CN108536175B - A kind of flap configuration output mechanism angular adjustment apparatus - Google Patents
A kind of flap configuration output mechanism angular adjustment apparatus Download PDFInfo
- Publication number
- CN108536175B CN108536175B CN201710128925.8A CN201710128925A CN108536175B CN 108536175 B CN108536175 B CN 108536175B CN 201710128925 A CN201710128925 A CN 201710128925A CN 108536175 B CN108536175 B CN 108536175B
- Authority
- CN
- China
- Prior art keywords
- module
- output mechanism
- flap configuration
- configuration output
- power
- 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.)
- Active
Links
Classifications
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D3/00—Control of position or direction
- G05D3/12—Control of position or direction using feedback
Landscapes
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Engineering & Computer Science (AREA)
- Automation & Control Theory (AREA)
- Testing Electric Properties And Detecting Electric Faults (AREA)
Abstract
The invention belongs to aircraft the field of test technology, disclose a kind of flap configuration output mechanism angular adjustment apparatus.Can be applied to component assembling in Aircraft Production manufacturing process, the general assembly stage carries out ground electric position angle and mechanical angle to flap configuration output mechanism and is adjusted and detects, progress electric position angle and mechanical angle are adjusted and detect when can also be applied to disassembly of the aircraft in the use process of outfield, reinstalling flap configuration output mechanism.Since flap configuration output mechanism is the important component of aircraft flap extension and retraction system, aircraft flap extension and retraction system to take off, landing safety plays an important role, be the important system for ensureing flight safety.Electric position angle is carried out by using this kind of flap configuration output mechanism angular adjustment apparatus to be adjusted and detect with mechanical angle, it can guarantee the consistency of aircraft flap electric angle and mechanical angle, component assembling, general assembly debugging cycle are saved, and ensure that the safety of aircraft.
Description
Technical field
The invention belongs to aircraft the field of test technology, and in particular to a kind of aircraft flap position output mechanism angle adjustment dress
It sets.
Background technique
Flap configuration output mechanism is the functional component in wing flap control system, and effect in systems is controlled to wing flap
The electrical feedback signal of box offer left and right flap angle position.
All there is in aircraft outer wing and outer in the component assembling of Aircraft Production process, general assembly stage in flap configuration output mechanism
After the wing and the big component docking of central wing, the adjustment of left and right wing, electrical null position and the inconsistent phenomenon of mechanical zero angle are caused a large amount of
Human and material resources waste.And in such as 15 ° of wing flap folding and unfolding other angles, 25 °, 35 ° there is also electric position and mechanical angle are different
Cause phenomenon, it is difficult to adjust.
Summary of the invention
Goal of the invention:
In order to solve the above technical problems, the present invention propose it is a kind of can be in internal field, outfield to the flap configurations of multiple models
The device that output mechanism carries out electric position angle and mechanical angle is adjusted and detects.
Technical solution:
A kind of flap configuration output mechanism angular adjustment apparatus, it is characterised in that including power module, voltage detection module,
Resistance detection module, interface module, circuit protection module, selecting module, state display module;
The function of the power module is to the voltage detection module, resistance detection module, state display module, circuit
The power supply such as protective module and flap configuration output mechanism;
The voltage detection module, the module are realized and are carried out to flap configuration output mechanism by the way of voltage detecting
The adjustment of electric position and mechanical angle consistency;
The resistance detection module, which is realized by the way of resistance detection carries out electricity to flap configuration output mechanism
The adjustment of gas position and mechanical angle;
The interface module, including a test socket and a Sets of Measurement detection hole, test socket is used for and various wing flap
Output mechanism connection in position carries out angle adjustment, and gauge check hole with ohmmeter and voltmeter for connecting to ohmmeter and voltage
Table carries out measurement verification;
The circuit protection module includes FU1 and insurance FU2 of an insurance, carries out second class protection to circuit;
The selecting module, the electromagnetism of panel toggle switch and a two-way normally-open normally-close including single-pole double throw after
Electric appliance, for the conversion between the voltage detection module and resistance detection module;
The state display module, the power supply including a power supply indicator for the device are shown;
The input terminal of the power module is connect with 36V industrial power, and output end and the voltage detection module, resistance are examined
It surveys module, state display module, circuit protection module and flap configuration output mechanism to connect and power, the resistance detection module
One end connect the other end with the selecting module and connect with power module, and the flap configuration of the interface module and different model is defeated
Mechanism is connected out;The circuit protection module includes FU1 and insurance FU2 of an insurance, carries out second class protection, electricity to circuit
Road one end FU1 is connect with 36V power supply anode, and the other end is connected with the control switch of the power module for protection power source
Module;Insurance FU2 is connect with the output plus terminal of the power module, for protecting the state display module, voltage inspection
Survey module, resistance detection module and each model flap configuration output mechanism, the selecting module, the face including a single-pole double throw
The electromagnetic relay of plate toggle switch and a two-way normally-open normally-close, the panel end toggle switch OFF of single-pole double throw and direct current are steady
Voltage source connection, the end ON1 are connect with the interface module, and the end ON2 is connect with digital ohmmeter in the resistance detection module,
Described state display module one end is connect with the power module output plus terminal, and the other end is connect for being somebody's turn to do with power module negative terminal
The power supply of device is shown.
The power module includes a digital voltmeter, digital voltmeter PV1 power input and the power supply
The output end of module is in parallel, and PV1 signal inputs one end and connect with the relay KM1 normally opened contact k1 in the selecting module, separately
One end is connect with power module output negative terminal, and voltage value when for flap configuration output mechanism difference mechanical angle is surveyed
Amount;
The resistance detection module, including a digital ohmmeter;Digital ohmmeter PR1 power input anode and institute
Change-over switch S2 connection in selecting module is stated, negative terminal is connect with power module output negative terminal, and PR1 signal inputs one end and the choosing
It selects relay KM1 normally-closed contact b2 connection in module and is followed by power module negative terminal, signal inputs the other end and the selecting module
It after middle relay KM1 normally-closed contact b2 connection, is connect with test socket in interface module and gauge check hole, is used for flap configuration
Resistance measurement when output mechanism difference mechanical angle.
The interface module, including a test socket and a Sets of Measurement detection hole, interface module a-road-through cross multichannel inspection
It surveys contact pin to be connected with the flap configuration output mechanism of different model, another way is connected with one group of panel detection socket for measuring
Calibrating.
The state display module is using a power supply indicator.
The power module, including a 24V D.C. regulated power supply and power switch S1,24V a D.C. regulated power supply
It is the available 24V direct-current working volts of flap configuration output mechanism by the 36V electrotransformation of safety.
Beneficial effect
Compared with prior art, the beneficial effects of the present invention are: this flap configuration output mechanism angular adjustment apparatus, passes through
It is connect with industry security electricity consumption 36V AC power source, a complete test macro can be formed, it can be respectively to four kinds of wing flap positions
The electric position angle and mechanical location angle for setting output mechanism are adjusted by the different requirements of voltage or resistance and keep one
It causes.
Detailed description of the invention
Fig. 1 is this flap configuration output mechanism angular adjustment apparatus composition block diagram,
Fig. 2 is the schematic diagram of flap configuration output mechanism angular adjustment apparatus of the present invention.
Specific embodiment
This flap configuration output mechanism angular adjustment apparatus is that a 400mm × 250mm × 150mm is complete independent
Appearance uses TLE aluminum profile Portable cabinet, internal to be connected by operation display panel, 1 D.C. regulated power supply, 2 byproducts
Connect cable and 1 feed cable composition.Feed cable is connect with exchange 36V power supply, is realized and is powered to the safe 36V of exerciser.
D.C. regulated power supply is mounted on the bottom plate inside exerciser, and digital voltage is equipped on operation display panel
Table, power control switch, stirs change-over switch, indicator light, Insurance Block, test socket, power outlet, meter at digital ohmmeter
The components such as amount detection banana jack.When needing to carry out some flap configuration output mechanism angle adjustment or detection, by the flap
Connecting cable one end of wing position output mechanism is connect with the flap configuration output mechanism, and other end plug and flap configuration export
The test socket of mechanism angular adjustment apparatus connects, by manipulation power switch and change-over switch, by voltage or resistance realization pair
The adjustment of aircraft flap position output mechanism angle.This flap configuration output mechanism angular adjustment apparatus it is practical, be conducive to interior
Field, line.
Present invention is further described in detail with specific embodiment with reference to the accompanying drawing:
Exchange 36V anode is connect with insurance one end FU1, and negative terminal is connect with 24V D.C. regulated power supply input negative terminal;Insurance
The other end of FU1 is connect with power switch S1 movable end, and the power switch S1 other end and 24V D.C. regulated power supply input anode connect
It connects;Insurance one end FU2 is connect with D.C. regulated power supply 24V output plus terminal, the insurance FU2 other end and power supply indicator anode and S2
The connection of the end change-over switch OFF;Power supply indicator negative terminal is connect with D.C. regulated power supply 24V output negative terminal;S2 change-over switch ON1 with
The connection of the contact pin 1 of gauge check hole anode and test socket XP1, the binding post of S2 change-over switch ON2 and digital ohmmeter PR1
The other end of G connection, the coil of relay KM1 is connect with D.C. regulated power supply 24V output negative terminal;Digital ohmmeter PR1's
Binding post H is connect with D.C. regulated power supply 24V output negative terminal, and the one of the normally-closed contact b1 of the binding post E and relay KM1 of PR1
End connection, the other end of the normally-closed contact b1 of KM1 are connect with the contact pin 2 of gauge check hole negative terminal (2) and test socket XP1, PR1
Binding post F connect with one end of the normally-closed contact b2 of relay KM1, the other end and gauge check of the normally-closed contact b2 of KM1
The connection of the contact pin 3 of hole negative terminal (1) and test socket XP1;The post D of digital voltmeter PV1 and D.C. regulated power supply 24V are defeated
Anode connects out, and binding post C and D.C. regulated power supply 24V the output negative terminal of PV1 is connect, the binding post A and relay KM1 of PV1
Normally opened contact k1 one end connection, the other end of KM1 normally opened contact k1 and gauge check hole negative terminal (2) and test socket XP1
Contact pin 2 connect, the binding post B of PV1 connect with the contact pin 3 of gauge check hole negative terminal (1) and test socket XP1.
1,2 detailed description flap configuration output mechanism electric positions and the program of mechanical angle adjustment with reference to the accompanying drawing.
1 carries out zero-bit adjustment with resistance
1.1 when carrying out zero-bit adjustment with resistance, will test one end socket that cable indicates flap configuration output mechanism model
It is connect with flap configuration output mechanism plug, one end plug for indicating " 123 or bdf " and the test socket in the interface module
Connection.
1.2 connection 36V power supply lines.Switch S1 in the power module is closed, power supply indicator in state display module
Circular lamp Ying Liang on H1 Ying Liang, S1 switch;Panel toggle switch S2 in the selecting module is got into " resistance " position, it is described at this time
Digital ohmmeter should have instruction in resistance detection module.
1.3 adjustment flap configuration output mechanism electrical null positions, by flap configuration output mechanism by established procedure unlock after
Universal joint is rotated within the scope of ± 30 °, when digital ohmmeter is shown in the range of electrical null position in the resistance detection module
When interior, and observing red zero-bit groove should be in two white gauge mark middle position.After adjustment is qualified, remove " 123 or
The cable of the one end bdf ".
1.4, which will test cable, indicates the one end of " 456 or hBE " and connect with test socket in the interface module, observes institute
Digital ohmmeter in resistance detection module is stated to be shown in the range of electrical null position.
After 1.5 tests, panel toggle switch S2 in the selecting module is got into neutral position, disconnects the power module
Middle switch S1, removes all cables and power supply line.
2 electricity consumptions pressure carries out angle adjustment:
The adjustment of 2.1 zero-bit angles:
2.1.1 will test cable indicate flap configuration output mechanism model one end socket and flap configuration output mechanism insert
Seat connection, the one end for indicating " 123 or bdf " is connect with the test socket in the interface module.
2.1.2 connecting 36V power supply line.Switch S1 in the power module is closed, power supply instruction in state display module
Circular lamp Ying Liang on lamp H1 Ying Liang, S1 switch;Panel toggle switch S2 in the selecting module is got into " voltage " position, at this time institute
Instruction should be had by stating digital voltmeter in voltage detection module.
2.1.3 flap configuration output mechanism electrical null position is adjusted, after flap configuration output mechanism is unlocked by established procedure
Universal joint is rotated within the scope of ± 30 °, when digital voltmeter is shown in electrical null position in the electricity voltage detection module
When in range, and observing red zero-bit groove should be in two white gauge mark middle positions, i.e. stopping adjustment.Adjustment
Afterwards, the cable of the one end " 123 or bdf " is removed.
2.1.4 it will test cable and indicate the one end of " 456 or hBE " and connect with test socket in the interface module, observed
Digital voltmeter is shown in the range of electrical null position in the voltage detection module.
2.2 other angle adjustment.
2.2.1 2.1 are connect, the universal joint of swivel flap position output mechanism is continued, it can be to wing flap position by 2.1 methods
It sets output mechanism and carries out the electric position of different angles and the consistency adjustments of mechanical angle such as 15 °, 25 °, 35 °, 45 °.
2.2.2 after testing, panel toggle switch S2 in the selecting module is got into neutral position, disconnects the power supply mould
Switch S1 in block removes all cables and power supply line.
Claims (6)
1. a kind of flap configuration output mechanism angular adjustment apparatus, it is characterised in that including power module, voltage detection module, electricity
Hinder detection module, interface module, circuit protection module, selecting module, state display module;
The function of the power module is to the voltage detection module, resistance detection module, state display module, circuit protection
Module and the power supply of flap configuration output mechanism;
The voltage detection module, the module are realized and are carried out electrically to flap configuration output mechanism by the way of voltage detecting
The adjustment of position and mechanical angle consistency;
The resistance detection module, which is realized by the way of resistance detection carries out electrical position to flap configuration output mechanism
Set the adjustment with mechanical angle;
The interface module, including a test socket and a Sets of Measurement detection hole, test socket is used for and various flap configuration
Output mechanism connection carries out angle adjustment, gauge check hole for connect with ohmmeter and voltmeter to ohmmeter and voltmeter into
Row measurement verification;
The circuit protection module includes FU1 and insurance FU2 of an insurance, carries out second class protection to circuit;
The selecting module, the electromagnetism relay of panel toggle switch and a two-way normally-open normally-close including single-pole double throw
Device, for the conversion between the voltage detection module and resistance detection module;
Power supply of the state display module for the device is shown;
The input terminal of the power module is connect with 36V industrial power, output end and the voltage detection module, resistance detection mould
Block, state display module, circuit protection module and flap configuration output mechanism are connected and are powered, resistance detection module one end
It connect the other end with the selecting module to connect with power module, the flap configuration of the interface module and different model exports machine
Structure is connected;Insurance one end FU1 is connect with 36V power supply anode, and the control switch of the other end and the power module is mutually used in conjunction
In protection power source module;Insurance FU2 connect with the output plus terminal of the power module, for protect the state display module,
The voltage detection module, resistance detection module and each model flap configuration output mechanism, the selecting module, including a list
The electromagnetic relay of the panel toggle switch of dpdt double-pole double-throw (DPDT) and a two-way normally-open normally-close, the panel toggle switch OFF of single-pole double throw
End connect with D.C. regulated power supply, the end ON1 is connect with the interface module, the end ON2 with it is digital in the resistance detection module
Ohmmeter connection, described state display module one end are connect with the power module output plus terminal, and the other end and power module are negative
Power supply of the end connection for the device is shown.
2. flap configuration output mechanism angular adjustment apparatus as described in claim 1, it is characterised in that the power module packet
A digital voltmeter is included, digital voltmeter PV1 power input is in parallel with the output end of the power module, PV1 letter
Number input one end connect with the relay KM1 normally opened contact k1 in the selecting module, the other end and the power module output
Negative terminal connection, voltage value measurement when for flap configuration output mechanism difference mechanical angle.
3. flap configuration output mechanism angular adjustment apparatus as described in claim 1, it is characterised in that the resistance detection mould
Block, including a digital ohmmeter;Change-over switch S2 in digital ohmmeter PR1 power input anode and the selecting module
Connection, negative terminal are connect with power module output negative terminal, and PR1 signal inputs one end and relay KM1 in the selecting module is normally closed
B2 connection in contact is followed by power module negative terminal, and signal inputs relay KM1 normally-closed contact b2 in the other end and the selecting module
It after connection, is connect with test socket in interface module and gauge check hole, is used for flap configuration output mechanism difference mechanical angle
When resistance measurement.
4. flap configuration output mechanism angular adjustment apparatus as described in claim 1, it is characterised in that the interface module, packet
It includes a test socket and a Sets of Measurement detection hole, interface module a-road-through crosses the wing flap of multi-way detecting contact pin and different model
Position output mechanism is connected, and another way is connected with one group of panel detection socket for measurement verification.
5. flap configuration output mechanism angular adjustment apparatus as described in claim 1, it is characterised in that the status display mould
Block is using a power supply indicator.
6. the flap configuration output mechanism angular adjustment apparatus as described in claim 1-5 any one, it is characterised in that described
Power module, including a 24V D.C. regulated power supply and power switch S1,24V a D.C. regulated power supply are by the 36V electricity of safety
It is converted into the available 24V direct-current working volts of flap configuration output mechanism.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201710128925.8A CN108536175B (en) | 2017-03-06 | 2017-03-06 | A kind of flap configuration output mechanism angular adjustment apparatus |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201710128925.8A CN108536175B (en) | 2017-03-06 | 2017-03-06 | A kind of flap configuration output mechanism angular adjustment apparatus |
Publications (2)
Publication Number | Publication Date |
---|---|
CN108536175A CN108536175A (en) | 2018-09-14 |
CN108536175B true CN108536175B (en) | 2019-11-15 |
Family
ID=63489402
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201710128925.8A Active CN108536175B (en) | 2017-03-06 | 2017-03-06 | A kind of flap configuration output mechanism angular adjustment apparatus |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN108536175B (en) |
Citations (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH0463799A (en) * | 1990-07-04 | 1992-02-28 | Mitsubishi Heavy Ind Ltd | Airplane having flap |
JP3448240B2 (en) * | 1999-05-31 | 2003-09-22 | 三菱重工業株式会社 | Aircraft control system |
CN101321666A (en) * | 2005-12-06 | 2008-12-10 | 空中客车德国有限公司 | Device for error detection of adjustable flaps |
CN102099247A (en) * | 2008-07-14 | 2011-06-15 | 空中客车营运有限公司 | Aerodynamic flap and wing |
CN102209662A (en) * | 2008-11-10 | 2011-10-05 | 空中客车营运有限公司 | Vane having a regulating flap and a gap covering device and an adjusting mechanism for a gap covering device |
CN102717889A (en) * | 2012-06-01 | 2012-10-10 | 湖南山河科技股份有限公司 | Flap control method and device of light airplane |
CN102791574A (en) * | 2009-11-13 | 2012-11-21 | 空中客车运作有限责任公司 | Flap adjusting system of an aircraft with a regulating flap |
CN203053397U (en) * | 2012-11-16 | 2013-07-10 | 哈尔滨飞机工业集团有限责任公司 | Tab position meter tester |
CN103303463A (en) * | 2012-03-09 | 2013-09-18 | 陕西飞机工业(集团)有限公司 | Electrical control method and system for airplane flap |
CN104048874A (en) * | 2014-06-24 | 2014-09-17 | 西北工业大学 | Load follow-up loading system for plane flap reliability test |
CN104976981A (en) * | 2014-04-10 | 2015-10-14 | 哈尔滨飞机工业集团有限责任公司 | Flap position indicator verification system |
CN105091834A (en) * | 2014-05-07 | 2015-11-25 | 哈尔滨飞机工业集团有限责任公司 | Position indicator tester |
CN105691633A (en) * | 2014-11-28 | 2016-06-22 | 上海航空电器有限公司 | Flap zero-position self-adaptive recognition device |
-
2017
- 2017-03-06 CN CN201710128925.8A patent/CN108536175B/en active Active
Patent Citations (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH0463799A (en) * | 1990-07-04 | 1992-02-28 | Mitsubishi Heavy Ind Ltd | Airplane having flap |
JP3448240B2 (en) * | 1999-05-31 | 2003-09-22 | 三菱重工業株式会社 | Aircraft control system |
CN101321666A (en) * | 2005-12-06 | 2008-12-10 | 空中客车德国有限公司 | Device for error detection of adjustable flaps |
CN102099247A (en) * | 2008-07-14 | 2011-06-15 | 空中客车营运有限公司 | Aerodynamic flap and wing |
CN102209662A (en) * | 2008-11-10 | 2011-10-05 | 空中客车营运有限公司 | Vane having a regulating flap and a gap covering device and an adjusting mechanism for a gap covering device |
CN102791574A (en) * | 2009-11-13 | 2012-11-21 | 空中客车运作有限责任公司 | Flap adjusting system of an aircraft with a regulating flap |
CN103303463A (en) * | 2012-03-09 | 2013-09-18 | 陕西飞机工业(集团)有限公司 | Electrical control method and system for airplane flap |
CN102717889A (en) * | 2012-06-01 | 2012-10-10 | 湖南山河科技股份有限公司 | Flap control method and device of light airplane |
CN203053397U (en) * | 2012-11-16 | 2013-07-10 | 哈尔滨飞机工业集团有限责任公司 | Tab position meter tester |
CN104976981A (en) * | 2014-04-10 | 2015-10-14 | 哈尔滨飞机工业集团有限责任公司 | Flap position indicator verification system |
CN105091834A (en) * | 2014-05-07 | 2015-11-25 | 哈尔滨飞机工业集团有限责任公司 | Position indicator tester |
CN104048874A (en) * | 2014-06-24 | 2014-09-17 | 西北工业大学 | Load follow-up loading system for plane flap reliability test |
CN105691633A (en) * | 2014-11-28 | 2016-06-22 | 上海航空电器有限公司 | Flap zero-position self-adaptive recognition device |
Non-Patent Citations (1)
Title |
---|
襟翼位置指示器通用规范;谢春华等;《中国人民共和国航空行业标准》;20030925;第1-9页 * |
Also Published As
Publication number | Publication date |
---|---|
CN108536175A (en) | 2018-09-14 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN103440803B (en) | The authentic training system of 10kV power distribution equipment real voltage analog current closed loop | |
CN106708003B (en) | A kind of electric machine controller fault detection system and method | |
CN102901891B (en) | Flexible simulation test platform for electric power system transformer protection devices | |
CN207114725U (en) | Proximity switch control assembly testboard | |
CN106935089A (en) | Power information acquisition terminal installation training system and method | |
CN108777089A (en) | A kind of correct errors with wiring connects electric training system with the dress table of fabrication evaluation | |
CN208985418U (en) | Dress table connects electric Simulated training device | |
CN209417960U (en) | It corrects errors with wiring and connects electric actual training device with the dress table of fabrication evaluation | |
CN207742282U (en) | A kind of Portable mutual inductor polarity and measurent wiring differentiate wireless test instrument | |
CN108536175B (en) | A kind of flap configuration output mechanism angular adjustment apparatus | |
CN207908655U (en) | Power module testboard | |
CN207946485U (en) | Operation vehicle for contact wire's AC power distribution cabinet/AC distribution panel device for fast detecting | |
CN102854405A (en) | Safe and efficient high-voltage nuclear phasing method | |
CN203520719U (en) | 10kV power distribution unit actual voltage simulation current closed-loop all-real training system | |
CN211124488U (en) | Low-voltage centralized meter reading intelligent simulation device | |
CN108061867A (en) | Debugging and testing method of combined power supply monitoring unit | |
CN206292302U (en) | A kind of power rating tester exerciser | |
CN103869114A (en) | Manufacturing technology and device for high-voltage high-power adjustable simulative transformer substation | |
CN208488501U (en) | A kind of experimental rig for electromagnetic compatibility power supply line conducted susceptibility | |
CN108226773A (en) | The portable tester and test method of pantagraph current collector and its controller solenoid valve | |
CN106872810A (en) | A kind of distribution socket technical security detecting system | |
CN104345229B (en) | Steering wheel exerciser in parallel | |
CN105091677B (en) | Fault simulation device of safety initiation device | |
CN206058712U (en) | A kind of massive quantity power supply and measurement phase three-wire three measures instructional device of opposing electricity-stealing | |
CN202275125U (en) | Mobile comprehensive debugging cabinet for reactive compensation device |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PB01 | Publication | ||
PB01 | Publication | ||
SE01 | Entry into force of request for substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
GR01 | Patent grant | ||
GR01 | Patent grant | ||
CP03 | Change of name, title or address | ||
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. |