CN105529969B - A kind of circuit of double-direction control aircraft DC motor movement - Google Patents
A kind of circuit of double-direction control aircraft DC motor movement Download PDFInfo
- Publication number
- CN105529969B CN105529969B CN201410508443.1A CN201410508443A CN105529969B CN 105529969 B CN105529969 B CN 105529969B CN 201410508443 A CN201410508443 A CN 201410508443A CN 105529969 B CN105529969 B CN 105529969B
- Authority
- CN
- China
- Prior art keywords
- switch
- motor
- relay
- circuit
- automatic
- 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
Landscapes
- Control Of Direct Current Motors (AREA)
- Stopping Of Electric Motors (AREA)
Abstract
The invention belongs to aero dynamo control technology field, is related to the circuit that direct current generator motion on a kind of double-direction control aircraft is artificial and is combined automatically.The step of solution, is as follows：Automatic control relay is added in the circuit of conventional manual's double-direction control motor, realizes the function that automatic control motor is switched on or switched off；Meanwhile added in automatic control circuit and cancel automatic switch, realize that automatic function is cancelled in manual intervention.It is of the invention can be for double-direction control motor circuit increase automatic control function, while add manual cancellation's automatic function, guarantee motor can reliable and stable work as requested, and integrated level height is in light weight, and easy to implement, cost is low.
Description
Technical field
The invention belongs to aero dynamo control technology field, is related to a kind of electricity of double-direction control aircraft DC motor movement
Road.
Background technology
In general aircraft DC circuit for controlling motor, more using independent manual control and automatic control mode.People's industry control
Motor bidirectional-movement processed, require that the concern dynamics to motor is higher in certain circumstances, the notice for expending pilot is more.From
Dynamic controlled motor bidirectional-movement, can mitigate pilot's burden, and stable and clear and definite motor environment is possible, but to aircraft
May occur undesirable motor movement for upper part complex environment and the not high computer of maturity and move and it is expected electricity
Machine moves and no motion of situation.If not increasing additional circuit, under partial status, then pilot guidance motor fortune can be deprived
Dynamic authority.Therefore pilot can not be deprived by needing one kind to combine manual control and automatically control while automatically control aboard
The DC motor control circuit of authority.
In Patent No. ZL200920171677.6, the device of two-way control of direct current motor uses one kind side of operating with
Just the device for two-way control of direct current motor, including six layers of two grades of rotary switch and two travel switches, pass through circuit group
Connection is closed, realizes double-direction control motor movement, while realize travel limit.This circuit connection is simple, applies in part industry
Field is possible, but in aviation field, this rotary switch does not meet ergonomic, and pilot is difficult identification rotary switch
Direction and other functional requirements.
The content of the invention
The purpose of the present invention is：It is proposed a kind of circuit of double-direction control aircraft DC motor movement, realize manual control and
Integrated design is automatically controlled, automatic control function is cancelled in increase, there is provided the alternative of double-direction control aircrafts electric machinery, collects successfully
Can, weight and cost are reduced, mitigates the burden of pilot.
The technical scheme is that：Design is optimized to the circuit of two-way control of direct current motor motion, by motor people
Work controlling switch and computer controlled automatic are combined, meanwhile, increase manual cancellation's auto-switch function, realize direct current
Machine is artificial and automatically controls and can be automatically controlled taking human as cancellation.
A kind of circuit of double-direction control aircraft DC motor movement, including manual control switch, relay and cancellation are certainly
Dynamic switch, wherein, it is high-end that manual control switch inputs termination power output, and acquiescence output relay termination is high-end and relay control
The acquiescence input of system switch one, it is high-end and contact relay controlling switch two non-default defeated that another output termination motor closes input
Go out end, relay control switch two inputs termination power and exports high-end, the acquiescence output termination motor of relay control switch one
Opening input is high-end, and another output end of relay control switch one is connectionless, the acquiescence output end of relay control switch two
Connectionless, relay low side accesses the acquiescence output end for the automatic switch that disappears, and the input termination computer for cancelling automatic switch is automatic
The output end of logic switch is closed, another output end for cancelling automatic switch is connectionless.
It is an advantage of the invention that：For the circuit of double-direction control aircraft DC motor movement, manual control and automatic is realized
Integrated design is controlled, function is integrated with, reduces weight and cost, and easy to implement, wide adaptability, cost are low.
Brief description of the drawings
Fig. 1 is circuit diagram of the present invention.
Embodiment
The present invention is described in further details below.
In design actuator in the control circuit of direct current generator, consider manually to be switched off and on function, while consider certainly
It is dynamic to be switched off and on function, because working environment is complicated on aircraft, while to consider that the function of automatically cutting off can be cancelled.In synthesis
Functional requirement is stated, in the control circuit of its actuator motor, the circuit of such two-way control of direct current motor motion can be used.
As illustrated, a kind of circuit of double-direction control aircraft DC motor movement, wherein, 28VDC power supplys, export high termination
Stitch 1 and low side connect stitch 6；Computer closes logic switch automatically, there is logical bit NC and stitch 7, externally output termination stitch
2；Direct current generator, including its motor close and open input it is high-end connect stitch 3 and stitch 4 respectively, motor low side connects stitch 5, electricity
Touching switch meets vacant position CLOSE and OPEN to the machine both ends limit respectively in place；Stitch 5,6,7 is with all connecing power supply；
Controlled motor circuit, including manual control switch, relay and cancellation automatic switch, wherein, manual control is opened
Close input termination power and export high-end stitch 1, acquiescence output end stitch A contact relays are high-end and relay control switch one is given tacit consent to
Input, another output end stitch B connect motor close stance and input the non-default defeated of high-end stitch 3 and contact relay controlling switch two
Go out end, relay control switch two inputs termination power and exports high-end stitch 1, the acquiescence output termination of relay control switch one
Motor open position inputs high-end stitch 4, and another output end of relay control switch one is connectionless, relay control switch two
Acquiescence output end is connectionless, and relay low side accesses the acquiescence output end stitch C for the automatic switch that disappears, and cancels the input of automatic switch
Termination computer closes the output end stitch 2 of logic switch automatically, and another output end stitch D for cancelling automatic switch is connectionless.
When manual control switch is placed in B contact, 28V power supplys provide close stance to motor by stitch 3 and input high-end electricity
Source, stitch 5 provide power supply, motor movement to extreme position to motor so that and top closing circuit is disconnected to CLOSE positions, under
Side opens circuit and connected, and causes motor movement to closed position, to realize the function that motor is manually cut off so as to disconnect motor power；
When manual control switch is placed in A contacts, 28V power supplys are provided to motor by manual control switch A and stitch 4 and open electricity
Source is high-end, and stitch 5 provides to motor turns on the power ground, motor movement to opening extreme position so that top is closed circuit and connected
To CLOSE positions, lower section open circuit be disconnected to OPEN positions, so as to disconnect motor turn on the power it is high-end cause motor movement to opening
Position, realize the function that motor is manually connected；
When computer automatic cut-off switch, which is placed in, is spaced apart (NC), that is, when giving tacit consent to above-mentioned state, motor is in an open position
State；
When computer automatic cut-off switch, which is placed in stitch 7, to be grounded, then relay works, by controlling switch one and switch two
Control is to non-default output end, then 28V power supplys provide high-end, stitch 5 of closing power input by stitch 1 and stitch 3 to motor
To motor offer power supply, motor movement to closing extreme position so that top closes circuit and is disconnected to CLOSE positions, and lower section is beaten
Open circuit is switched to OPEN positions, causes motor movement to closed position, to realize that motor is cut automatically so as to disconnect motor closing power supply
Disconnected function；
When computer automatic cut-off switch, which is placed in stitch 7, to be grounded, after realizing the function that motor is automatically cut off, if manually
Pressing cancels automatic switch to output end D, then disconnects relay function, then two-way snap switch is back to acquiescence output end automatically,
Then 28V power supplys stitch 1 is switched on power by stitch A and stitch 4 to motor offer, and opening input is high-end, and stitch 5 gives motor to provide
Power supply, motor movement to opening extreme position so that top closes circuit and is switched to CLOSE positions, and lower section is opened circuit and disconnected
To OPEN positions, turn on the power high-end so that motor movement is to open position so as to disconnect motor, realize the function that motor is connected, after
And realize manual cancellation's motor function of automatically cutting off.
Claims (1)
1. a kind of circuit of double-direction control aircraft DC motor movement, it is characterized in that, including manual control switch, relay and
Cancel automatic switch, wherein, manual control switch input termination power output it is high-end, acquiescence output relay termination it is high-end and after
Electric control switch one gives tacit consent to input, and it is high-end and contact relay controlling switch two non-that another output termination motor closes input
Give tacit consent to output end, relay control switch two inputs termination power and exports high-end, the acquiescence output end of relay control switch one
Connect motor open input it is high-end, another output end of relay control switch one is connectionless, the acquiescence of relay control switch two
Output end is connectionless, and relay low side accesses the acquiescence output end for the automatic switch that disappears, and the input termination for cancelling automatic switch calculates
Machine closes the output end of logic switch automatically, cancels that another output end of automatic switch is connectionless, and computer closes logic automatically
The input of switch is spaced apart pass and earth terminal including acquiescence.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410508443.1A CN105529969B (en) | 2014-09-28 | 2014-09-28 | A kind of circuit of double-direction control aircraft DC motor movement |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410508443.1A CN105529969B (en) | 2014-09-28 | 2014-09-28 | A kind of circuit of double-direction control aircraft DC motor movement |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN105529969A CN105529969A (en) | 2016-04-27 |
| CN105529969B true CN105529969B (en) | 2018-03-02 |
Family
ID=55772009
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201410508443.1A Active CN105529969B (en) | 2014-09-28 | 2014-09-28 | A kind of circuit of double-direction control aircraft DC motor movement |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN105529969B (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106354074B (en) * | 2016-11-22 | 2018-11-16 | 天津航空机电有限公司 | A kind of two mode switch interlocking control circuit applied to aviation liquid cooling system |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1990300A (en) * | 2005-12-28 | 2007-07-04 | 比亚迪股份有限公司 | Electromobile chair controlling means |
| TW200908538A (en) * | 2007-08-15 | 2009-02-16 | Delta Electronics Inc | Fan system and motor control device |
| CN201393191Y (en) * | 2009-04-17 | 2010-01-27 | 刘珍 | Device for two-way control of direct current motor |
| CN202257178U (en) * | 2011-09-29 | 2012-05-30 | 深圳市芭田生态工程股份有限公司 | Automatic electric switch |
| CN103117690A (en) * | 2013-02-26 | 2013-05-22 | 贵阳冶金机电工艺有限公司 | Integrated control circuit for manual-automatic forward and reverse rotation of motor |
Family Cites Families (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP4290951B2 (en) * | 2002-09-20 | 2009-07-08 | 正一 大重 | Automotive information display device |
-
2014
- 2014-09-28 CN CN201410508443.1A patent/CN105529969B/en active Active
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1990300A (en) * | 2005-12-28 | 2007-07-04 | 比亚迪股份有限公司 | Electromobile chair controlling means |
| TW200908538A (en) * | 2007-08-15 | 2009-02-16 | Delta Electronics Inc | Fan system and motor control device |
| CN201393191Y (en) * | 2009-04-17 | 2010-01-27 | 刘珍 | Device for two-way control of direct current motor |
| CN202257178U (en) * | 2011-09-29 | 2012-05-30 | 深圳市芭田生态工程股份有限公司 | Automatic electric switch |
| CN103117690A (en) * | 2013-02-26 | 2013-05-22 | 贵阳冶金机电工艺有限公司 | Integrated control circuit for manual-automatic forward and reverse rotation of motor |
Also Published As
| Publication number | Publication date |
|---|---|
| CN105529969A (en) | 2016-04-27 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN106553552B (en) | City rail vehicle pantograph and pantagraph current collector switching control system and trailer system | |
| US8829707B2 (en) | Methods for aircraft emergency power management | |
| US7936084B2 (en) | System and method for electric power distribution inside an aircraft | |
| CN110450940B (en) | Aircraft elevator trim control circuit | |
| CN105905284B (en) | The anti-oscillator system of Nose Wheel Steering with middling speed deviation-correcting function | |
| CN105529969B (en) | A kind of circuit of double-direction control aircraft DC motor movement | |
| CN102854871A (en) | Bus control system and engineering machinery | |
| CN103578853A (en) | Automobile intelligent relay | |
| CN203951254U (en) | One comes off to power and disconnects control circuit | |
| US20150263651A1 (en) | Movable barrier operator with backup control module | |
| CN104494648A (en) | Multi-machine control system for switch machines | |
| EP2316735A1 (en) | Power distribution apparatus | |
| CN106005358B (en) | A kind of aircraft hatchcover interlocking control circuit | |
| US20170287652A1 (en) | Switching device with a modular auxiliary switching unit | |
| US9948110B2 (en) | Power distribution system | |
| US1995780A (en) | Automatic circuit-control apparatus | |
| CN112230537A (en) | Electromechanical integrated control system of unmanned aerial vehicle | |
| CN204492995U (en) | Under a kind of electric-control motor car, throttle determines rotating speed diverter switch control gear | |
| KR20180099970A (en) | Remote power reset circuit | |
| CN109989837B (en) | Double-remote throttle control device | |
| US10121620B2 (en) | Control unit and actuator with control unit | |
| CN104747299A (en) | Electronic-controlled engine under-vehicle accelerator constant-rotation-speed switching switch control device | |
| CN205130949U (en) | Guarantee controlling means of electric automobile safety traffic | |
| CN112895974B (en) | Method for increasing the reliability of an onboard battery system and corresponding operating method | |
| US11840151B2 (en) | Device for encapsulating and interrupting the power supply of a battery |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| GR01 | Patent grant | ||
| GR01 | Patent grant |