CN105947167A - Air suspension radar - Google Patents
Air suspension radar Download PDFInfo
- Publication number
- CN105947167A CN105947167A CN201610308141.9A CN201610308141A CN105947167A CN 105947167 A CN105947167 A CN 105947167A CN 201610308141 A CN201610308141 A CN 201610308141A CN 105947167 A CN105947167 A CN 105947167A
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- CN
- China
- Prior art keywords
- radar
- gas
- unit body
- inflation unit
- power
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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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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64B—LIGHTER-THAN AIR AIRCRAFT
- B64B1/00—Lighter-than-air aircraft
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Radar Systems Or Details Thereof (AREA)
Abstract
Air suspension radar comprises an air suspension platform, power sources, power driving parts and a radar assembly, wherein the air suspension platform comprises inflatable unit bodies; at least one face of each inflatable unit body is provided with a connector; pressure adjusting parts are arranged on the inflatable unit bodies; the power driving parts are matched with the power sources and used for achieving adjustment of position and height of the inflatable unit bodies; and the radar assembly is arranged on the inflatable unit bodies. The radar has the advantages of being wide in signal collection, high in precision, good in safety and flexible to control.
Description
Technical field
The present invention relates to radar application technical field, especially relate to a kind of be arranged on gas suspension platform, complete the gas suspension radar of radar detection at stratosphere.
Background technology
Radar includes transmitter, launches antenna, receiver, reception antenna, process part and display etc., by antenna, electromagnetic wave energy is launched to space a direction, after being in the electromagnetic wave that the object emission that this side up is encountered, radar antenna receives this electromagnetic wave, deliver to reception equipment process, reception equipment extracts some information of object and carries out corresponding Treatment Analysis, to obtain the parameter informations such as the position of target object, speed, height.
High altitude kite balloon radar is with captive balloon as carrier, and radar antenna, transmitter, the height of receiver lift-off to hundreds of to thousands of meters are carried out Low Altitude Target Detection, as AWACS and the good complement of home radar chain.Captive balloon carrier radar system economic performance is good, and equipment is simple, and exploitation and operating cost are low, but its flying height and detection range are limited, and general common high altitude kite balloon radar working depth is at 3000 meters, and limiting altitude is 6000 meters；Due to reasons such as balloon volume and cables, need mooring radar is drop to ground in harsh weather.
Disclosing high-altitude kite mooring radar method in the application for a patent for invention of Application No. 201110224877.5, the method is completed the lift-off of radar by kite manipulation device, and the method exists following defect: the 1) intensity of kite and inequality in service life；2) lift-off of kite 2-4 platform hoist engine and corresponding sensor is constituted, and overall dimensions is huge and heavy；3) rope of kite extends to high-altitude from ground, and not only intensity and the diameter of rope has particular/special requirement, and poor stability.
Summary of the invention
It is an object of the invention to provide a kind of gas suspension radar, this radar is arranged on knockdown gas and hangs on platform, gone up to the air to stratosphere by power drive portion, not only overcome radar altitude present in prior art inadequate, the problem that detection range is short, and without rope, safety is good, the technical scheme is that a kind of gas suspension radar, it is characterized in that: described gas suspension radar includes: gas hangs platform, described gas hangs platform and includes inflation unit body, equipped with adapter at least one side of described inflation unit body, described inflation unit body is provided with pressure adjustment unit part；Power source and supporting with described power source, for realizing the power drive portion of inflation unit body position and height adjustment；It is placed in the radar component on described inflation unit body.
The technical characteristic of the present invention also has: described radar component includes: antenna；Emitting portion；Receiving portion；Signal processing；Tcp data segment；Also include power pack.
The technical characteristic of the present invention also has: described radar component is phased-array radar assembly, and the antenna of described phased-array radar assembly is array antenna.
The technical characteristic of the present invention also has: described power source includes solar powered assembly, and described solar powered assembly connects the power pack of described radar component.
The technical characteristic of the present invention also has: described inflation unit body includes capsule skin, and being full of at described capsule Intradermal has gas, and the density of described gas is less than atmospheric density.
The technical characteristic of the present invention also has: described gas is helium or hydrogen.
The technical characteristic of the present invention also has: described power drive portion includes controlling parts, driving guiding parts and power part, and described power part includes air propeller.
The beneficial effects of the present invention is: 1) radar is except civilian uses, more value is also embodied in military use, it is the sensor collecting various military informations, and changes radar installation site, can collect extensively and information exactly, most important for military field.The gas suspension radar that the present invention provides hangs platform by gas, radar is risen to the stratosphere that weather conditions are good, it is being prevented effectively from while the external world causes signal disturbing, increase radar gather the height of signal and then expand the scope of signals collecting, and enhance the disguise of radar, reduce the probability found by reconnaissance plane etc..
2) this gas hangs radar and can be selected for phased-array radar, this kind of radar is by changing the synthesis mode of the sent wave beam of antenna surface array, change beam scanning direction, can reduce or avoid the antenna driver section part in mechanical radar completely, have scan efficiency height, beam direction changes speed soon, for the advantage that target signal measuring accuracy is high.Phased-array radar is arranged on gas and hangs on platform, compared to traditional mechanical type radar, not only reduce the volume of radar, and be effectively improved accuracy and the efficiency of military surveillance.
3) this radar has that signals collecting is extensive, precision is high, safety is good, the advantage of manoeuvrable.
Accompanying drawing explanation
Accompanying drawing 1 is inventive structure schematic diagram, and wherein 1 is that gas hangs platform, and 2 is solar panel Power Supply Assembly, and 3 is radar component, and 4 is inflation unit body, and 5 is solar powered assembly, and 6 is air propeller, and 7 is power drive portion.
Detailed description of the invention
Below in conjunction with the accompanying drawings, the detailed description of the invention of the present invention is illustrated.The invention discloses a kind of gas suspension radar, this gas suspension radar is under multiple inflation unit bodies 4 drive, after rising to certain altitude, each inflation unit body 4 is one can the individuality of self-movement, all can adjust position flexibly, and and then gas after making combination to hang position of platform adjustable, hang at gas and on platform, mounted radar component 3.
This gas suspension radar includes: gas hangs platform, gas hangs platform and includes that inflation unit body 4, inflation unit body 4 include capsule skin, is filled with, at capsule Intradermal, the gas that density is less than air, such as helium or hydrogen, little density gases full in inflation unit body 4 contributes to the lift-off of inflation unit body.Inflation unit body 4 at least one side is provided with adapter, typically all can install adapter in the upper and lower, left and right of inflation unit body, and inflation unit body 4 satisfactory gas sized by adapter is formed by connecting hangs platform.Inflation unit body is provided with power source and supporting with power source, for realizing the power drive portion of inflation unit body position and height adjustment, power source is solar energy type power supply mode, including solar powered assembly, this solar panel Power Supply Assembly is connected with the power pack of radar component, to realize the solar powered of radar component simultaneously.
The needs adjusted for pressure, prevent the explosion of the excessive inflation unit body caused of inflation unit body pressure in uphill process, this inflation unit body is provided with pressure adjustment unit part, portion gas is discharged in inflation unit body uphill process by these parts, and gas is filled with in decline inflation unit body.
Inflation unit body, under power drive portion drives, completes lift-off and the position adjustment of lift-off, hangs installation radar component on platform at the gas being made up of inflation unit body.The present embodiment has been selected phased-array radar assembly, this kind of radar component has the most intensive aerial array, any one array all can maneuver radar wave, adjacent several antennas i.e. have the function of a radar, therefore a radar can complete multiple target or the scanning in region or tracking simultaneously.This kind of radar component is arranged on inflation unit body, when inflation unit body rises, drives radar component rise and be positioned at stratospheric appropriate location, so, under the weather conditions that stratosphere is good, phased-array radar assembly can collect sufficient information, to meet the needs of military use.
In the present embodiment, power drive portion includes controlling parts, driving guiding parts and power part, power part includes air propeller 6, the adjustment of the positions such as the lifting being completed inflation unit body by air propeller, air propeller 6 can be selected for propeller, can drive the lift-off of inflation unit body when propeller rotational and adjust position as required.
Solar powered assembly in the present embodiment can be solar panel Power Supply Assembly or solar energy membrane Power Supply Assembly.
Certainly, described above not limitation of the present invention, the present invention is also not limited to the example above, change that those skilled in the art are made in the essential scope of the present invention, retrofits, adds or replaces, and falls within protection scope of the present invention.
Claims (7)
1. a gas suspension radar, it is characterised in that: described gas suspension radar includes: gas hangs platform, and described gas hangs
Platform includes inflation unit body, equipped with adapter at least one side of described inflation unit body, and described inflation unit
Body is provided with pressure adjustment unit part；Power source and supporting with described power source, be used for realizing inflation unit position
Put the power drive portion with height adjustment；It is placed in the radar component on described inflation unit body.
2. according to the gas suspension radar described in claim 1, it is characterised in that: described radar component includes: sky
Line；Emitting portion；Receiving portion；Signal processing；Tcp data segment；Also include power pack.
3. according to the gas suspension radar described in claim 2, it is characterised in that: described radar component is phased array
Radar component, the antenna of described phased-array radar assembly is array antenna.
4. according to the gas suspension radar described in claim 2, it is characterised in that: described power source includes solar energy
Power Supply Assembly, described solar powered assembly connects the power pack of described radar component.
5. according to the gas suspension radar described in claim 2, it is characterised in that: described inflation unit body includes capsule
Skin, is full of at described capsule Intradermal and has gas, and the density of described gas is less than atmospheric density.
6. according to the gas suspension radar described in claim 5, it is characterised in that: described gas is helium or hydrogen
Gas.
7. according to the gas suspension radar described in claim 1, it is characterised in that: described power drive portion includes
Controlling parts, drive guiding parts and power part, described power part includes air propeller.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610308141.9A CN105947167A (en) | 2016-05-10 | 2016-05-10 | Air suspension radar |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610308141.9A CN105947167A (en) | 2016-05-10 | 2016-05-10 | Air suspension radar |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN105947167A true CN105947167A (en) | 2016-09-21 |
Family
ID=56911251
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610308141.9A Pending CN105947167A (en) | 2016-05-10 | 2016-05-10 | Air suspension radar |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN105947167A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108693525A (en) * | 2018-03-23 | 2018-10-23 | 深圳高科新农技术有限公司 | Unmanned plane avoidance based on microwave radar imitative ground flight system |
Citations (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE2719893A1 (en) * | 1977-05-04 | 1978-11-09 | Erich Groeger | Monocoque type rigid dirigible - has series of rings of gas-tight cells in place of framework and held by envelope pressure or bonding |
| CN86105611A (en) * | 1986-07-23 | 1988-03-30 | 海斯塔航天发展公司 | Aircraft |
| WO1989010868A1 (en) * | 1988-05-13 | 1989-11-16 | Marcro Holdings Pty. Ltd. | Improved airship |
| DE20004028U1 (en) * | 2000-03-03 | 2000-09-07 | Epperlein Frank | Aircraft |
| DE10053775A1 (en) * | 2000-10-30 | 2002-05-08 | Frank Epperlein | Air vehicle, lighter than air with flexible outer hull and several separated inner gas cells has gas cells fastened above and below hull and stability of hull against bending moments generated by inner excess pressure |
| US6527223B1 (en) * | 2002-08-05 | 2003-03-04 | Richard Warfield Mondale | Platform-type airship |
| KR20110029318A (en) * | 2009-09-15 | 2011-03-23 | 이문희 | Carrier aircraft |
| US20110315811A1 (en) * | 2008-05-15 | 2011-12-29 | King Fahd University Of Petroleum And Minerals | Lighter-than-air vehicle for shading |
| CN102407934A (en) * | 2011-12-05 | 2012-04-11 | 魏少康 | Hitching type movable radar |
| CN205087138U (en) * | 2015-10-22 | 2016-03-16 | 深圳光启合众科技有限公司 | Multi -rotor aircraft |
-
2016
- 2016-05-10 CN CN201610308141.9A patent/CN105947167A/en active Pending
Patent Citations (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE2719893A1 (en) * | 1977-05-04 | 1978-11-09 | Erich Groeger | Monocoque type rigid dirigible - has series of rings of gas-tight cells in place of framework and held by envelope pressure or bonding |
| CN86105611A (en) * | 1986-07-23 | 1988-03-30 | 海斯塔航天发展公司 | Aircraft |
| WO1989010868A1 (en) * | 1988-05-13 | 1989-11-16 | Marcro Holdings Pty. Ltd. | Improved airship |
| DE20004028U1 (en) * | 2000-03-03 | 2000-09-07 | Epperlein Frank | Aircraft |
| DE10053775A1 (en) * | 2000-10-30 | 2002-05-08 | Frank Epperlein | Air vehicle, lighter than air with flexible outer hull and several separated inner gas cells has gas cells fastened above and below hull and stability of hull against bending moments generated by inner excess pressure |
| US6527223B1 (en) * | 2002-08-05 | 2003-03-04 | Richard Warfield Mondale | Platform-type airship |
| US20110315811A1 (en) * | 2008-05-15 | 2011-12-29 | King Fahd University Of Petroleum And Minerals | Lighter-than-air vehicle for shading |
| KR20110029318A (en) * | 2009-09-15 | 2011-03-23 | 이문희 | Carrier aircraft |
| CN102407934A (en) * | 2011-12-05 | 2012-04-11 | 魏少康 | Hitching type movable radar |
| CN205087138U (en) * | 2015-10-22 | 2016-03-16 | 深圳光启合众科技有限公司 | Multi -rotor aircraft |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108693525A (en) * | 2018-03-23 | 2018-10-23 | 深圳高科新农技术有限公司 | Unmanned plane avoidance based on microwave radar imitative ground flight system |
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| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20160921 |
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| RJ01 | Rejection of invention patent application after publication |