CN110211832A - A kind of disconnect switch suitable for flight simulation control - Google Patents

A kind of disconnect switch suitable for flight simulation control Download PDF

Info

Publication number
CN110211832A
CN110211832A CN201910512293.4A CN201910512293A CN110211832A CN 110211832 A CN110211832 A CN 110211832A CN 201910512293 A CN201910512293 A CN 201910512293A CN 110211832 A CN110211832 A CN 110211832A
Authority
CN
China
Prior art keywords
shell
button cap
simulation control
iron axis
flight simulation
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.)
Pending
Application number
CN201910512293.4A
Other languages
Chinese (zh)
Inventor
刘勇军
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.)
Chengdu Weihang Technology Co Ltd
Original Assignee
Chengdu Weihang Technology Co 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 Chengdu Weihang Technology Co Ltd filed Critical Chengdu Weihang Technology Co Ltd
Priority to CN201910512293.4A priority Critical patent/CN110211832A/en
Publication of CN110211832A publication Critical patent/CN110211832A/en
Pending legal-status Critical Current

Links

Classifications

    • GPHYSICS
    • G09EDUCATION; CRYPTOGRAPHY; DISPLAY; ADVERTISING; SEALS
    • G09BEDUCATIONAL OR DEMONSTRATION APPLIANCES; APPLIANCES FOR TEACHING, OR COMMUNICATING WITH, THE BLIND, DEAF OR MUTE; MODELS; PLANETARIA; GLOBES; MAPS; DIAGRAMS
    • G09B9/00Simulators for teaching or training purposes
    • G09B9/02Simulators for teaching or training purposes for teaching control of vehicles or other craft
    • G09B9/08Simulators for teaching or training purposes for teaching control of vehicles or other craft for teaching control of aircraft, e.g. Link trainer
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01HELECTRIC SWITCHES; RELAYS; SELECTORS; EMERGENCY PROTECTIVE DEVICES
    • H01H13/00Switches having rectilinearly-movable operating part or parts adapted for pushing or pulling in one direction only, e.g. push-button switch
    • H01H13/02Details
    • H01H13/12Movable parts; Contacts mounted thereon
    • H01H13/14Operating parts, e.g. push-button
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01HELECTRIC SWITCHES; RELAYS; SELECTORS; EMERGENCY PROTECTIVE DEVICES
    • H01H13/00Switches having rectilinearly-movable operating part or parts adapted for pushing or pulling in one direction only, e.g. push-button switch
    • H01H13/02Details
    • H01H13/12Movable parts; Contacts mounted thereon
    • H01H13/20Driving mechanisms
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01HELECTRIC SWITCHES; RELAYS; SELECTORS; EMERGENCY PROTECTIVE DEVICES
    • H01H3/00Mechanisms for operating contacts
    • H01H3/22Power arrangements internal to the switch for operating the driving mechanism
    • H01H3/28Power arrangements internal to the switch for operating the driving mechanism using electromagnet

Landscapes

  • Engineering & Computer Science (AREA)
  • Theoretical Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Business, Economics & Management (AREA)
  • Educational Administration (AREA)
  • Educational Technology (AREA)
  • General Physics & Mathematics (AREA)
  • Electromagnetism (AREA)
  • Manufacture Of Switches (AREA)

Abstract

The present invention discloses a kind of disconnect switch suitable for flight simulation control, including button cap, shell, spring, electromagnet coil, iron axis, magnet, signaling switch, pcb board assembly, button cap is inserted into shell, iron axis is connected with button cap by disposed thread, and spring is mounted on above iron axis, and both ends of the spring is contacted in button cap and shell, electromagnet coil is fixed inside the shell, iron axis is mounted in electromagnet coil, and magnet is fixed inside the shell, and signaling switch is welded on pcb board assembly.The present invention can simulate the working condition of true breaker on flight simulator, it may be implemented manually and automatically to control breaker closing and off-state, the present invention is using standarized component and traditional process for machining production, and structure simplifies, is easy to operate, manufacturing cost and difficulty are substantially reduced, and is very suitable to single-piece or mass production.

Description

A kind of disconnect switch suitable for flight simulation control
Technical field
Present invention relates particularly to a kind of disconnect switchs suitable for flight simulation control, belong to flight simulation technology field.
Background technique
It is increasing to the flight simulator demand of training pilot with opening gradually for national low latitude, but if Flight simulator is manufactured using actual airplane component, that will improve the manufacturing cost of flight simulator, and actual airplane is disconnected Way switch working method is that residual current generates magnetic field and heat deformation driving disconnect switch, with the electric drive of flight simulator It differs greatly, so can not be applied to above flight simulator.
Differed using the quantity of disconnect switch from dozens to hundreds of in modern actual airplane, thus be badly in need of occurring it is a kind of and Actual airplane operation control, the consistent flight simulation disconnect switch of apparent size, and to meet structure is simplified, manufacturing cost is low, It is required convenient for assembling and safeguarding etc..
Summary of the invention
In view of the above-mentioned deficiencies in the prior art, the present invention devises a kind of open circuit suitable for flight simulation control Switch, can simulate the disconnection and Operating In Persistent Current Mode state of true disconnect switch on flight simulator, and operating handle and Apparent size is consistent with actual airplane.
To achieve the goals above, the following technical scheme that the present invention uses:
A kind of disconnect switch suitable for flight simulation control, including button cap, shell, spring, electromagnet coil, iron axis, magnetic Iron, signaling switch, pcb board assembly, button cap are inserted into shell, and iron axis and button cap are linked by disposed thread, spring installation On iron axis, both ends of the spring is contacted in button cap and shell, and electromagnet coil is fixed inside the shell, and iron axis is mounted on electromagnet In coil, magnet is fixed inside the shell, and signaling switch is welded on pcb board assembly.
Further, there is step inside the electromagnet coil, be external screw thread on the left of the iron axis.
Further, there is through-hole among the magnet.
Further, pcb board assembly tail portion is welded with external tapping end.
Further, the electromagnet coil is connected with pcb board assembly using wire welding.
Further, the pcb board assembly is using screw connection in shell tail portion.
Due to the adoption of the above technical scheme, the invention has the advantages that: the present invention can simulate on flight simulator really The working condition of breaker may be implemented manually and automatically to control breaker closing and off-state, and the present invention uses standard portion Part and traditional process for machining production, and structure simplifies, is easy to operate, manufacturing cost and difficulty are substantially reduced, and is very suitable to Single-piece or mass production.
Detailed description of the invention
Attached drawing of the invention is constituted to be used to provide further understanding of the present invention, illustrative examples of the invention and its Explanation is used to explain the present invention, and is not constituted improper limitations of the present invention.
Fig. 1 is a kind of closed state of disconnect switch suitable for flight simulation control of the invention.
Fig. 2 is a kind of off-state of disconnect switch suitable for flight simulation control of the invention.
Description of symbols:
1- button cap, 2- shell, 3- spring, 4- electromagnet coil, 5- iron axis, 6- magnet, 7- signaling switch, 8-PCB plate are total At.
Specific embodiment
Present invention will be further explained below with reference to the attached drawings and examples, and the present invention is that embodiment includes but is not limited to Following implementation.
As shown in Figure 1, button cap 1 is pressed into shell 2 when the electromagnet coil 4 powers off, compressed spring 3 to deflation shape State, iron axis 5 and magnet 6 are attracted, while 5 tail portion of iron axis and signaling switch 7 contact.
As shown in Figure 2.When the electromagnet coil 4 is powered, 4 magnetic force of electromagnet coil overcomes 6 magnetic force of magnet to inhale iron axis 5 It closes, iron axis 5 drives button cap 1 to pop up, and spring 3 squeezes the pop-up of button cap 1 and remains off.
Wherein, there is step inside the electromagnet coil 4, the iron axis 5 can do limit left and right in electromagnet coil and move It is dynamic.
In addition, the electromagnet coil 4 is connected with pcb board assembly 8 using wire welding, and pcb board assembly 8 is external above The electronic signal transmission with flight simulator may be implemented in port.
As shown in Fig. 1 and figure two, when the electromagnet coil 4 powers off, button cap 1 is pressed into shell 2 manually, iron axis 5 Tail portion and signaling switch 7 contact, and send signal to simulator by the external-connected port of pcb board assembly 8.After simulator receives signal It can be required to be powered according to state of flight and electromagnet coil 4 is attracted iron axis 5 and button cap 1 is popped up disconnection, if electromagnet coil 4 remain powered on, then button cap 1 is always maintained at off-state.Simulator can require to keep disconnected according to state of flight after receiving signal Electricity, then iron axis 5 and magnet 6 will keep attracting state, if extracted manually to button cap 1, spring 3 applies bullet to button cap 1 Power remains off it, if manual slighter compress button cap 1, moves inside 1 compressed spring 3 of button cap, unclamps manually Key 1, then spring 3 squeezes the pop-up of button cap 1 and remains off.
The above description is only a preferred embodiment of the present invention, is not intended to limit the scope of the invention, all utilizations Equivalent structure made by description of the invention and accompanying drawing content or process transformation, or directly or indirectly it is used in other related skills Art field, it is included within the scope of the present invention.

Claims (6)

1. it is a kind of suitable for flight simulation control disconnect switch, it is characterised in that: button cap (1), shell (2), spring (3), Electromagnet coil (4), iron axis (5), magnet (6), signaling switch (7), pcb board assembly (8), the button cap (1) are inserted into shell (2) in, the state iron axis (5) is connected with button cap (1) by disposed thread, and the spring (3) is mounted on iron axis (5) Face, state spring (3) both ends are contacted in button cap (1) and shell (2), and the electromagnet coil (4) is fixed on shell (2) Interior, the iron axis (5) is mounted in electromagnet coil (4), and the magnet (6) is fixed in shell (2), the signaling switch (7) it is welded on pcb board assembly (8).
2. a kind of disconnect switch suitable for flight simulation control according to claim 1, it is characterised in that: the electromagnetism There is step inside iron coil (4), is external screw thread on the left of the iron axis (5).
3. a kind of disconnect switch suitable for flight simulation control according to claim 2, it is characterised in that: the magnet (6) intermediate to have through-hole.
4. a kind of disconnect switch suitable for flight simulation control according to claim 3, it is characterised in that: the PCB Plate assembly (8) tail portion is welded with external tapping end.
5. a kind of disconnect switch suitable for flight simulation control according to claim 4, it is characterised in that: the electromagnetism Iron coil (4) is connected with pcb board assembly (8) using wire welding.
6. a kind of disconnect switch suitable for flight simulation control according to claim 1, it is characterised in that: the PCB Plate assembly (8) is using screw connection in shell tail portion.
CN201910512293.4A 2019-06-13 2019-06-13 A kind of disconnect switch suitable for flight simulation control Pending CN110211832A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201910512293.4A CN110211832A (en) 2019-06-13 2019-06-13 A kind of disconnect switch suitable for flight simulation control

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201910512293.4A CN110211832A (en) 2019-06-13 2019-06-13 A kind of disconnect switch suitable for flight simulation control

Publications (1)

Publication Number Publication Date
CN110211832A true CN110211832A (en) 2019-09-06

Family

ID=67792681

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201910512293.4A Pending CN110211832A (en) 2019-06-13 2019-06-13 A kind of disconnect switch suitable for flight simulation control

Country Status (1)

Country Link
CN (1) CN110211832A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114373644A (en) * 2021-12-22 2022-04-19 姜文凤 Power supply circuit device of miniature universal machine tool

Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1499540A (en) * 2002-10-30 2004-05-26 株式会社日立制作所 Solenoid operator and solenoid-operated switching device and control device for electromagnet
CN2760735Y (en) * 2004-08-04 2006-02-22 陈晓鹏 Electromagnetism controlled lighting circuit switch
KR20120026735A (en) * 2010-09-10 2012-03-20 김경복 Electromagnetic contact magnet
CN204760255U (en) * 2015-07-28 2015-11-11 牛猛 Outage back automatic disconnection's switch
CN105826133A (en) * 2016-06-01 2016-08-03 宁波精业保管箱有限公司 Electromagnet on-off state detection device and detection method
CN106571252A (en) * 2016-10-18 2017-04-19 上海工程技术大学 Simulation circuit breaker of flight simulator
CN107345589A (en) * 2016-05-04 2017-11-14 魏立虎 A kind of step-less adjustment rotating shaft of touch-control Electromagnetic Control
CN208189442U (en) * 2018-05-22 2018-12-04 成都泛美视界科技有限公司 A kind of break protective switch suitable for flight simulator

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1499540A (en) * 2002-10-30 2004-05-26 株式会社日立制作所 Solenoid operator and solenoid-operated switching device and control device for electromagnet
CN2760735Y (en) * 2004-08-04 2006-02-22 陈晓鹏 Electromagnetism controlled lighting circuit switch
KR20120026735A (en) * 2010-09-10 2012-03-20 김경복 Electromagnetic contact magnet
CN204760255U (en) * 2015-07-28 2015-11-11 牛猛 Outage back automatic disconnection's switch
CN107345589A (en) * 2016-05-04 2017-11-14 魏立虎 A kind of step-less adjustment rotating shaft of touch-control Electromagnetic Control
CN105826133A (en) * 2016-06-01 2016-08-03 宁波精业保管箱有限公司 Electromagnet on-off state detection device and detection method
CN106571252A (en) * 2016-10-18 2017-04-19 上海工程技术大学 Simulation circuit breaker of flight simulator
CN208189442U (en) * 2018-05-22 2018-12-04 成都泛美视界科技有限公司 A kind of break protective switch suitable for flight simulator

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114373644A (en) * 2021-12-22 2022-04-19 姜文凤 Power supply circuit device of miniature universal machine tool

Similar Documents

Publication Publication Date Title
CN101083182A (en) Sealed type electromagnetic relays with manual test switch
CN102163519A (en) High-power automatic reset magnetic latching relay
CN109326483B (en) Alternating-current high-voltage SF6 circuit breaker and permanent magnet operating mechanism thereof
CN107039212B (en) A kind of electromagnetic relay
CN110211832A (en) A kind of disconnect switch suitable for flight simulation control
CN203013634U (en) Magnetic latching relay direct operated magnetic circuit structure
CN103500689B (en) A kind of electromagnetic structure of high power relay
CN100403475C (en) Electromagnetic relay with spring pushing structure
CN202259053U (en) Single-coil bi-stable permanent magnet mechanism
CN207038370U (en) A kind of coaxial electric mechanical switch of self-shield single-pole double-throw radio frequency
CN203491196U (en) Large-power DC contactor
CN208723236U (en) Patch board
CN205069539U (en) Communication circuit breaker of good reliability
CN202008963U (en) High-power automatic reset magnetic holding relay
CN202948872U (en) Vacuum circuit breaker
CN202940194U (en) High-voltage direct-current electromagnetic relay
CN204834384U (en) Operating mechanism and use locomotive of this operating mechanism
CN201282065Y (en) Permanent magnet AC vacuum contactor
CN206628422U (en) Small-sized energy-saving electromagnetic relay
CN211479948U (en) High-safety relay convenient for automatic production
CN202888070U (en) Low-middle pressure dual-pressure switch of automobile air conditioner
CN201773759U (en) High-voltage vacuum circuit breaker
CN2775823Y (en) Electromagnetic relay with spring push structure
CN201032620Y (en) Electromagnetic drive permanent-magnet holding mechanism
CN219267582U (en) Permanent magnet quick-release mechanism

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
WD01 Invention patent application deemed withdrawn after publication
WD01 Invention patent application deemed withdrawn after publication

Application publication date: 20190906