GMC-I集團的航空電子電氣測試方案及應(yīng)用解析
在航空運輸領(lǐng)域,安全一直是首要關(guān)注的重點。對飛機電子電氣系統(tǒng)的測試測量對于確保飛行安全極為重要。在這方面,GMC-I集團作為行業(yè)領(lǐng)先的測試儀器供應(yīng)商,提供了一系列專業(yè)的航空電子電氣測試解決方案。
航空電子電氣測試背景
? 航空運輸安全第一,飛機電子電氣系統(tǒng)測試測量至關(guān)重要
? 低阻測量:機體保持低阻通路,防止雷擊產(chǎn)生大熱量及靜電放電產(chǎn)生的EMI干擾
? 絕緣測試:電線電纜老化對飛行安全隱患巨大,絕緣測試是重要判斷依據(jù)
? 常規(guī)電子/電氣測試:飛機電子電氣系統(tǒng)安全保障
GMC-I常用測試儀器
? MTRAHIT 27EX Airbus
? MTRAHIT IM XTRA BT
? MTRAHIT 27M
? METRAHIT ISO@AERO
? Aero Master Test Kit I / II
? CROPICO DO7010
? PROFITEST INRO
? MAVOSPEC BASE
? MAVO SPOT 2 USB
手持式防爆毫歐表
法國空客Airbus飛機
維修手冊AMM (A300..380) 編碼 97F92003500 000
總裝線FAL 編碼 97000F92001015000
?CROPICO DO7010
高精度微歐計
巴西航空維修手冊工具
?AERO MASTER TEST KIT I / II & METRAHIT 27M
| Range | Resolution | Typical Current | FSV | Accuracy at 20°C±5°C 1 year | |||||
| 6Ω | 1mΩ | 100mA/1A | ±(0.1% Rdg +0.1% FS) | 40ppm Rdg+30ppm FS | |||||
| 600mΩ | 100μΩ | 1/10A | ±(0.1% Rdg +0.1% FS) | 40ppm Rdg+30ppm FS | |||||
| 60mΩ | 10μΩ | 1/10A | ±(0.1% Rdg +0.1% FS) | 40ppm Rdg+30ppmFS | |||||
| 6mΩ | 1μΩ | 1/10A | ±(0.1% Rdg +0.1% FS) | 40ppm Rdg+30ppmFS | |||||
| PART NUMBER | OPT OR ALT | REPLACED BY ORSUPERSEDED |
STILL USABLE |
EFFECTIVITY | ||||
| RCP2JE | . | GSE 008/PN RCP2A | YES | ALL | ||||
| RCP2A | . | GSE 008/PN DO7010 | YES | ALL | ||||
| DO7010 | - | . | YES | ALL | ||||
?AERO MASTER TEST KIT I / II & METRAHIT 27M
METRAHIT ISO@AERO / Aero Master Test Kit
手持式絕緣萬用表
荷蘭皇家航空公司KLM定制的波音飛機檢測維護工具
適用于航空維護、維修的68個航空電子常用測試配件
METRAHIT 27M(計劃停產(chǎn))
METRAHIT 27M(計劃停產(chǎn))
?METRAHIT IM TECH/ XTRA BT
手持式 毫歐 / 絕緣毫歐 多用表
?MAVO SPOT 2 USB
高精度瞄點式亮度計
航空電子測試應(yīng)用介紹
易爆環(huán)境測量內(nèi)部或外的低阻試 易爆環(huán)境測量內(nèi)部或外的低阻試
易爆環(huán)境測量內(nèi)部或外部的低阻測試飛機燃油箱內(nèi)側(cè)接觸電阻(壓接測試) METRAHIT 27EX Airbus
? 毫歐表
? 測試電流 I < 100mA
? 背光顯示
? 本質(zhì)安全型 符合:
EN 60079-0 and 60079-11
? INERIS防爆證書件號:
INERIS 05ATEX0040
? 防爆等級:Ex II 2 G Ex ia IIA T4 Gb
?環(huán)境溫度:-10°C….+50°C
? 空客維修手冊Airbus AMM (A300..380)編碼 97F92003500 000
? 總裝線FAL 編碼 97000F92001015000

故障:

靜電放電測試
作用:
機身空氣摩擦積累靜電,尖端放電避免靜電干擾通信和導(dǎo)航系統(tǒng)
復(fù)合材料機身對放電刷要求更高
類型:
A型30°傾角,B型平行固定
| LOCATION | QTY | REMARKS |
|
Wing tip and aileron. ① |
9 per wing. | 2m ay be missing on each wing. |
| Horizontal stabilizer tip zone.② | 5 per side. | 1 may be missing on each side. |
| Fin and Rudder.③ | 5. | 1 may be missing. |
| Flap track fairing④ | 3 per wing. | 1 may be missing on each wing. |
故障:
換季工作
雷擊發(fā)生時,放電刷損壞
物理損壞(松動、腐蝕…)
內(nèi)部損壞(內(nèi)部結(jié)構(gòu)損壞,阻值變化…)
靜電放電刷電阻測量 第一部分絕緣電阻測試
METRAHIT ISO@AERO METRAHIT IM XTRA BT
依照:波音飛機AMM維修手冊
Boeing 737- 300/400/500
? 任務(wù):23-61-00-766-010
? 章節(jié):第三章(1) – (5)點
? 使用絕緣電阻測試儀器,設(shè)置測試電壓為500V
? 用濕毛巾或金屬絲包裹以便與放電刷末端均勻接觸
? 將絕緣測試儀器表筆連接到放電刷尖端和底座
? 對于A型:測試結(jié)果大概在6至120MΩ之間
? 對于B型:測試結(jié)果大概在6至200MΩ之間
靜電放電刷電阻測量 第二部分搭接電阻測試
靜電放電刷電阻測量 第二部分搭接電阻測試
METRAHIT 27M
METRAHIT IM XTRA BT CROPICO DO7010
? 依照:波音飛機AMM維修手冊Boeing 737- 300/400/500
? 任務(wù):23-61-00-766-010
? 章節(jié):第三章(6) – (11)點
? 將毫歐表測試探針連接到放電刷底座和飛機表面搭接處
? 對于金屬面板的阻值需低于0.05Ω
? 玻璃纖維層壓板蓋平噴鋁蓋或玻璃纖維織物阻值需低于0.50Ω
? 安裝在沒有鋁層的復(fù)合板上的放電器底座的阻值需低于5Ω使用經(jīng)認證可用于爆炸區(qū)域(本質(zhì)安全)的毫歐表
METRAHIT 27EX Airbus
燃油泵的絕緣測試
? 根據(jù)波音747服務(wù)公告-第01部分
747-28A-2194
? 燃油 - 分配 - 燃油增壓和超馳/噴射泵 - 檢查
BACKGROUND
This inspection will make sure the 747 fuel pumps
will not cause a fuel leak.Operators have sent reports of fuel leaks at the fuel boost and override/jetison pumps.
The reports tell that eight fuel pumpe have been removed for this reason. The removed fuel pumps had between
34.000-67 ,000 hours since new or since overhaul. The leaks occurred at the pump/wire bundle interface.
The result of one leak was a fire at an inboard main tank jettison pump during maintenance.
The reports tell that eight fuel pumpe have been removed for this reason. The removed fuel pumps had between
34.000-67 ,000 hours since new or since overhaul. The leaks occurred at the pump/wire bundle interface.
The result of one leak was a fire at an inboard main tank jettison pump during maintenance.
METRAHIT ISO@AERO
量程:5kΩ...3100MΩ @ 10, 50,100,250,500 V
根據(jù)波音747服務(wù)公告-第02部分
文章來源于GMC-I集團,深圳銀飛公司有售航空電子電氣常用測試儀器
C. Special Tools and Equipment
1. A special megohmmeter is necessary to do the electrical check of the fuel pump on the airplane.
The megohmmeter must have 10VDC and 500VDC voltage supply options with a maximum short
circuit current of 5 milliamperes. We use a QuadTech model 1864 megohmmeter. Any equivalent
meter is acceptable. The QuadTech model 1864 Is available from:
COMPLIANCE
Boeing recommends that the initial inspection be accomplished at the next opportunity when
manpower and facilities are available. For pumps with insulation resistance between
1and5 megohms when the 500VDC is done, it is recommended that the pump be replaced. If the
pump is not replaced, do the inspection of this pump at every A-check or an equivalent time.
For pumps with insulation resistance greater than 5 megohms
For pumps with insulation resistance greater than 5 megohms
when the 500VDC is done, the inspection should be repeated at every
C-check or an equal time period after the initial inspection.
C-check or an equal time period after the initial inspection.
CAUTION:
The fuolpumpe are in. flammahie, leakage zones. Each pump is tested at 10 VDC before it is tested at 500 VDC.
The 10 VDC test is to find fuel pumps with low insulaton resistance that can arc or overneat when a high voltage ls
aplled. the results of the 10 VDC test determine if the 500 VDC test is done on a fuel pump installed on the airplane.
GMC-I集團的航空電子電氣測試方案以其專業(yè)性和創(chuàng)新性,為航空業(yè)的安全提供了有力保障。通過精準(zhǔn)的測試和測量,確保飛機電子電氣系統(tǒng)的穩(wěn)定運行,為全球的航空運輸安全做出了重要貢獻。The 10 VDC test is to find fuel pumps with low insulaton resistance that can arc or overneat when a high voltage ls
aplled. the results of the 10 VDC test determine if the 500 VDC test is done on a fuel pump installed on the airplane.
文章來源于GMC-I集團,深圳銀飛公司有售航空電子電氣常用測試儀器



