CN109270413A - A kind of FSS radar overcoat layer thunder and lightning is sliding to dodge voltage test method - Google Patents

A kind of FSS radar overcoat layer thunder and lightning is sliding to dodge voltage test method Download PDF

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Publication number
CN109270413A
CN109270413A CN201710586221.5A CN201710586221A CN109270413A CN 109270413 A CN109270413 A CN 109270413A CN 201710586221 A CN201710586221 A CN 201710586221A CN 109270413 A CN109270413 A CN 109270413A
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CN
China
Prior art keywords
lightning
thunder
radar
overcoat layer
sliding
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Pending
Application number
CN201710586221.5A
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Chinese (zh)
Inventor
高俊福
乔承晓
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AVIC Research Institute Special Structures Aeronautical Composites
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AVIC Research Institute Special Structures Aeronautical Composites
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Application filed by AVIC Research Institute Special Structures Aeronautical Composites filed Critical AVIC Research Institute Special Structures Aeronautical Composites
Priority to CN201710586221.5A priority Critical patent/CN109270413A/en
Publication of CN109270413A publication Critical patent/CN109270413A/en
Pending legal-status Critical Current

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    • GPHYSICS
    • G01MEASURING; TESTING
    • G01RMEASURING ELECTRIC VARIABLES; MEASURING MAGNETIC VARIABLES
    • G01R31/00Arrangements for testing electric properties; Arrangements for locating electric faults; Arrangements for electrical testing characterised by what is being tested not provided for elsewhere
    • G01R31/12Testing dielectric strength or breakdown voltage ; Testing or monitoring effectiveness or level of insulation, e.g. of a cable or of an apparatus, for example using partial discharge measurements; Electrostatic testing
    • G01R31/1227Testing dielectric strength or breakdown voltage ; Testing or monitoring effectiveness or level of insulation, e.g. of a cable or of an apparatus, for example using partial discharge measurements; Electrostatic testing of components, parts or materials
    • G01R31/1263Testing dielectric strength or breakdown voltage ; Testing or monitoring effectiveness or level of insulation, e.g. of a cable or of an apparatus, for example using partial discharge measurements; Electrostatic testing of components, parts or materials of solid or fluid materials, e.g. insulation films, bulk material; of semiconductors or LV electronic components or parts; of cable, line or wire insulation
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01RMEASURING ELECTRIC VARIABLES; MEASURING MAGNETIC VARIABLES
    • G01R19/00Arrangements for measuring currents or voltages or for indicating presence or sign thereof
    • G01R19/0084Arrangements for measuring currents or voltages or for indicating presence or sign thereof measuring voltage only

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  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Details Of Aerials (AREA)

Abstract

The present invention relates to radome more particularly to a kind of sliding sudden strain of a muscle voltage test methods of FSS radar overcoat layer thunder and lightning.Thunder and lightning generator exports lightning surge to radar overcoat layer by electrode according to thunder and lightning waveform, and records the sliding sudden strain of a muscle voltage value of the radar overcoat layer under two electrode difference spacing of radome, and fits the sliding relation curve for dodging voltage value and electrode spacing of radar overcoat layer.Provide the method that one kind accurately tests the sliding lightning pressure of FSS radar overcoat layer in the case of lightning impulse.

Description

A kind of FSS radar overcoat layer thunder and lightning is sliding to dodge voltage test method
Technical field
The present invention relates to radome more particularly to a kind of sliding sudden strain of a muscle voltage test methods of FSS radar overcoat layer thunder and lightning.
Background technique
FSS radome surface, which generally sprays defence, makes antistatic coating, has the function of anticorrosion and antistatic.And aircraft Thunderstorm Weather can be in-flight encountered in the sky, and inevitably ash is struck by lightning, and for FSS radome, lightning leader is possible to FSS radome surface is fallen in, is dodged by the way that the figure layer on FSS radome surface is sliding to lightning protection systems such as shunt bars, thus water conservancy diversion To aircraft metal fuselage, finally release.
In the design process of FSS radome lightning protection system, the cunning lightning pressure of FSS radome surface covering is to thunder and lightning The design of guard system has important influence, and traditional test method is tested using DC voltage or power-frequency voltage, then It is realized in design by increasing biggish safe clearance, design result is more coarse.
Summary of the invention
The purpose of the present invention: the side of the sliding lightning pressure of FSS radar overcoat layer in the case of the accurate test lightning impulse of one kind is provided Method.
Technical solution of the present invention: a kind of FSS radar overcoat layer thunder and lightning is sliding to dodge voltage test method, it is characterised in that described Method are as follows: thunder and lightning generator exports lightning surge to radar overcoat layer by electrode according to thunder and lightning waveform, and records radar The sliding sudden strain of a muscle voltage value of radar overcoat layer under two electrode difference spacing is covered, and fits the sliding sudden strain of a muscle voltage value of radar overcoat layer and electrode The relation curve of spacing.
Preferably, the thunder and lightning waveform is GJB 3567-99 " military aircraft lightning protection qualification test method " regulation Simulation thunder and lightning waveform A wave and D wave.
Preferably, the electrode is laminated structure, and has the curved edge of smooth transition, and electrode is fitted in radar Overcoat layer surface.
Preferably, two electrodes on radome are fitted in mirror symmetry.
Preferably, the thickness of electrode is 0.1mm~0.15mm.
Preferably, the electrode is semicircle laminated structure.
Preferably, the radius R of electrode is more than or equal to 50mm.
Preferably, the equidistant increase of the spacing of two electrodes.
Beneficial effects of the present invention:
This method uses simulation thunder and lightning waveform as defined in GJB 3567-99 " military aircraft lightning protection qualification test method " A wave and D wave measurement ensure that the data of test acquisition can be used in lightning protection and design and pass through radome identification examination It tests, to keep the design of lightning protection more true and reliable.
Pellet electrode thickness is smaller can be guaranteed just to be attached to radome coating surface after electric arc occurs, and avoid the jump of electric arc It jumps and punctures air, ensure that test result for sliding lightning pressure.
Electrode, which has the curved edge of smooth transition, and electrode is fitted in radome coating surface can be effectively reduced two The sliding local voltage concentration phenomenon for dodging initial position being likely to occur between electrode, while electric current breakdown cover wall being avoided to enter in cover The FSS screen in portion.
Semicircular electrode radius is more than or equal to 50mm, can effectively ensure that the sliding initial position that dodges between two electrodes in circle Arc front end, to guarantee that the sliding spacing of dodging of electric arc is default space D.
Detailed description of the invention
Fig. 1 is testpieces placement position;
Fig. 2 is test electrode schematic diagram;
Fig. 3 thunder and lightning analog waveform A;
Fig. 4 thunder and lightning analog waveform B;
Fig. 5 electrode adhesive effect figure;
The arc-shaped pellet electrode of Fig. 6;
Fig. 7 ellipse pellet electrode.
In figure: 1 is electrode, and 2 be electrode, and 3 be testpieces.
Specific embodiment
Embodiment
When testing, electrode 1 and electrode 2 are bonded on radome surface, the symmetry axis of electrode 1 and electrode 2 is same On straight line, the initial space D of electrode 1 and electrode 2 is 50mm.Testpieces 3 is placed on test fixture, electrode 1 and thunder and lightning Generator connection, electrode 2 are grounded.
By adjusting thunder and lightning generator, thunder and lightning generator is enable to export GJB 3567-99 " military aircraft lightning protection mirror Determine test method " as defined in simulation thunder and lightning waveform A wave and D wave.Then it is tested, records the collected mould of data acquisition equipment The cunning lightning of coating surface presses U between quasi- lightning wave breakdown electrode 1 and electrode 2, uses the sliding arc dodged of digital camera record thunder and lightning Road (is capable of deciding whether sliding dodge occur on radome surface by the arc road that digital camera is shot).It records to glide according to table 1 and dodge Voltage U and electrode spacing D.
Table 1 is sliding to dodge graphic voltmeter
Test waveform Sliding lightning pressure (U) Electrode spacing (D)
Adjustment electrode D spacing is 100mm, records sliding lightning pressure, and so on, stop surveying when test to spacing is 400mm Examination.The relation curve of sliding lightning pressure and electrode spacing is fitted according to the data recorded in table 1.
In case study on implementation, testing the thunder and lightning analog waveform used is GJB 3567-99 " military aircraft lightning protection identification Test method " as defined in the waveform (as shown in Figure 3 and Figure 4) that uses of lightning protection qualification test, can authentic testing go out radar Cunning lightning pressure of overcoat layer during qualification test provides truthful data for lightning protection design.
The click used in case study on implementation is semicircle pellet electrode, and electrode shape is as shown in Fig. 2, on radome surface Bonding graph Fig. 5 shown in.For pellet electrode thickness in 0.1mm~0.15mm, electrode height can be guaranteed by being bonded in radome surface The distance on radome surface is smaller out, after thunder and lightning is issued from 1 leading edge of electrode, before thunder and lightning can be along radome coating surface Row, until reaching grounding electrode 2.
Electrode edge is that the arc with smooth transition can be avoided electrode leading edge and thunder and lightning centrostigma occurs, guarantee thunder and lightning from The most leading edge of electrode 1 issues, and receives from the most leading edge of electrode 2, and the cunning lightning pressure tested out is the cunning lightning pressure of space D;It simultaneously can also It enough avoids electrode from thunder and lightning concentration effect locally occur, generates coupling effect with the FSS screen inside radome and puncture radome cover Wall reaches the FSS screen inside radome.
The electrode used in case study on implementation may be Fig. 6 and the curved edge with smooth transition shown in fig. 7 Pellet electrode.The central angle of sheet arc-shaped electrode in Fig. 6 should be greater than 120 °.

Claims (8)

1. a kind of FSS radar overcoat layer thunder and lightning is sliding to dodge voltage test method, it is characterised in that the method are as follows: thunder and lightning generator Lightning surge is exported to radar overcoat layer by electrode according to thunder and lightning waveform, and is recorded under two electrode difference spacing of radome Radar overcoat layer it is sliding dodge voltage value, and fit the sliding relation curve for dodging voltage value and electrode spacing of radar overcoat layer.
2. a kind of FSS radar overcoat layer thunder and lightning according to claim 1 is sliding to dodge voltage test method, it is characterised in that described Thunder and lightning waveform be simulation thunder and lightning waveform A wave and D as defined in GJB 3567-99 " military aircraft lightning protection qualification test method " Wave.
3. a kind of FSS radar overcoat layer thunder and lightning according to claim 1 is sliding to dodge voltage test method, it is characterized in that: it is described Electrode be laminated structure, and there is the curved edge of smooth transition, electrode is fitted in radome coating surface.
4. a kind of FSS radar overcoat layer thunder and lightning according to claim 3 is sliding to dodge voltage test method, it is characterized in that: fitting Two electrodes on radome are in mirror symmetry.
5. a kind of FSS radar overcoat layer thunder and lightning according to claim 3 is sliding to dodge voltage test method, it is characterized in that: it is described Thickness of electrode be 0.1mm~0.15mm.
6. a kind of FSS radar overcoat layer thunder and lightning according to claim 3 is sliding to dodge voltage test method, it is characterized in that: it is described Electrode be semicircle laminated structure.
7. a kind of FSS radar overcoat layer thunder and lightning according to claim 6 is sliding to dodge voltage test method, it is characterized in that: electrode Radius R be more than or equal to 50mm.
8. a kind of FSS radar overcoat layer thunder and lightning according to claim 1 is sliding to dodge voltage test method, it is characterized in that: two The equidistant increase of the spacing of electrode.
CN201710586221.5A 2017-07-18 2017-07-18 A kind of FSS radar overcoat layer thunder and lightning is sliding to dodge voltage test method Pending CN109270413A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201710586221.5A CN109270413A (en) 2017-07-18 2017-07-18 A kind of FSS radar overcoat layer thunder and lightning is sliding to dodge voltage test method

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201710586221.5A CN109270413A (en) 2017-07-18 2017-07-18 A kind of FSS radar overcoat layer thunder and lightning is sliding to dodge voltage test method

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CN109270413A true CN109270413A (en) 2019-01-25

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Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2007134132A (en) * 2005-11-09 2007-05-31 Ngk Spark Plug Co Ltd Method and device for inspecting insulator for spark plug
CN101345458A (en) * 2008-05-22 2009-01-14 山东齐鲁电机制造有限公司 Full anti-dizzy VPI impregnation stator line stick and its industrial frequency overpressure-resistant detection method
CN203894370U (en) * 2014-06-10 2014-10-22 国家电网公司 Insulating separator plate surface power-frequency voltage withstanding testing device
CN104535911A (en) * 2015-01-14 2015-04-22 上海申和热磁电子有限公司 Method for testing performance of aluminum spraying coating

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2007134132A (en) * 2005-11-09 2007-05-31 Ngk Spark Plug Co Ltd Method and device for inspecting insulator for spark plug
CN101345458A (en) * 2008-05-22 2009-01-14 山东齐鲁电机制造有限公司 Full anti-dizzy VPI impregnation stator line stick and its industrial frequency overpressure-resistant detection method
CN203894370U (en) * 2014-06-10 2014-10-22 国家电网公司 Insulating separator plate surface power-frequency voltage withstanding testing device
CN104535911A (en) * 2015-01-14 2015-04-22 上海申和热磁电子有限公司 Method for testing performance of aluminum spraying coating

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
段泽民等: "《中华人民共和国国家军用标准》", 24 March 1999 *

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Application publication date: 20190125

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