CN101944650A - Airship type antenna dragging device for aircraft carrier - Google Patents
Airship type antenna dragging device for aircraft carrier Download PDFInfo
- Publication number
- CN101944650A CN101944650A CN2009103041638A CN200910304163A CN101944650A CN 101944650 A CN101944650 A CN 101944650A CN 2009103041638 A CN2009103041638 A CN 2009103041638A CN 200910304163 A CN200910304163 A CN 200910304163A CN 101944650 A CN101944650 A CN 101944650A
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- China
- Prior art keywords
- aircraft carrier
- dirigible
- airship
- type antenna
- equipment
- 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.)
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Abstract
The invention relates to an airship type antenna dragging device for an aircraft carrier, which belongs to mechanical and electronic integrated devices for increasing a radar detection area and an early warning range on an aircraft carrier in the technical field of military application. The device mainly comprises a radar antenna (1), a circular or elliptic hard shell airship (2), a steel cable and data line (3), a windlass (4), power equipment (5), a conducting control device (6), a safe exhaust valve (7), an inflating pipe (8), an exhaust opening (9), a closing steel rib (10), and other equipment and parts.
Description
Technical field:
The present invention relates to military technology equipment field, be specifically related to a kind of aircraft carrier radar antenna towing gear.
Background technology:
The greatness conception of the establishment of a harmonious world that proposes according to government, China must set up the aircraft carrier fleet that can undertake the task of safeguarding world peace.Putting before this, it is promising important that the warning of aircraft carrier fleet and communication just seem.Common radar antenna all is fixed on the warship body usually, because the angularity of the earth self, but cause scanning distance limited, cause many inconvenience for scouting, early warning work, make the combat readiness time hasty, hurry.And present carrier-borne torpedo reaches the over the horizon emission to the warship guided missile, brings bigger challenge for especially scouting, the early warning work of naval vessels.In order to realize that the enemy finds earlier, oppose the guiding of opening fire earlier, thoroughly solve this type of problem, so improving, this device of invention defends warning.
Summary of the invention: the present invention will provide a kind of aircraft carrier with filling helium dirigible trailing aerial device.Height, the detection range that its rises be far away, simple in structure, be convenient to folding and unfolding, is desirable detection equipment.
The object of the present invention is achieved like this: radar antenna is assembled on a circle or the oval dirigible, after dirigible is full of helium, can goes up to the air, make scanning, scouting, early warning distance improve greatly.Use wirerope to carry out mooring warship body below, utilize hoist engine to carry out folding and unfolding, and assemble certain power set and be used for orientation and move with warship.Dirigible itself does not carry the energy, provides power and data to accept by cable and data wire.
Main member of the present invention: radar antenna 1., circular or oval duricrust dirigible 2., wirerope cable and data wire 3., hoist engine 4., power-equipment 5., commander's control device 6., safety exhaust 7., gas-filled tube 8., exhaust outlet 9., the closing in reinforcing bar 10.
Description of drawings:
Concrete structure drawings attached of the present invention provides.
Fig. 1 is the aircraft carrier airship type trailing aerial device elevation that proposes according to the present invention.
Fig. 2 is the A-A profile.
Fig. 3 is the Safety control valve detail drawing.
Specific implementation method:
The operating position of this device is as follows: 2. dirigible is full of helium makes it floating, 3. connect hoist engine 4. with wirerope cable and data wire, utilize commander's control device 6. to control height.With radar antenna 1. hang on dirigible 2. the below, wirerope cable and data wire 3. connect respectively radar antenna 1. with power-equipment 5..Hoist engine 4. cable laying arrives desired height, closes hoist engine and 4. also fixes.When naval vessels travelled or big windage is arranged, 5. the equipment that can turn on the power came together to advance or resist windage with naval vessels.
Because the variation of height, radar antenna has improved to be looked under it and the Space surveillance scope, prepares to create favorable conditions for improving warning and fight.This antenna can repeat to recycle, and also can be detained in the air for a long time and guard against.Can be according to the difference of task, change various radar antennas or multiple antenna hangs successively, for the triumph of fight is taken a firm foundation.
When running into sudden change weather, in the time of dirigible need being reduced to safe altitude rapidly, can utilize commander's control device 6. to open safety exhaust 7., 9. discharge helium according to the atmospheric density principle voluntarily from exhaust outlet, drop to safe altitude rapidly.Then, carry out take-up or inflation come-up again according to actual conditions.
Claims (3)
1. aircraft carrier is that stainless steel cloth or memory titanium wire network and foamed plastics constitute jointly with the duricrust material of dirigible towing scanner unit.
2. aircraft carrier is to drive dirigible motion and the power-equipment of resisting windage with the dynamic characteristic of dirigible towing scanner unit, has control appliance, motor and screw to constitute.
3. aircraft carrier is to finish by the unlatching of control appliance control safety valve with the emergency safety landing feature of dirigible towing scanner unit.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2009103041638A CN101944650A (en) | 2009-07-09 | 2009-07-09 | Airship type antenna dragging device for aircraft carrier |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2009103041638A CN101944650A (en) | 2009-07-09 | 2009-07-09 | Airship type antenna dragging device for aircraft carrier |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN101944650A true CN101944650A (en) | 2011-01-12 |
Family
ID=43436520
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2009103041638A Pending CN101944650A (en) | 2009-07-09 | 2009-07-09 | Airship type antenna dragging device for aircraft carrier |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN101944650A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105742779A (en) * | 2016-02-15 | 2016-07-06 | 中国船舶重工集团公司第七〇五研究所 | Flexible inflatable antenna floating body inflation control device |
| CN106549681A (en) * | 2016-05-06 | 2017-03-29 | 中国人民解放军海军工程大学 | A kind of very long wave transmission system based on aerial platform |
| CN114455058A (en) * | 2022-03-17 | 2022-05-10 | 苏州璟融环保科技有限公司 | Environment-friendly solar farmland yield increasing instrument |
-
2009
- 2009-07-09 CN CN2009103041638A patent/CN101944650A/en active Pending
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105742779A (en) * | 2016-02-15 | 2016-07-06 | 中国船舶重工集团公司第七〇五研究所 | Flexible inflatable antenna floating body inflation control device |
| CN105742779B (en) * | 2016-02-15 | 2018-04-13 | 中国船舶重工集团公司第七〇五研究所 | A kind of flexible inflatable antenna floating body aeration control device |
| CN106549681A (en) * | 2016-05-06 | 2017-03-29 | 中国人民解放军海军工程大学 | A kind of very long wave transmission system based on aerial platform |
| CN114455058A (en) * | 2022-03-17 | 2022-05-10 | 苏州璟融环保科技有限公司 | Environment-friendly solar farmland yield increasing instrument |
| CN114455058B (en) * | 2022-03-17 | 2024-02-20 | 苏州璟融环保科技有限公司 | Environment-friendly solar farmland yield-increasing instrument |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C02 | Deemed withdrawal of patent application after publication (patent law 2001) | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20110112 |