CN107878781A - A kind of vehicle-mounted power supply performs device for Aerospace vehicle test - Google Patents
A kind of vehicle-mounted power supply performs device for Aerospace vehicle test Download PDFInfo
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- CN107878781A CN107878781A CN201711046719.9A CN201711046719A CN107878781A CN 107878781 A CN107878781 A CN 107878781A CN 201711046719 A CN201711046719 A CN 201711046719A CN 107878781 A CN107878781 A CN 107878781A
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
- B64F5/60—Testing or inspecting aircraft components or systems
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- Engineering & Computer Science (AREA)
- Manufacturing & Machinery (AREA)
- Transportation (AREA)
- Aviation & Aerospace Engineering (AREA)
- Remote Monitoring And Control Of Power-Distribution Networks (AREA)
Abstract
The invention discloses a kind of vehicle-mounted power supply performs device for Aerospace vehicle test, and disclose a kind of aircraft integrated test system and its application method for including the vehicle-mounted power supply performs device.The vehicle-mounted power supply performs device of the present invention meets the requirement installed on equipment cart by the Curve guide impeller in structure；Reliably working under subzero 40 DEG C of temperature environments is realized by the adaptable device of Environment；Remote on-off function and emergency-off function are devised in terms of automatic test and emergency processing, and remote control is realized by Remote control interface；In power supply perform function, there are 16 passage double-pole power supply control abilities, the carrying current capacity of hilted broadsword is not less than 15A；In terms of state data acquisition, each on off state is exported by acquisition interface.
Description
Technical field
The present invention relates to vehicle technology field, and in particular to a kind of vehicle-mounted power supply for Aerospace vehicle test performs dress
Put.
Background technology
Aircraft needs to carry out a series of ground validation experiment before transmission, to allow flight in these ground experiments
Device startup optimization just must have power supply excitation.The mode for providing power supply excitation for aircraft typically has two kinds, and one kind is by flying
The row device battery of itself is directly powered for aircraft, and another kind is to be carried using ground power supply by land cable for aircraft
For power supply.In the ground experiment stage, the overwhelming majority is to use ground power supply power supply mode.
In the past, the use of ground power supply is the mode that was powered of aircraft, generally require by signal adaptation combination or
Power supply performs device is powered control and output control.The control mode combined using signal adaptation is typically no to shape of powering
State is monitored, for the aircraft with multiple-way supply demand, the power supply distribution capability deficiency of signal adaptation combination, and signal
Adapter combination major function is signal adaptation conditioning, and excessive subsidiary function makes its design cumbersome, is unfavorable for product versatility.
Existing power supply performs device has following defect in the application in Aerospace vehicle test field：Existing power supply performs
Device is typically placed on indoor use, and its environmental suitability is poor, is typically used in the test environment more than 0 DEG C, it is impossible to meet
Vehicle-mounted less than 0 DEG C of use environment requirement；Existing power supply performs device does not possess remote control power up function, it is necessary to personnel's hand
Dynamic start, is unfavorable for realizing remote control；Existing power supply performs device does not possess emergency power off function, is needed under emergency case
When wanting emergency power off, passage it can only power off one by one；It is existing in configuration aspects, it is necessary to which power supply performs device is arranged on equipment cart
The physical dimension of some power supply performs devices can not meet equipment installation requirement on equipment cart.
The content of the invention
In order to solve above technical problem existing for prior art, the present invention provides a kind of for the vehicle-mounted of Aerospace vehicle test
Power performs device, solve it is existing power supply performs device environmental suitability it is poor, do not possess remote on-off function and promptly break
Electricity Functional, it is unsatisfactory for the problem of vehicle-mounted use demand.
One aspect of the present invention provides a kind of vehicle-mounted power supply performs device for Aerospace vehicle test, and the vehicle-mounted power supply performs
Device includes：Cabinet 1, power control module 2, remote on-off module 3, emergency power off module 4, sampling module 5 and power supply mould
Block 6；
The cabinet 1 includes：Casing 1-1, front panel 1-2 and rear board 1-3；Front panel 1-2 and rear board the 1-3 peace
Dress is fixed on casing 1-1；
The power control module 2 includes：Magnetic latching relay 2-3, the logical button 2-1 of power supply, the disconnected button 2-2 of power supply, control
Interface 2-4, input interface 2-5 and output interface 2-6 processed；
The remote on-off module 3 includes：Switching on and shutting down relay 3-1, power on button 3-2, power-off button 3-3 and remote control
Interface 3-4；
The emergency power off module 4 includes：Electromagnetic relay 4-1, emergency power off button 4-2 and diode 4-3；
The sampling module 5, including：Sampling resistor 5-1 and Sampling Interface 5-2；
Wherein described power on button 3-2, power-off button 3-3, emergency power off button 4-2, the logical button 2-1 of power supply and power supply are disconnected
Button 2-2 is arranged on front panel 1-2；The input interface 2-5, output interface 2-6, control interface 2-4, Sampling Interface 5-2
It is arranged at Remote control interface 3-4 on rear board 1-3；Power interface 7 is additionally provided with the rear board 1-3；
The control anode of the magnetic latching relay 2-3 is connected with the output plus terminal of power module 6, controls open end and two
Pole pipe 4-3 anode connection；Control closed end and control open end are connected with control interface 2-4 respectively；In addition, control closed end
Logical button 2-1 is connected with powering, and control open end is connected with the disconnected button 2-2 that powers；Magnetic latching relay 2-3 switch contact is public
End connection input interface 2-5 altogether, switch contact normal-closed end connection output interface 2-6；
The control anode of the switching on and shutting down relay 3-1 is connected with the output plus terminal of power module 6, control negative terminal and control
Interface 2-4 and Remote control interface 3-4 connections, realize remote control switch machine relay 3-1 on and off, complete to described vehicle-mounted
The remote control of the startup and shutdown for performs device of powering；Switching on and shutting down relay 3-1 control negative terminal simultaneously with power on button 3-2
Connected with power-off button 3-3, realize the manual control of the startup and shutdown to the vehicle-mounted power supply performs device；
The common port of first switch of the electromagnetic relay 4-1 is connected with diode 4-3 negative terminal, first switch
Normal-closed end ground connection；Second switch common port be connected with the output plus terminal of power module 6, second switch normal-closed end and
Indicator lamp anode in emergency power off button 4-2 connects, the indicator lamp negativing ending grounding in emergency power off button 4-2；The electromagnetism
Relay 4-1 control anode is connected with the output plus terminal of power module 6, control negative terminal be connected with control interface 2-4, electromagnetism after
Electrical equipment 4-1 control negative terminal is connected with emergency power off button 4-2 simultaneously, is realized to the urgent disconnected of the vehicle-mounted power supply performs device
The manual control of Electricity Functional；
The magnetic latching relay 2-3, electromagnetic relay 4-1 and switching on and shutting down relay 3-1 are provided which that one group of switch is used for
State is sampled, and the common port of the switch is connected with the output plus terminal of power module 6, normal-closed end and the sampling resistor 5-1 of switch
One end connection, the sampling resistor 5-1 other end is connected with Sampling Interface 5-2；
The power interface 7 is connected with mains electricity input end of power module 6.
Preferably, the cabinet 1 is 19 inch standard cabinets, is highly 4U, depth is not more than 350mm.
Preferably, 16 power control modules 2 are provided with the cabinet 1.
Preferably, all components are low temperature resistant device.
Another aspect of the present invention also provides a kind of aircraft integrated test system for including above-mentioned vehicle-mounted power supply performs device,
The aircraft integrated test system includes equipment cart and test carriage, and the vehicle-mounted power supply performs device is arranged on equipment cart,
Characterized in that, the equipment cart is also equipped with：Observing and controlling combination and aircraft power supply, master control calculating is installed on test carriage
Machine and remote control device, are connected between equipment cart and test carriage by netting twine, and man-machine interaction is carried out using main control computer.
Further aspect of the present invention also provides the application method of above-mentioned aircraft integrated test system, comprises the following steps：
Before use, power interface 7 is connected with 220V mains supplies, input interface 2-5 and aircraft power supply are connected
Connect, output interface 2-6 is connected with aircraft, control interface 2-4 and Sampling Interface 5-2 are combined into connection with observing and controlling respectively, will
Remote control interface 3-4 is connected with remote control device；The 220V mains supplies are 220V power supplys used in common citizen.
In use, by main control computer, observing and controlling combination start, combine to send to vehicle-mounted power supply performs device using observing and controlling and open
Machine is instructed, and start-up command is delivered to control interface 2-4, and into remote on-off module 3, switching on and shutting down relay 3-1 closures are completed
Boot action；
Control aircraft power supply output voltage signal is combined using observing and controlling, voltage signal is delivered to input interface 2-5；
Being combined using observing and controlling to vehicle-mounted power supply performs device and send power supply output order, power supply output order is delivered to control interface 2-4,
Magnetic latching relay 2-3 closures are controlled, the input interface 2-5 voltage signals introduced are delivered to output interface 2-6, then be delivered to
On aircraft, power supply control is realized；
Combined using observing and controlling from Sampling Interface 5-2 and read power supply state and on-off state in real time；
In case of emergency case need to aircraft implement emergency power off, using observing and controlling combine to it is vehicle-mounted power supply performs device send out
Emergency power off is sent to instruct, emergency power off instruction is delivered to control interface 2-4, emergency power off module 4 is reached, by emergency power off module
4 all No. 16 magnetic latching relay 2-3 of control disconnect, and cut off the voltage signal of output, realize emergency power off control；
After use, with observing and controlling combine to it is vehicle-mounted power supply perform combination successively send power supply open command and shutdown refer to
Order, power supply open command are delivered to control interface 2-4, and control magnetic latching relay 2-3 disconnects, and realizes power-off control；Shutdown refers to
Order is delivered to control interface 2-4, and controlling switch machine relay 3-1 disconnects, and realizes power-off control；Power interface 7 will finally be pulled out
The power line being connected with 220V mains supplies；
Further, switching on and shutting down control function and emergency power off control function are summarized in Remote control interface 3-4, is filled with remote control
Connection is put, switching on and shutting down control is completed by remote control device and emergency power off controls, is backed up as function, when needing control manually
Use.
Beneficial effects of the present invention
The vehicle-mounted power supply performs device for Aerospace vehicle test of the present invention is met by the Curve guide impeller in structure
The requirement installed on equipment cart；All components that the present invention selects are low temperature resistant device, are realized in subzero 40 DEG C of temperature
The reliably working spent under environment；Remote on-off function and emergency-off work(are devised in terms of automatic test and emergency processing
Can, and remote control is realized by Remote control interface 3-4；In power supply perform function, by optimizing cabinet inside topology layout,
16 power control modules of reasonable Arrangement, realize with 16 passage double-pole power supply control abilities, the carrying current capacity of hilted broadsword
Not less than 15A；In terms of state data acquisition, each on off state is exported by Sampling Interface.
Brief description of the drawings
Fig. 1 is a kind of vehicle-mounted power supply performs device composition schematic diagram for Aerospace vehicle test of the invention；
Description of reference numerals：1. cabinet, 1-1. casings, 1-2. front panels, 1-3. rear boards, 2. power control modules, 2-
1. the logical button of power supply, the disconnected button of 2-2. power supplies, 2-3. magnetic latching relays, 2-4. control interfaces, 2-5. input interfaces, 2-6. are defeated
Outgoing interface, 3. remote on-off modules, 3-1. switching on and shutting down relays, 3-2. power on button, 3-3. power-off buttons, 3-4. far controls connect
Mouthful, 4. emergency power off modules, 4-1. electromagnetic relays, 4-2. emergency power off buttons, 4-3. diodes, 5. sampling modules, 5-1.
Sampling resistor, 5-2. Sampling Interfaces, 6. power modules, 7. power interfaces.
Embodiment
The present invention is specifically described below by embodiment, it is necessary to it is pointed out here that be that the present embodiment is served only for pair
The present invention is further described, it is impossible to is interpreted as limiting the scope of the invention, the person skilled in the art in the field can
Some nonessential modifications and adaptations are made with the content of the invention more than.In the case where not conflicting, the reality in the present invention
Applying the feature in example and embodiment can be mutually combined.
One aspect of the present invention provides a kind of vehicle-mounted power supply performs device for Aerospace vehicle test, and the vehicle-mounted power supply performs
Device includes：Cabinet 1, power control module 2, remote on-off module 3, emergency power off module 4, sampling module 5 and power supply mould
Block 6；
The cabinet 1 includes：Casing 1-1, front panel 1-2 and rear board 1-3；Front panel 1-2 and rear board the 1-3 peace
Dress is fixed on casing 1-1；In this preferred embodiment, cabinet 1 is 19 inch standard cabinets, is highly 4U, depth is not more than
350mm；The requirement assembled on equipment cart can be met.
The power control module 2 includes：The logical button 2-1 of power supply, the disconnected button 2-2 of power supply, magnetic latching relay 2-3, control
Interface 2-4, input interface 2-5 and output interface 2-6 processed；
The remote on-off module 3 includes：Switching on and shutting down relay 3-1, power on button 3-2, power-off button 3-3 and remote control
Interface 3-4；
The emergency power off module 4 includes：Electromagnetic relay 4-1, emergency power off button 4-2 and diode 4-3；
The sampling module 5, including：Sampling resistor 5-1 and Sampling Interface 5-2；
Wherein described power on button 3-2, power-off button 3-3, emergency power off button 4-2, the logical button 2-1 of power supply and power supply are disconnected
Button 2-2 is arranged on front panel 1-2；The input interface 2-5, output interface 2-6, control interface 2-4, Sampling Interface 5-2
It is arranged at Remote control interface 3-4 on rear board 1-3；Power interface 7 is additionally provided with the rear board 1-3；
The control anode of the magnetic latching relay 2-3 is connected with the output plus terminal of power module 6, controls open end and two
Pole pipe 4-3 anode connection；Control closed end and control open end are connected with control interface 2-4 respectively；In addition, control closed end
Logical button 2-1 is connected with powering, and control open end is connected with the disconnected button 2-2 that powers；Magnetic latching relay 2-3 switch contact is public
End connection input interface 2-5 altogether, normal-closed end connection output interface 2-6；
The control anode of the switching on and shutting down relay 3-1 is connected with the output plus terminal of power module 6, control negative terminal and control
Interface 2-4 and Remote control interface 3-4 connections, realize remote control switch machine relay 3-1 on and off, complete to described vehicle-mounted
The remote control of the startup and shutdown for performs device of powering；Switching on and shutting down relay 3-1 control negative terminal simultaneously with power on button 3-2
Connected with power-off button 3-3, realize the manual control of the startup and shutdown to the vehicle-mounted power supply performs device；
The common port of first switch of the electromagnetic relay 4-1 is connected with diode 4-3 negative terminal, first switch
Normal-closed end ground connection；Second switch common port be connected with the output plus terminal of power module 6, second switch normal-closed end and
Indicator lamp anode in emergency power off button 4-2 connects, the indicator lamp negativing ending grounding in emergency power off button 4-2；The electromagnetism
Relay 4-1 control anode is connected with the output plus terminal of power module 6, control negative terminal be connected with control interface 2-4, electromagnetism after
Electrical equipment 4-1 control negative terminal is connected with emergency power off button 4-2 simultaneously, is realized to the urgent disconnected of the vehicle-mounted power supply performs device
The manual control of Electricity Functional；
The magnetic latching relay 2-3, electromagnetic relay 4-1 and switching on and shutting down relay 3-1 are provided which that one group of switch is used for
State is sampled, and the common port of the switch is connected with the output plus terminal of power module 6, normal-closed end and the sampling resistor 5-1 of switch
One end connection, the sampling resistor 5-1 other end is connected with Sampling Interface 5-2；
The power interface 7 is connected with mains electricity input end of power module 6 by power line.
Preferably, the cabinet 1 is 19 inch standard cabinets, is highly 4U, depth is not more than 350mm.It can meet filling
The requirement assembled on standby car.
Preferably, 16 power control modules 2 are provided with the cabinet 1.Realize with the power supply control of 16 passage double-poles
Ability processed, the carrying current capacity of hilted broadsword are not less than 15A；Aircraft multiple-way supply demand can be met.
Preferably, above-mentioned all components use low temperature resistant device, can meet under subzero 40 DEG C of temperature environments can
By work.
Another aspect of the present invention also provides a kind of aircraft integrated test system for including above-mentioned vehicle-mounted power supply performs device,
The aircraft integrated test system includes equipment cart and test carriage, and the vehicle-mounted power supply performs device is arranged on equipment cart,
Characterized in that, the equipment cart is also equipped with：Observing and controlling combination and aircraft power supply, master control calculating is installed on test carriage
Machine and remote control device, are connected between equipment cart and test carriage by netting twine, and man-machine interaction is carried out using main control computer.
Further aspect of the present invention also provides the application method of above-mentioned aircraft integrated test system, comprises the following steps：
Before use, power interface 7 is connected with 220V power supplys, it is powered for vehicle-mounted power supply performs device；Input is connect
Mouth 2-5 is connected with aircraft power supply, and output interface 2-6 is connected with aircraft, is powered for aircraft；Control is connect
Mouth 2-4 and Sampling Interface 5-2 combines connection with observing and controlling respectively, and Remote control interface 3-4 is connected with remote control device；
In use, by main control computer, observing and controlling combination start, combine to send to vehicle-mounted power supply performs device using observing and controlling and open
Machine is instructed, and start-up command is delivered to control interface 2-4, and into remote on-off module 3, switching on and shutting down relay 3-1 closures are completed
Boot action；
Control aircraft power supply output voltage signal is combined using observing and controlling, voltage signal is delivered to input interface 2-5；
Being combined using observing and controlling to vehicle-mounted power supply performs device and send power supply output order, power supply output order is delivered to control interface 2-4,
Magnetic latching relay 2-3 closures are controlled, the input interface 2-5 voltage signals introduced are delivered to output interface 2-6, then be delivered to
On aircraft, power supply control is realized；
Combined using observing and controlling from Sampling Interface 5-2 and read power supply state and on-off state in real time；
In case of emergency case need to aircraft implement emergency power off, using observing and controlling combine to it is vehicle-mounted power supply performs device send out
Emergency power off is sent to instruct, emergency power off instruction is delivered to control interface 2-4, emergency power off module 4 is reached, by emergency power off module
4 all magnetic latching relay 2-3 of control disconnect, and cut off the voltage signal of output, realize emergency power off control；
After use, with observing and controlling combine to it is vehicle-mounted power supply perform combination successively send power supply open command and shutdown refer to
Order, power supply open command are delivered to control interface 2-4, and control magnetic latching relay 2-3 disconnects, and realizes power-off control；Finally will
Observing and controlling combination shutdown；
Switching on and shutting down control function and emergency power off control function are summarized in Remote control interface 3-4, is connected with remote control device, is led to
Cross remote control device and complete switching on and shutting down control and emergency power off control, backed up as function, used when needing control manually.
Obviously, described embodiment is only part of the embodiment of the present invention, rather than whole embodiments.Based on this
Embodiment in invention, the every other reality that those of ordinary skill in the art are obtained under the premise of creative work is not made
Example is applied, belongs to the scope of the present invention.
Claims (7)
- A kind of 1. vehicle-mounted power supply performs device for Aerospace vehicle test, it is characterised in that the vehicle-mounted power supply performs device bag Include：Cabinet, power control module, remote on-off module, emergency power off module, sampling module and power module；The cabinet includes：Casing, front panel and rear board；The front panel and rear board are fixed on casing；The power control module includes：Magnetic latching relay, the logical button of power supply, the disconnected button of power supply, control interface, input interface And output interface；The remote on-off module includes：Switching on and shutting down relay, power on button, power-off button and Remote control interface；The emergency power off module includes：Electromagnetic relay, emergency power off button and diode；The sampling module, including：Sampling resistor and Sampling Interface；Wherein described power on button, power-off button, emergency power off button, the logical button of power supply and the disconnected button of power supply are arranged at front panel On；The input interface, output interface, control interface, Sampling Interface and Remote control interface are arranged on rear board；The rear board On be additionally provided with power interface；The control anode of the magnetic latching relay and the output plus terminal of power module connect, and are controlling open end and diode just End connection；Control closed end and control open end are connected with control interface respectively；In addition, control closed end connects with the logical button of power supply Connect, control open end and the disconnected button connects of power supply；The switch contact common port connection input interface of magnetic latching relay, normal-closed end Connect output interface；The control anode of the switching on and shutting down relay and the output plus terminal of power module connect, control negative terminal and control interface and Remote control interface connects, and realizes the on and off of remote control switch machine relay, completes to open the vehicle-mounted power supply performs device Machine and the remote control of shutdown；The control negative terminal of switching on and shutting down relay is connected with power on button and power-off button simultaneously, realization pair The manual control of the startup and shutdown of the vehicle-mounted power supply performs device；The common port of first switch and the negative terminal of diode of the electromagnetic relay connect, the normally closed termination of first switch Ground；The output plus terminal connection of the common port and power module of second switch, the normal-closed end of second switch are pressed with emergency power off Indicator lamp anode in button connects, the indicator lamp negativing ending grounding in emergency power off button；The control anode of the electromagnetic relay Be connected with the output plus terminal of power module, control negative terminal is connected with control interface, the control negative terminal of electromagnetic relay at the same with it is tight Anxious cut-off button connection, realize the manual control of the emergency power off function to the vehicle-mounted power supply performs device；The magnetic latching relay, electromagnetic relay and switching on and shutting down relay are provided which that one group of switch samples for state, described The common port of switch and the output plus terminal of power module connect, and the normal-closed end of switch and one end of sampling resistor connect, sampling electricity The other end of resistance is connected with Sampling Interface；The mains electricity input end son connection of the power interface and power module.
- 2. vehicle-mounted power supply performs device according to claim 1, it is characterised in that the cabinet is 19 inch standard machines Case, it is highly 4U, depth is not more than 350mm.
- 3. vehicle-mounted power supply performs device according to claim 1, it is characterised in that 16 power supplies are provided with the cabinet Control module.
- 4. vehicle-mounted power supply performs device according to claim 1, it is characterised in that all components are low temperature resistant device Part.
- 5. a kind of aircraft integrated test system of the vehicle-mounted power supply performs device including described in claim 1, the aircraft Integrated test system includes equipment cart and test carriage, and the vehicle-mounted power supply performs device is arranged on equipment cart, it is characterised in that The equipment cart is also equipped with：Observing and controlling combination and aircraft power supply, main control computer is provided with test carriage and remote control fills Put, connected between equipment cart and test carriage by netting twine, man-machine interaction is carried out using main control computer.
- 6. the application method of aircraft integrated test system according to claim 5, it is characterised in that including following step Suddenly：Before use, power interface is connected with 220V power supplys, input interface is connected with aircraft power supply, by output interface It is connected with aircraft, control interface and Sampling Interface is combined into connection with observing and controlling respectively, Remote control interface is connected with remote control device；In use, by main control computer, observing and controlling combination start, combined to vehicle-mounted power supply performs device transmission start and referred to using observing and controlling Order, start-up command are delivered to control interface, and into remote on-off module, switching on and shutting down relay closure completes boot action；Control aircraft power supply output voltage signal is combined using observing and controlling, voltage signal is delivered to input interface；Use survey Control combination sends power supply output order to vehicle-mounted power supply performs device, and power supply output order is delivered to control interface, and control magnetic is protected Relay closure is held, the voltage signal that input interface introduces is delivered to output interface, then is delivered on aircraft, realizes power supply Control；Combined using observing and controlling from Sampling Interface and read power supply state and on-off state in real time；In case of emergency case needs to implement emergency power off to aircraft, combined using observing and controlling sent to vehicle-mounted power supply performs device it is tight Anxious cut-offing instruction, emergency power off instruction are delivered to control interface, reach emergency power off module, are controlled by emergency power off module all Magnetic latching relay disconnects, and cuts off the voltage signal of output, realizes emergency power off control；After use, combined with observing and controlling to vehicle-mounted power supply and perform combination transmission power supply open command and shutdown command successively, supplied Electrically disconnected instruction is delivered to control interface, and control magnetic latching relay disconnects, and realizes power-off control；Finally observing and controlling is combined and closed Machine.
- 7. application method according to claim 6, it is characterised in that summarized in Remote control interface switching on and shutting down control function and Emergency power off control function, is connected with remote control device, completes switching on and shutting down control by remote control device and emergency power off controls, as Function backs up, and is used when needing control manually.
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711046719.9A CN107878781B (en) | 2017-10-31 | 2017-10-31 | vehicle-mounted power supply execution device for aircraft test |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711046719.9A CN107878781B (en) | 2017-10-31 | 2017-10-31 | vehicle-mounted power supply execution device for aircraft test |
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| Publication Number | Publication Date |
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| CN107878781A true CN107878781A (en) | 2018-04-06 |
| CN107878781B CN107878781B (en) | 2019-12-06 |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4996520A (en) * | 1988-06-17 | 1991-02-26 | Williams Instruments, Inc. | Overvoltage detection test apparatus for military aircraft weapons systems |
| EP2573930A1 (en) * | 2010-05-20 | 2013-03-27 | Mitsubishi Heavy Industries, Ltd. | Current generation device |
| CN103592908A (en) * | 2013-10-16 | 2014-02-19 | 中国运载火箭技术研究院 | Air vehicle integrated testing system based on 1553B bus |
| CN106841853A (en) * | 2016-12-30 | 2017-06-13 | 北京航天易联科技发展有限公司 | A kind of Aerospace vehicle test system and Aerospace vehicle test method |
| FR3045837A1 (en) * | 2015-12-18 | 2017-06-23 | Aircelle Sa | TEST ASSEMBLY IN FLIGHT OF AN ELECTRONIC POWER CHAIN OF AN AIRCRAFT COMPONENT |
-
2017
- 2017-10-31 CN CN201711046719.9A patent/CN107878781B/en active Active
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4996520A (en) * | 1988-06-17 | 1991-02-26 | Williams Instruments, Inc. | Overvoltage detection test apparatus for military aircraft weapons systems |
| EP2573930A1 (en) * | 2010-05-20 | 2013-03-27 | Mitsubishi Heavy Industries, Ltd. | Current generation device |
| CN103592908A (en) * | 2013-10-16 | 2014-02-19 | 中国运载火箭技术研究院 | Air vehicle integrated testing system based on 1553B bus |
| FR3045837A1 (en) * | 2015-12-18 | 2017-06-23 | Aircelle Sa | TEST ASSEMBLY IN FLIGHT OF AN ELECTRONIC POWER CHAIN OF AN AIRCRAFT COMPONENT |
| CN106841853A (en) * | 2016-12-30 | 2017-06-13 | 北京航天易联科技发展有限公司 | A kind of Aerospace vehicle test system and Aerospace vehicle test method |
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| Publication number | Publication date |
|---|---|
| CN107878781B (en) | 2019-12-06 |
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