CN103309343A - Heating control box detection device of airplane windshield - Google Patents

Heating control box detection device of airplane windshield Download PDF

Info

Publication number
CN103309343A
CN103309343A CN201210060893XA CN201210060893A CN103309343A CN 103309343 A CN103309343 A CN 103309343A CN 201210060893X A CN201210060893X A CN 201210060893XA CN 201210060893 A CN201210060893 A CN 201210060893A CN 103309343 A CN103309343 A CN 103309343A
Authority
CN
China
Prior art keywords
heating
control enclosure
phase
signal
resistance
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.)
Granted
Application number
CN201210060893XA
Other languages
Chinese (zh)
Other versions
CN103309343B (en
Inventor
王利
张宇翔
齐彦宾
李铜
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Shaanxi Aircraft Industry Co Ltd
Original Assignee
AVIC Shaanxi Aircraft Industry Group Corp Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by AVIC Shaanxi Aircraft Industry Group Corp Ltd filed Critical AVIC Shaanxi Aircraft Industry Group Corp Ltd
Priority to CN201210060893.XA priority Critical patent/CN103309343B/en
Publication of CN103309343A publication Critical patent/CN103309343A/en
Application granted granted Critical
Publication of CN103309343B publication Critical patent/CN103309343B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Landscapes

  • Testing Of Short-Circuits, Discontinuities, Leakage, Or Incorrect Line Connections (AREA)
  • Control Of Resistance Heating (AREA)

Abstract

The invention belongs to the testing technology and relates to a heating control box detection device of an airplane windshield. The heating control box detection device of the airplane windshield comprises an AC signal module, a DC display module, a resistance conversion module and a connection output module. The AC signal module for providing a three phase current signal to a heating control box, the DC display module for providing a DC signal to the heating control box, and the resistance conversion module for providing a resistance signal to the heating control box are mutually independent, and are respectively connected with the connection output module which is used for providing an output signal to the heating control box. The AC signal module comprises a left three phase AC mutual inductor, a right three phase AC mutual inductor, a change over switch and an externally connected load. According to the invention, the one phase 115V is used to replace the three phase 115V as a power supply, and one slide bar resistor is used to replace three load resistors. The detection circuit is effectively simplified; the production cost of the detection device is reduced; and the detection work is easier to carry out.

Description

A kind of control enclosure pick-up unit of heating of aircraft windshield
Technical field
The invention belongs to measuring technology, relate to a kind of control enclosure pick-up unit of heating of aircraft windshield.
Background technology
Aircraft before fortune 8 certain model, driver's windshield is 4, they are respectively left-hand drive person's side glass, left-hand drive person's front glass, right driver's front glass, right driver side surface glass, these 4 windshields all are to adopt single-phase 115V power supply to power for 1 temperature and resistance in the glass, realization is heated to 4 windshields, guarantee the aviator in the high-altitude to the observation outside the machine.Begin from certain model, driver's windshield changes 2 into by 4, each 1 of left and right sides driver, and every block of glass also is original 12 times, it is obviously open to make driver's high-altitude machine observe the visual field outward.
Because the windshield area increases, so every block of interior resistance of heating of glass also is increased to 3 by 1, power supply changes present three-phase 115V into also by original single-phase 115V, powers for respectively 3 temperature and resistances in the windshield by A, B, the C three-phase of three-phase 115V power supply.As shown in Figure 1, three live wire A phases, B phase, C of this three-phase 115V power supply are three through wires holes of a, b, c that pass the three-phase alternating current mutual inductor respectively mutually, three-phase current signal is provided for the XJW-1 glass control enclosure of heating, with realize to about 2 windshields add temperature control.Therefore the configuration of existing single-phase 115V power supply power supply mode and single ohmic load can't have been satisfied the heat needs of control enclosure ground detection of the XJW-1 glass of aircraft after certain model.
Summary of the invention
The objective of the invention is: propose a kind of control enclosure pick-up unit of heating that utilizes existing single-phase 115V power supply and single load also can realize large tracts of land windshield control enclosure detection requirement.
Technical solution of the present invention is: a kind of control enclosure pick-up unit of heating of aircraft windshield, it comprises AC signal module, direct current display module, resistance modular converter, connects output module, wherein, be used for to give AC signal module that the control enclosure of heating provides three-phase current signal, be used for to the control enclosure of heating provide direct current signal the direct current display module, be used for providing the resistance modular converter of resistance signal separate to the glass control enclosure of heating, and respectively be used for providing the output module that is connected of output signal to link to each other for the control enclosure of heating.
Described AC signal module comprises left three-phase alternating current mutual inductor, right three-phase alternating current mutual inductor, switch, external load, wherein, single-phase 115V AC power live wire links to each other with the movable end of switch, the left and right sides switch terminal of switch links to each other with left and right three-phase alternating current mutual inductor input end respectively, simultaneously, the output termination external load of left and right three-phase alternating current mutual inductor.
Single-phase 115V AC power live wire penetrates from c hole one end of three-phase alternating current mutual inductor, pass from the other end in c hole, and then around penetrating the b hole to the direction that penetrates with the c hole, pass from the other end in b hole, again around penetrating a hole to the direction that penetrates with the b hole, the other end from a hole passes again, and then is connected with single external load one end, and the other end of external load is connected with single-phase 115V zero line.
Described external load is slide bar resistance.
Be connected with the load current table between external load and the 115V zero line.
Be provided with fuse between the movable end of single-phase 115V AC power and switch.
The advantage that the present invention has and beneficial effect: the present invention uses single-phase 115V power supply to substitute three-phase 115V power supply, and use single slide bar resistance to substitute three pull-up resistors, effectively simplified testing circuit, reduced the cost of manufacture of pick-up unit, made the easier realization of testing and safe and reliable.
Description of drawings
Fig. 1 is that a kind of prior art three-phase 115V power supply is to the power supply the principle figure of the control enclosure test of heating;
Fig. 2 is the theory diagram of the control enclosure pick-up unit of heating of aircraft windshield of the present invention;
Fig. 3 is the schematic diagram of AC signal module.
Wherein, 1-AC signal module, 2-direct current display module, 3-resistance modular converter, 4-connect output module, 5-external load, the right three-phase alternating current mutual inductor of 6-, 7-load current table, 8-left side three-phase alternating current mutual inductor, the single-phase 115V output plug of 9-, 10-left and right sides switch, 11-fuse.
Embodiment
The present invention is described further below by specific embodiment:
See also Fig. 2, it is the theory diagram of the control enclosure pick-up unit of heating of aircraft windshield of the present invention.The control enclosure pick-up unit of heating of aircraft windshield of the present invention comprises AC signal module 1, direct current display module 2, resistance modular converter 3, connects output module 4.Wherein, AC signal module 1, direct current display module 2, resistance modular converter 3 are separate, and respectively be connected output module 4 and link to each other.The AC signal module provides three-phase current signal for the control enclosure of heating to glass, the direct current display module provides direct current signal for the control enclosure of heating to glass, the resistance modular converter provides resistance signal for the control enclosure of heating to glass, and connecting output module provides output signal for the control enclosure of heating to glass.
Consult Fig. 3, it is the circuit diagram of AC signal module.Described AC signal module comprises external load 5, right three-phase alternating current mutual inductor 6, load current table 7, left three-phase alternating current mutual inductor 8, single-phase 115V output plug 9, left and right sides switch 10, fuse 11.Wherein, the live wire of 115V links to each other by the movable end of fuse with left and right sides switch, and the left and right sides switch terminal of left and right sides switch links to each other with left and right three-phase alternating current mutual inductor input end respectively.Simultaneously, the output termination external load of left and right three-phase alternating current mutual inductor is connected with the load current table between external load and the 115V zero line.
During actual the use, single-phase 115V AC power live wire penetrates from c hole one end of three-phase alternating current mutual inductor, pass from the other end in c hole, and then around penetrating the b hole to the direction that penetrates with the c hole, pass from the other end in b hole, around penetrating a hole to the direction that penetrates with the b hole, the other end from a hole passes again again, and then be connected with single external load one end, the other end of external load is connected with single-phase 115V zero line.The three-phase alternating current mutual inductor can be experienced three-phase current signal like this.
This external load is selected the slide bar resistance of 1 9.9A for use in addition, when slide bar resistance is adjusted to load current demonstration 3A, can check the heat temperature control of heating a little less than control enclosure is realized of windshield, when slide bar resistance is adjusted to load current and shown 9A, can realize forcing Wen Wendu control and check the windshield control enclosure of heating.
Provide the heat process of the test of control enclosure pick-up unit of XJW-1 glass of the present invention below.
A is from seizure test
1 provides to exerciser and to exchange 400Hz 115V and direct current 28V power supply, and call through test device " power supply " switch makes voltage table indication 28V.
2 transfer to 3450 Ω with standard resistance box, " about conversion ", " passage conversion ", " conversion of heating " switch on the exerciser are put " left side ", " active and standby conversion " switch is put " main using " position, " strong and weak conversion " switch is put " by force " position, " self check 1 " on the control enclosure dialled upward, then control enclosure give successively in about 10s that left glass stops to heat, heats, short trouble, four kinds of cycle of states of open circuit fault once, carry out the heat left road self check of control enclosure of XJW-1 glass.In like manner each switch is placed " right side " position, " self check 2 " on the control enclosure dialled upward, then can carry out the heat right wing self check of control enclosure of XJW-1 glass.
After the b self check is finished, can carry out the inspection of sensor translation function respectively, force the inspection of temperature control temperature, a little less than add the inspection of temperature control temperature, trouble shooting, introduce specific operation process that each checks below respectively.
1 sensor translation function checks
1.1 " conversion 1 " switch on the control enclosure is dialled upward, exerciser " active and standby conversion " switch is put " standby " position, " heating in a left side " lamp is bright for normal on the exerciser at this moment.
1.2 " about conversion ", " passage conversion ", " conversion of heating " switch on the exerciser are put " right side " position, and " conversion 2 " switch on the control enclosure is dialled upward, on this moment exerciser " heating in the right side " lamp bright be normally.
2 force the inspection of temperature control temperature
2.1 reduce the resistance box resistance, go out until exerciser " heating in a left side " lamp, record this resistance and be left passage disconnect the resistance of forcing temperature should be at 2016 Ω~2472 Ω.
2.2 increase the resistance box resistance again, bright until exerciser " heating in a left side " lamp, record this resistance and be left passage connect the resistance of forcing temperature should be at 2942 Ω ± 90 Ω.
2.3 " about conversion ", " passage conversion ", " conversion of heating " switch on the exerciser are put " right side ", reduce the resistance box resistance, go out until exerciser " heating in the right side " lamp, record this resistance and be right passage disconnect the resistance of forcing temperature should be at 2016 Ω~2472 Ω.
2.4 increase the resistance box resistance again, bright until exerciser " heating in the right side " lamp, record this resistance and be right passage connect the resistance of forcing temperature should be at 2942 Ω ± 90 Ω.
Add the inspection of temperature control temperature a little less than in the of 3
3.1 " strong and weak conversion " switch on the exerciser is put " weak " position, reduce the resistance box resistance, " heating in the right side " lamp goes out on exerciser, and recording this resistance is that the resistance of heating a little less than right passage disconnects should be at 2016 Ω~2472 Ω.
3.2 increase the resistance box resistance again, " heating in the right side " lamp is bright on exerciser, recording this resistance is that the resistance of heating a little less than right passage is connected should be at 2942 Ω ± 90 Ω.
3.3 " about conversion ", " passage conversion ", " conversion of heating " switch on the exerciser are put " left side ", reduce the resistance box resistance, " heating in a left side " lamp goes out on exerciser, and recording this resistance is that the resistance of heating a little less than left passage disconnects should be at 2016 Ω~2472 Ω.
3.4 increase the resistance box resistance again, " heating in a left side " lamp is bright on exerciser, recording this resistance is that the resistance of heating a little less than left passage is connected should be at 2942 Ω ± 90 Ω.
4 trouble shootings
4.1 short circuit sensor, testing for continuity
4.1.1 the resistance box resistance is adjusted to 0 Ω, and " heating in a left side " lamp goes out on this moment exerciser, " left fault " lamp bright (on the control enclosure left side " short circuit " lamp bright) is for normal." about conversion ", " passage conversion ", " conversion of heating " switch on the exerciser are put " right side " position, and " heating in the right side " lamp goes out on this moment exerciser, " right fault " lamp bright (right " short circuit " lamp is bright on the control enclosure) is normally.
Make on the exerciser " heating in the right side " lamp bright 4.1.2 increase resistance, with disengagement of resistance box connecting line, " heating in the right side " lamp goes out on this moment exerciser, " right fault " lamp bright (right " opening circuit " lamp is bright on the control enclosure) is for normal." about conversion ", " passage conversion ", " conversion of heating " switch on the exerciser are put " left side ", adjusting resistance makes " heating in a left side " lamp bright, throw off connecting line of resistance box, " heating in a left side " lamp goes out at this moment, " left fault " lamp bright (left side " opening circuit " lamp is bright on the control enclosure) is for normal.
4.2 there is not the galvanoscopy of heating when heating
4.2.1 " conversion of heating " switch on the exerciser is put the neutral position, and " heating in a left side ", " left fault " lamp bright (left side " no current " lamp is bright on the control enclosure) are for normal at this moment.
4.2.2 " about conversion ", " passage conversion " switch on the exerciser are put " right side " position, and " heating in the right side ", " right fault " lamp bright (right " no current " lamp is bright on the control enclosure) are for normally at this moment.
The current failure inspection 4.3 heat when not heating
4.3.1 " conversion of heating " switch on the exerciser is put " right side " position, adjusting resistance box goes out " heating in the right side " lamp, " false current " switch is put " right side " position, and " heating in the right side ", " right fault " lamp bright (right " false current " lamp is bright on the control enclosure) are for normal at this moment.
4.3.2 " about conversion ", " passage conversion ", " conversion of heating " switch on the exerciser are put " left side ", adjusting resistance box goes out " heating in a left side " lamp, " false current " switch is put " left side " position, and " heating in a left side ", " left fault " lamp bright (left side " false current " lamp is bright on the control enclosure) are for normal at this moment.
In sum, the present invention uses single-phase 115V power supply to substitute three-phase 115V power supply, and uses single slide bar resistance to substitute three pull-up resistors, effectively simplify testing circuit, reduced the cost of manufacture of pick-up unit, and easy to operate, safe and reliable, make the easier realization of testing.

Claims (6)

1. the control enclosure pick-up unit of heating of an aircraft windshield, it is characterized in that: comprise AC signal module, direct current display module, resistance modular converter, connect output module, wherein, be used for to give AC signal module that the control enclosure of heating provides three-phase current signal, be used for to the control enclosure of heating provide direct current signal the direct current display module, be used for providing the resistance modular converter of resistance signal separate to the glass control enclosure of heating, and respectively be used for providing the output module that is connected of output signal to link to each other for the control enclosure of heating.
2. the control enclosure pick-up unit of heating of aircraft windshield according to claim 1, it is characterized in that: described AC signal module comprises left three-phase alternating current mutual inductor, right three-phase alternating current mutual inductor, switch, external load, wherein, the live wire of 115V links to each other with the movable end of switch, the left and right sides switch terminal of switch links to each other with left and right three-phase alternating current mutual inductor input end respectively, simultaneously, the output termination external load of left and right three-phase alternating current mutual inductor.
3. the control enclosure pick-up unit of heating of aircraft windshield according to claim 2, it is characterized in that: single-phase 115V AC power live wire penetrates from c hole one end of three-phase alternating current mutual inductor, pass from the other end in c hole, and then around penetrating the b hole to the direction that penetrates with the c hole, pass from the other end in b hole, around penetrating a hole to the direction that penetrates with the b hole, the other end from a hole passes again again, and then be connected with single external load one end, the other end of external load is connected with single-phase 115V zero line.
4. the control enclosure pick-up unit of heating of aircraft windshield according to claim 3, it is characterized in that: described external load is slide bar resistance.
5. the control enclosure pick-up unit of heating of aircraft windshield according to claim 4 is characterized in that: be connected with the load current table between external load and the 115V zero line.
6. the control enclosure pick-up unit of heating of aircraft windshield according to claim 5 is characterized in that: be provided with fuse between the movable end of live wire and switch.
CN201210060893.XA 2012-03-09 2012-03-09 A kind of control enclosure pick-up unit of heating of airplane windscreen Active CN103309343B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201210060893.XA CN103309343B (en) 2012-03-09 2012-03-09 A kind of control enclosure pick-up unit of heating of airplane windscreen

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201210060893.XA CN103309343B (en) 2012-03-09 2012-03-09 A kind of control enclosure pick-up unit of heating of airplane windscreen

Publications (2)

Publication Number Publication Date
CN103309343A true CN103309343A (en) 2013-09-18
CN103309343B CN103309343B (en) 2016-04-06

Family

ID=49134668

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201210060893.XA Active CN103309343B (en) 2012-03-09 2012-03-09 A kind of control enclosure pick-up unit of heating of airplane windscreen

Country Status (1)

Country Link
CN (1) CN103309343B (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105301353A (en) * 2014-06-30 2016-02-03 中国南方航空工业(集团)有限公司 System and method for detecting control box of AC power supply system
CN107345991A (en) * 2016-05-06 2017-11-14 哈尔滨飞机工业集团有限责任公司 A kind of windscreen wiper systems modelling device
CN111770594A (en) * 2020-06-17 2020-10-13 陕西飞机工业(集团)有限公司 Portable multipurpose glass system of heating debugging circuit

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2006117137A1 (en) * 2005-04-29 2006-11-09 Paolo Tripodi Invisible system of antifogging and antifreezing for transparent and non transparent large surfaces

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2006117137A1 (en) * 2005-04-29 2006-11-09 Paolo Tripodi Invisible system of antifogging and antifreezing for transparent and non transparent large surfaces

Non-Patent Citations (3)

* Cited by examiner, † Cited by third party
Title
冯斌: "EMB145风挡加温故障的分析排除", 《江苏航空》, no. 1, 15 February 2011 (2011-02-15), pages 47 *
张小玉等: "基于单片机的机载测温系统自动检测仪设计", 《中国测试》, vol. 35, no. 6, 30 November 2009 (2009-11-30), pages 57 - 59 *
郝世勇等: "某型飞机温控盒综合试验器的研制", 《科技信息》, no. 11, 15 April 2011 (2011-04-15), pages 113 - 128 *

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105301353A (en) * 2014-06-30 2016-02-03 中国南方航空工业(集团)有限公司 System and method for detecting control box of AC power supply system
CN107345991A (en) * 2016-05-06 2017-11-14 哈尔滨飞机工业集团有限责任公司 A kind of windscreen wiper systems modelling device
CN111770594A (en) * 2020-06-17 2020-10-13 陕西飞机工业(集团)有限公司 Portable multipurpose glass system of heating debugging circuit

Also Published As

Publication number Publication date
CN103309343B (en) 2016-04-06

Similar Documents

Publication Publication Date Title
CN102072997B (en) Spare automatic switching logic test method for checking main transformer mutual switching mode
CN105572496B (en) Electric automobile high-voltage safety dynamic simulant test system
CN106371009A (en) Test device and test method of safety type relay
CN103022959A (en) Method and device for adhesion detection of main contact of alternating-current contactor
CN110456267A (en) The method of the reason of for determining voltage interruption, auxiliary unit and electric system
CN205229445U (en) Electric energy meter RS485 communication interface comprehensive properties test module
CN104979894A (en) RMU uninterrupted power supply load transfer method
CN105047036A (en) Virtual-real fusion rail transit vehicle whole-vehicle electrical practical training apparatus and method
CN103309343A (en) Heating control box detection device of airplane windshield
CN105761569A (en) 10Kv distribution transformer simulation system
CN103345870A (en) Transformer intelligent simulation device
CN107492684A (en) The battery management system and vehicle of electrokinetic cell
CN204452063U (en) Elec. vehicle fuse state testing circuit
CN203191519U (en) Device for testing alternating-current circuit breaker of aircraft
CN207946485U (en) Operation vehicle for contact wire's AC power distribution cabinet/AC distribution panel device for fast detecting
CN204719205U (en) Isolating switch time-parameters test simulator
CN102095951B (en) Spare power automatic switching logic test method for checking automatic switching mode of low-pressure side section switch
CN203838333U (en) On-site universal load tester for newly installed electric energy meters
CN205608133U (en) Phase to earth fault auxiliary detection device
CN201386894Y (en) Startup circuit for emergency DC oil pump in lubricant station
CN208314106U (en) A kind of high-voltage interlocking detection circuit
CN105572586A (en) Phase-precise-timing three-phase AC motor high-voltage safety dynamic simulation system
CN203909158U (en) Automatic checking device
CN204333937U (en) Detect the intellectualized detection device based on the intellectualized switchgear one-phase ground protection function of 10kV isolated neutral distribution network systems
CN202994950U (en) Leak current test instrument for three-phase equipment

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
C14 Grant of patent or utility model
GR01 Patent grant
CP03 Change of name, title or address

Address after: 723213 Liulin Town, Chenggu County, Hanzhong City, Shaanxi Province

Patentee after: Shaanxi Aircraft Industry Co.,Ltd.

Address before: Box 34, Hanzhong City, Shaanxi Province, 723213

Patentee before: Shaanxi Aircraft INDUSTRY(GROUP) Co.,Ltd.

CP03 Change of name, title or address