CN103224030A - Support pillar for double-layered deck of aircraft carrier - Google Patents
Support pillar for double-layered deck of aircraft carrier Download PDFInfo
- Publication number
- CN103224030A CN103224030A CN2013101458826A CN201310145882A CN103224030A CN 103224030 A CN103224030 A CN 103224030A CN 2013101458826 A CN2013101458826 A CN 2013101458826A CN 201310145882 A CN201310145882 A CN 201310145882A CN 103224030 A CN103224030 A CN 103224030A
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- deck
- pillar stiffener
- double
- aircraft carrier
- support pillar
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Abstract
The invention discloses a support pillar for a double-layered deck of an aircraft carrier. The support pillar comprises support pillars, wherein the support pillars are hollow cylindrical, are made of metal, are connected to an upper layer deck and a lower layer deck, and are erectly arranged on two sides of a runway of the lower layer deck and on the outer side edge of the lower layer deck. The support pillar for the double-layered deck of the aircraft carrier is simple in structure, can not affect the use of the lower layer runway and not waste the valuable space of the lower layer deck during use, and is suitable for all aircraft carriers.
Description
Technical field the present invention relates to a kind of pillar stiffener, the double-decked pillar stiffener that especially uses on aircraft carrier.
Background technology and airfield are compared, and the airstrip length on the aircraft carrier shortens greatly.Flight deck on the aircraft carrier will be born the functions such as taking off, land, deposit of carrier-borne aircraft.Chinese patent CN201437404U number disclosed " aircraft carrier of double-deck flight deck notion " patent (application number: 200920149309.1); be on the former flight deck of aircraft carrier; add a cover second layer flight deck; and then the design of the double-deck flight deck of formation tool; the separately operation on the deck of different layers of landing of taking off of aircraft; the landing of taking off can not interfere with each other; task simple many also safety many; and can make aircraft carrier increase nearly 2 times operational space and capacity increasing a little fabrication cost; and on flight deck; be provided with the runway shock absorber; needed runway slides length and slows down the speed that aircraft dashes row when being used for reducing aircraft landing; can increase the easness on safety and the personnel operation; simultaneously in former flight deck and second layer flight deck one side; being provided with stretches out protrudes from elevator landing outside the deck, and aircraft transports mobile purpose between canopy to shut down as two-layer flight deck and orlop.The weak point of this patent is: the pillar stiffener between the double deck is the W type, and such design causes the lower layer space waste, also is unfavorable for using.
Summary of the invention purpose of the present invention is exactly to provide a kind of aircraft carrier simple in structure double-decked pillar stiffener, in the saves valuable space, optimizes structure.
In order to achieve the above object, the double-decked pillar stiffener of aircraft carrier provided by the invention comprises pillar stiffener, and wherein, pillar stiffener is a hollow cylinder shape, and pillar stiffener is by the metal manufacturing, and pillar stiffener has many; Pillar stiffener connects upper and lower two-layer deck, and pillar stiffener is erected at lower tween deck runway both sides and lower tween deck outer side edges edge.When the present invention used, pillar stiffener neither can influence the use of lower tween deck runway, also can wasting space.
The double-decked pillar stiffener of aircraft carrier provided by the invention has positive effect: pillar stiffener is a hollow cylinder shape, pillar stiffener is by the metal manufacturing, pillar stiffener has many, pillar stiffener connects upper and lower two-layer deck, pillar stiffener is erected at lower tween deck runway both sides and lower tween deck outer side edges edge, and is simple in structure; Pillar stiffener neither can influence the use of lower tween deck runway during use, also can not waste the space of lower tween deck preciousness, is applicable to all aircraft carriers.
Description of drawings the present invention will be further described in conjunction with the accompanying drawings, please referring to accompanying drawing:
Accompanying drawing 1 expression scheme drawing of the present invention.
Structure shown in the accompanying drawing 1 comprises: pillar stiffener 1, runway 2, lower tween deck 3.
The double-decked pillar stiffener of specific embodiment aircraft carrier provided by the invention comprises pillar stiffener 1, and wherein, pillar stiffener 1 is a hollow cylinder shape, and pillar stiffener 1 is by the metal manufacturing, and pillar stiffener 1 has many; Pillar stiffener 1 connects upper and lower two-layer deck, and pillar stiffener 1 is erected at lower tween deck 3 runways, 2 both sides and lower tween deck 3 outer side edges edges.When the present invention used, pillar stiffener 1 neither can influence the use of lower tween deck 3 runways 2, also can wasting space.
Protection domain of the present invention relates to all changes form recited above.
Claims (1)
1. the double-decked pillar stiffener of aircraft carrier comprises pillar stiffener (1), and pillar stiffener (1) connects upper and lower two-layer deck, and it is characterized in that: pillar stiffener (1) is a hollow cylinder shape, and pillar stiffener (1) is by the metal manufacturing, and pillar stiffener (1) has many; Pillar stiffener (1) is erected at lower tween deck (3) runway (2) both sides and lower tween deck (3) outer side edges edge.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2013101458826A CN103224030A (en) | 2013-04-11 | 2013-04-11 | Support pillar for double-layered deck of aircraft carrier |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2013101458826A CN103224030A (en) | 2013-04-11 | 2013-04-11 | Support pillar for double-layered deck of aircraft carrier |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN103224030A true CN103224030A (en) | 2013-07-31 |
Family
ID=48834723
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2013101458826A Pending CN103224030A (en) | 2013-04-11 | 2013-04-11 | Support pillar for double-layered deck of aircraft carrier |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN103224030A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112109916A (en) * | 2014-04-09 | 2020-12-22 | 兰威创新有限公司 | Runway arrangement |
Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2146430Y (en) * | 1990-11-19 | 1993-11-17 | 唐全国 | Aircraft-carrier flight deck |
| CN101740152A (en) * | 2009-12-22 | 2010-06-16 | 上海交通大学 | Semi-submerged small-waterplane-area mobile platform type marine nuclear power station |
| CN202279206U (en) * | 2011-10-12 | 2012-06-20 | 朱志斌 | Stable ship |
-
2013
- 2013-04-11 CN CN2013101458826A patent/CN103224030A/en active Pending
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2146430Y (en) * | 1990-11-19 | 1993-11-17 | 唐全国 | Aircraft-carrier flight deck |
| CN101740152A (en) * | 2009-12-22 | 2010-06-16 | 上海交通大学 | Semi-submerged small-waterplane-area mobile platform type marine nuclear power station |
| CN202279206U (en) * | 2011-10-12 | 2012-06-20 | 朱志斌 | Stable ship |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112109916A (en) * | 2014-04-09 | 2020-12-22 | 兰威创新有限公司 | Runway arrangement |
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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 | ||
| C02 | Deemed withdrawal of patent application after publication (patent law 2001) | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20130731 |