the engine installation category, relate to a kind of aircraft carrier landing power rod modular deck.
Background technology
Aircraft carrier warship deck, the world is the single load-bearing character of fixed type integral structure deck at present, has the poor problem of function and benefit.
Summary of the invention
The invention reside in the aircraft carrier warship deck function singleness problem that solves.A kind of power rod modular deck is provided, replaces aircraft carrier landing partial deck.
Technical scheme is, at motor drives power rod modular deck, in the rotation of bow direction level constant, when carrier-borne aircraft warship at bow, two load-bearing trailing wheels of body impulse force arrives on the power rod modular deck, can make the carrier landing forward momentum naturally be consumed to no-pull in touch panel moment and stop.Thereby, reduced carrier landing deck consumption length.Remove the check cable accessory device from.Can guarantee very warship rate safe effect.
Otherwise, when aircraft carrier from the warship lift-off of taking off, travel through power rod modular deck, during two consequence roller touch panels to the aircraft carrier bow, can receive the speed ahead power boosting kinetic energy that power rod modular deck sends to moment, accelerate carrier-borne aircraft from the warship dynamics of going up to the air.
Thus, this power rod modular deck is applied on the aircraft carrier, has namely solved the single weight-bearing function in aircraft carrier deck problem of poor benefits.The accessory devices such as check cable have been reduced again.And can warship landing ability and safety by the Effective Raise aircraft carrier.Simultaneously, also having broken through aircraft carrier landing deck can only be whole, smooth fixed construction designing technique theory.
Description of drawings
Fig. 1 is combined into the power rod sterogram that modular deck is used.Among the figure, the 1st, ditch shape pulley groove power club head entity part; The 2nd, power rod entity; The 3rd, be enclosed within on the power rod circumferential body tire lines rubber bush entity.
Fig. 2 is power rod entity section-drawing.Among the figure, the 2nd, steel power rod entity section; The 3rd, being enclosed within has gear shape hollow on the power rod circumferential body, tire lines rubber tube entity section.
The specific embodiment
Make one with circular steel, caput has ditch shape pulley groove, and barred body holds round tooth colyliform power rod entity.Compressing rubber, in the hollow entity tire lines rubber tube of gear-like is arranged, sectional gland on power rod entity, the power of the structure that is combined into one rod entity.
Power rod entity using one by one is neck and neck on the horizontal surface, is fixed into box-shaped or oblong power rod modular deck entity.Power rod modular deck place be fixed on aircraft carrier deck carrier-borne aircraft landing center of gravity two load-bearing trailing wheels must through circuit on, just formed in the whole fixed type of aircraft carrier deck, be embedded into two power rod modular deck bands.Make its with the periphery the smooth plane that is integrated, fixed type deck.At each root power rod of motor drives, rotate to bow direction constant synchronization, just realized in the whole deck of aircraft carrier fixed type, increased the power rod modular deck that kinetic energy is arranged.Such power type deck band has been arranged, when carrier-borne aircraft warship from bow, owing to the reverse kinetic energy that power rod modular deck rotates, acting on two consequence rollers of carrier-borne aircraft of warship, but moment has made carrier-borne aircraft preshoot dynamic retarding stop to zero.
Otherwise, when aircraft carrier goes up to the air through power rod modular deck, horizontally rotate the invariable kinetic energy effect of force direction at power rod modular deck, conduction is to two load-bearing trailing wheels of carrier-borne aircraft, moment can make aircraft carrier obtain a times speed ahead power boosting, thereby, increase substantially carrier-borne aircraft from the preshoot speed of warship lift-off, finish lift-off action purpose.
Because thing power rod modular deck of the present invention has only increased by two power rod modular deck bands on the aircraft carrier deck, just solved the poor problem of single bearing function and benefit on the whole deck of aircraft carrier fixed type.
Simultaneously, also having broken through aircraft carrier landing deck, can only be the designing technique theory of fixedly monolithic devices.
Claims (1)
1. power rod modular deck, it includes steel power rod ditch shape pulley groove caput entity (1), power rod entity (2) and overlaps the tire lines rubber bush entity (3) that is pressed on the power rod circumferential body, the power rod entity of the structure that is combined into one, it is characterized in that, with many power rod entities, parallel box-shaped or the oblong power rod modular deck entity that is fixed into side by side is as the special-purpose deck of aircraft carrier landing.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2013100165298A CN103057717A (en) | 2013-01-17 | 2013-01-17 | Modular deck with power rods |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2013100165298A CN103057717A (en) | 2013-01-17 | 2013-01-17 | Modular deck with power rods |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN103057717A true CN103057717A (en) | 2013-04-24 |
Family
ID=48100676
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2013100165298A Pending CN103057717A (en) | 2013-01-17 | 2013-01-17 | Modular deck with power rods |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN103057717A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103587711A (en) * | 2013-04-28 | 2014-02-19 | 叶元华 | Arresting device and runway being provided with arresting device |
| CN110284444A (en) * | 2019-07-05 | 2019-09-27 | 叶锦华 | A kind of safety collision-protection device on highway bridge |
Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4786014A (en) * | 1985-11-04 | 1988-11-22 | Indal Technologies Inc. | Helicopter rapid securing & traversing system |
| CN1927659A (en) * | 2005-09-11 | 2007-03-14 | 李江华 | Method and facility of zero movement accelerating short-slippage take-off and landing |
| CN101107183A (en) * | 2005-01-11 | 2008-01-16 | 马丁·韦斯特高 | Conveyor guard |
-
2013
- 2013-01-17 CN CN2013100165298A patent/CN103057717A/en active Pending
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4786014A (en) * | 1985-11-04 | 1988-11-22 | Indal Technologies Inc. | Helicopter rapid securing & traversing system |
| CN101107183A (en) * | 2005-01-11 | 2008-01-16 | 马丁·韦斯特高 | Conveyor guard |
| CN1927659A (en) * | 2005-09-11 | 2007-03-14 | 李江华 | Method and facility of zero movement accelerating short-slippage take-off and landing |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103587711A (en) * | 2013-04-28 | 2014-02-19 | 叶元华 | Arresting device and runway being provided with arresting device |
| CN110284444A (en) * | 2019-07-05 | 2019-09-27 | 叶锦华 | A kind of safety collision-protection device on highway bridge |
| CN110284444B (en) * | 2019-07-05 | 2021-08-24 | 江苏金鼎建设集团有限公司 | Safety anti-collision device on highway bridge |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WD01 | Invention patent application deemed withdrawn after publication | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20130424 |