CN106571252A - Simulation circuit breaker of flight simulator - Google Patents
Simulation circuit breaker of flight simulator Download PDFInfo
- Publication number
- CN106571252A CN106571252A CN201610906352.2A CN201610906352A CN106571252A CN 106571252 A CN106571252 A CN 106571252A CN 201610906352 A CN201610906352 A CN 201610906352A CN 106571252 A CN106571252 A CN 106571252A
- Authority
- CN
- China
- Prior art keywords
- expansion link
- cavity
- electromagnet
- breaker
- emulation
- 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
Links
Classifications
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01H—ELECTRIC SWITCHES; RELAYS; SELECTORS; EMERGENCY PROTECTIVE DEVICES
- H01H3/00—Mechanisms for operating contacts
- H01H3/22—Power arrangements internal to the switch for operating the driving mechanism
- H01H3/28—Power arrangements internal to the switch for operating the driving mechanism using electromagnet
Abstract
The invention provides a simulation circuit breaker of a flight simulator. A hollow supporting frame is shaped like a Chinese character "ri" and comprises an upper cavity, an intermediate crossbeam and a lower cavity. A telescopic rod is vertically configured in the hollow supporting frame. The upper end of the telescopic rod is provided with a key cap which is exposed out of the upper part of the top part of the hollow supporting frame. The intermediate segment of the telescopic rod is provided with a stop block which is arranged in the upper cavity. A spring is arranged between the stop block and the intermediate crossbeam in a pressing way. The lower end of the telescopic rod is arranged in the lower cavity, and the end part is provided with a contact disc which can be magnetically adsorbed or the telescopic rod is provided with the lower end which can be magnetically adsorbed. An electromagnet is fixedly arranged in the lower cavity, and a controller controls power supply of the electromagnet. The manufacturing cost of the aircraft simulator can be greatly reduced so that the structure is simple, the size is small, installation and configuration on the aircraft simulator are facilitated, and the simulation circuit breaker can be used for different types of machines through simple modification.
Description
Technical field
The present invention relates to flight simulation, more particularly to a kind of emulation breaker of flight simulator.
Background technology
In recent years, air force is quickly equipped for new military secret, navigation market constantly expands, the demand to Aircraft Simulator
Also it is increasing.Aircraft Simulator wants true simulation aircraft true to nature, and aircraft circuit breaker is essential.Due to actual airplane tool
There are a thirty or forty at least, the huge breaker quantity of at most up to a hundred, and single true aircraft circuit breaker 800-2000 units/not
Deng expensive so that the cost of Aircraft Simulator remains high.
Also it is not available in the market simulating the emulation breaker that real aircraft circuit breaker is used, so developing a kind of
Imperative for Aircraft Simulator, low cost aircraft circuit breaker, it can substantially reduce the cost of Aircraft Simulator, letter
Change the production of Aircraft Simulator.
The content of the invention
The technical problem to be solved is the emulation breaker for providing a kind of flight simulator, and the device can
Preferably meet Aircraft Simulator and use needs, solve the problems, such as to lack the dedicated emulated breaker of Aircraft Simulator on market.
The present invention is achieved by the following technical solutions：
A kind of emulation breaker of flight simulator, it is characterised in that：
Hollow support frame is in " day " font, including upper strata cavity, intermediate transverse girder and lower floor's cavity,
A piece expansion link of vertical configuration in hollow support framework；
Expansion link upper end is provided with button cap, and button cap exposes to hollow support frame roof top；
Expansion link stage casing is provided with block, and block is located in the cavity of upper strata, and spring is press-fitted between block and intermediate transverse girder；
Expansion link lower end be located at lower floor's cavity in, end be provided with can by the contact disc of magnetic absorption, or, expansion link tool
Having can be by the lower end of magnetic absorption；
Fixed electromagnet in lower floor's cavity, controller controls the power supply of electromagnet.
Controller control electromagnet power on/off come make electromagnet produce magnetic：When the solenoid is energized, by manually to
Lower pressing keys cap, expansion link promotes contact disc attracting with electromagnet, the process of this process simulation aircraft circuit breaker adhesive；When
During controller control electromagnet power-off, expansion link under the action of the spring, drives contact disc to separate with electromagnet, this process mould
When plan aircraft is faulty, aircraft circuit breaker disconnection process.
Further, the spring can be the spring stack being sleeved on expansion link, or the dish being sleeved on expansion link
Shape reed, or the reed in anti-" V " font configuration.
Further, support frame top is installed with fairlead, and fairlead is located at button cap lower section, and expansion link is from leading
The activity in set is passed through, and the direction of motion that fairlead is used to limit expansion link can only be along expansion link axial direction.
Further, the block is set screw, and expansion link stage casing is thread segment, and set screw is tightened on thread segment
On, can relative telescopic bar it is in rotary moving up and down, the initial deformation amount of spring is adjusted by set screw, to simulate different machines
The aircraft circuit breaker of type.
Further, the section of the intermediate transverse girder is L-shaped, and its bottom crosspiece vertically opens up through hole, and spring is press-fitted to
Between bottom crosspiece and set screw；The perpendicular section in its top is supported with playing a part of auxiliary stopper near spring with stable.
Further, in cylinder, contact disc is the disk with electromagnet concentric arrangement to the electromagnet, the disk of contact disc
Face outer rim is located at electromagnet upper surface outer rim outside, to ensure that contact disc is contacted fully with electromagnet.
Further, the intermediate transverse girder is arranged in the elongated vertically-mounted groove of support frame both sides by bolt, is led to
Crossing the height and position of adjustment intermediate transverse girder can change the size of upper strata cavity and lower floor's cavity, to simulate different type of machines
Aircraft circuit breaker stroke feel.
The beneficial effects of the present invention is：
1st, there is thirty or forty at least, the huge breaker quantity of at most up to a hundred, true aviation in view of actual airplane
Yuan/of breaker 800～2000, this Aircraft Simulator definite purpose circuit breaker price less than 100 yuan, the big reduction of this device
The manufacturing cost of Aircraft Simulator；
2nd, true aircraft circuit breaker complex structure, size is larger, and this Aircraft Simulator definite purpose circuit breaker is ensureing simulation very
Simple structure on the premise of solidity, size is less, is easy to install configuration on Aircraft Simulator；
3rd, true aircraft circuit breaker has specificity, it is impossible to meet different type of machines demand, and this breaker can be by letter
Singly change for different type of machines.
Description of the drawings
Fig. 1 is a kind of component locations schematic diagram of the preferred structure of this device when aircraft circuit breaker adhesive is simulated
Fig. 2 is that Fig. 1 is simulating component locations schematic diagram when aircraft circuit breaker disconnects
In Fig. 1～2：1 is support frame, and 101 is upper strata cavity, and 102 is intermediate transverse girder, and 103 is lower floor's cavity, and 2 is to stretch
Contracting bar, 3 is button cap, and 4 is block, and 5 is spring, and 6 is contact disc, and 7 is electromagnet, and 8 is fairlead.
Specific embodiment
Below in conjunction with the accompanying drawings the invention will be further described.
As shown in Fig. 1～2, hollow support frame 1 is in " day " font, including upper strata cavity 101, the He of intermediate transverse girder 102
Lower floor's cavity 103, the section of intermediate transverse girder 102 is L-shaped, and bottom crosspiece vertically opens up through hole, vertical in hollow support framework 1
A piece expansion link 2 of configuration；The upper end of expansion link 2 is provided with button cap 3, and button cap 3 exposes to the over top of hollow support framework 1；
The top of support frame frame 1 is installed with fairlead 8, and fairlead 8 is located at the lower section of button cap 3, and expansion link 2 is passed through from activity in fairlead 8.
The stage casing of expansion link 2 is provided with block 4, and block 4 is set screw, and the stage casing of expansion link 2 is thread segment, and set screw is screwed
On thread segment, can relative telescopic bar it is in rotary moving about 2；Block 4 is located in upper strata cavity 101, block 4 and intermediate transverse girder
Spring 5 is press-fitted between 102, spring 5 is the spring stack being sleeved on expansion link 2；The lower end of expansion link 2 is located in lower floor's cavity 103,
End be provided with can by the contact disc 6 of magnetic absorption, or, expansion link 2 have can be by the lower end of magnetic absorption；Lower floor's cavity
Fixed electromagnet 7 in 103, controller controls the power supply of electromagnet 7, and in cylinder, contact disc 6 is concentric with electromagnet 7 to magnet 7
The disk of configuration, the card outer rim of contact disc 6 is located at the upper surface outer rim outside of electromagnet 7.
The spring 5 of intermediate transverse girder 102 is press-fitted between bottom crosspiece and set screw 4；The perpendicular section in its top near spring 5, with
Play a part of auxiliary stopper and stable support.
As shown in figure 1, controller control electromagnet 7 is powered, electromagnet 7 is set to produce magnetic, now by manually pressing downwards
Pressure button cap 3, expansion link 2 promotes contact disc 6 attracting with electromagnet 7, the process of this process simulation aircraft circuit breaker adhesive；Such as
Shown in Fig. 2, when controller controls 7 power-off of electromagnet, expansion link 2 drives contact disc 6 and electromagnet 7 in the presence of spring 5
Separate, when this process simulation aircraft is faulty, aircraft circuit breaker disconnection process.
Claims (7)
1. the emulation breaker of a kind of flight simulator, it is characterised in that：
Hollow support frame (1) is in " day " font, including upper strata cavity (101), intermediate transverse girder (102) and lower floor's cavity
(103),
A piece expansion link (2) of vertical configuration in hollow support framework (1)；
Expansion link (2) upper end is provided with button cap (3), and button cap (3) exposes to hollow support framework (1) over top；
Expansion link (2) stage casing is provided with block (4), block (4) in upper strata cavity (101), block (4) and intermediate transverse girder
(102) spring (5) is press-fitted between；
Expansion link (2) lower end be located at lower floor's cavity (103) in, end be provided with can by the contact disc (6) of magnetic absorption, or,
Expansion link (2) is with can be by the lower end of magnetic absorption；
Fixed electromagnet (7) in lower floor's cavity (103), the power supply of controller control electromagnet (7).
2. the emulation breaker of flight simulator according to claim 1, it is characterised in that：The spring (5) is suit
Spring stack on expansion link (2), or the dish-shaped reed being sleeved on expansion link (2), or the spring in anti-" V " font configuration
Piece.
3. the emulation breaker of flight simulator according to claim 1, it is characterised in that：Support frame (1) top
Portion is installed with fairlead (8), and fairlead (8) is passed through positioned at button cap (3) lower section, expansion link (2) from activity in fairlead (8).
4. the emulation breaker of flight simulator according to claim 1, it is characterised in that：The block (4) is regulation
Screw, expansion link (2) stage casing is thread segment, and set screw is tightened on thread segment, can relative telescopic bar (2) rotate shifting up and down
It is dynamic.
5. the emulation breaker of flight simulator according to claim 1, it is characterised in that：The intermediate transverse girder (102)
Section it is L-shaped, its bottom crosspiece vertically opens up through hole, and spring (5) is press-fitted between bottom crosspiece and set screw (4)；
The perpendicular section in its top is near spring (5).
6. the emulation breaker of flight simulator according to claim 1, it is characterised in that：The electromagnet (7) is in circle
Cylindricality, contact disc (6) is the disk with electromagnet (7) concentric arrangement, and the card outer rim of contact disc (6) is located on electromagnet (7)
Surface periphery outside.
7. the emulation breaker of flight simulator according to claim 1, it is characterised in that：The intermediate transverse girder (102)
It is arranged in the elongated vertically-mounted groove of support frame (1) both sides by bolt, by the height position for adjusting intermediate transverse girder (102)
Putting can change the size of upper strata cavity (101) and lower floor's cavity (103).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610906352.2A CN106571252A (en) | 2016-10-18 | 2016-10-18 | Simulation circuit breaker of flight simulator |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610906352.2A CN106571252A (en) | 2016-10-18 | 2016-10-18 | Simulation circuit breaker of flight simulator |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106571252A true CN106571252A (en) | 2017-04-19 |
Family
ID=60414187
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610906352.2A Pending CN106571252A (en) | 2016-10-18 | 2016-10-18 | Simulation circuit breaker of flight simulator |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106571252A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110211832A (en) * | 2019-06-13 | 2019-09-06 | 成都纬航科技有限公司 | A kind of disconnect switch suitable for flight simulation control |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101866782A (en) * | 2010-07-27 | 2010-10-20 | 天津久安集团有限公司 | Auxiliary device of debug circuit breaker mechanism |
| CN102931024A (en) * | 2012-11-21 | 2013-02-13 | 正泰电气股份有限公司 | Device for simulating function of vacuum arc-extinguishing chamber |
| JP2014232618A (en) * | 2013-05-29 | 2014-12-11 | 三菱電機株式会社 | Electromagnetic operation device |
| CN204807686U (en) * | 2015-06-08 | 2015-11-25 | 杭州之江开关股份有限公司 | Circuit breaker electro -magnet measuring force device |
-
2016
- 2016-10-18 CN CN201610906352.2A patent/CN106571252A/en active Pending
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101866782A (en) * | 2010-07-27 | 2010-10-20 | 天津久安集团有限公司 | Auxiliary device of debug circuit breaker mechanism |
| CN102931024A (en) * | 2012-11-21 | 2013-02-13 | 正泰电气股份有限公司 | Device for simulating function of vacuum arc-extinguishing chamber |
| JP2014232618A (en) * | 2013-05-29 | 2014-12-11 | 三菱電機株式会社 | Electromagnetic operation device |
| CN204807686U (en) * | 2015-06-08 | 2015-11-25 | 杭州之江开关股份有限公司 | Circuit breaker electro -magnet measuring force device |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110211832A (en) * | 2019-06-13 | 2019-09-06 | 成都纬航科技有限公司 | A kind of disconnect switch suitable for flight simulation control |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN205899846U (en) | Virtual reality live working simulation training device | |
| CN203551693U (en) | Key detection device | |
| CN205177229U (en) | College mathematics teaching probability demonstration teaching aid | |
| CN106571252A (en) | Simulation circuit breaker of flight simulator | |
| CN206134526U (en) | Flight simulator's emulation circuit breaker | |
| CN204333697U (en) | A kind of 110kV isolating switch motor-operating mechanism mounting platform | |
| KR200450514Y1 (en) | The wool which uses the air spring mosyen base system | |
| CN204964564U (en) | Simple and easy clamp bar utensil of automatic test of mainboard | |
| CN204557858U (en) | A kind of two Graphic Panel devices of language teaching Electromagnetic Control lifting | |
| CN204791639U (en) | Aircraft is driven power of manipulation and is felt analogue means | |
| CN202282293U (en) | Indoor AC high voltage vacuum contactor | |
| CN204167214U (en) | The on-delay type relay that element moves into place can be ensured | |
| CN204373783U (en) | A kind of visual field switches put in place adsorbent equipment and thermal infrared imager | |
| CN203603087U (en) | Barrier gate with electromagnetic wind-resisting device | |
| CN209388516U (en) | Novel IPT flight simulation system with motion system | |
| CN204029323U (en) | A kind of silver-colored booth Special advertisement board automatic windproof device | |
| CN204167213U (en) | The system that power cut off delay type relay moves accuracy can be improved | |
| CN206155779U (en) | Four rotor craft wheel -retracting gears | |
| CN202036773U (en) | Electronic bowling game device | |
| CN205686555U (en) | Control electronic thinking balance car clean boot and the membrane switch mounting structure ridden | |
| CN209188080U (en) | Jump ball game machine ball-handling mechanism | |
| CN204028967U (en) | The tower probe control gear writing chip apparatus of a kind of smart card | |
| CN209190524U (en) | A kind of high iron sleeper production sanding and polishing device | |
| CN201677938U (en) | Device for improving buoyancy | |
| CN108436414B (en) | Solenoid valve block installs standby label turnover 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 | ||
| WD01 | Invention patent application deemed withdrawn after publication | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20170419 |