CN108597965A - A kind of emulation aircraft breaker - Google Patents
A kind of emulation aircraft breaker Download PDFInfo
- Publication number
- CN108597965A CN108597965A CN201810213437.1A CN201810213437A CN108597965A CN 108597965 A CN108597965 A CN 108597965A CN 201810213437 A CN201810213437 A CN 201810213437A CN 108597965 A CN108597965 A CN 108597965A
- Authority
- CN
- China
- Prior art keywords
- push
- microswitch
- fixture block
- solenoid valve
- encapsulating shell
- 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.)
- Granted
Links
- 230000006835 compression Effects 0.000 claims description 13
- 238000007906 compression Methods 0.000 claims description 13
- 238000009434 installation Methods 0.000 claims 1
- 238000000605 extraction Methods 0.000 abstract description 5
- 230000000694 effects Effects 0.000 abstract description 3
- 230000000712 assembly Effects 0.000 abstract 2
- 238000000429 assembly Methods 0.000 abstract 2
- 238000010586 diagram Methods 0.000 description 5
- 238000005516 engineering process Methods 0.000 description 3
- 238000004088 simulation Methods 0.000 description 3
- 230000009471 action Effects 0.000 description 2
- 230000002159 abnormal effect Effects 0.000 description 1
- 230000004913 activation Effects 0.000 description 1
- 230000008901 benefit Effects 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 239000000686 essence Substances 0.000 description 1
- 238000004880 explosion Methods 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
Classifications
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01H—ELECTRIC SWITCHES; RELAYS; SELECTORS; EMERGENCY PROTECTIVE DEVICES
- H01H71/00—Details of the protective switches or relays covered by groups H01H73/00 - H01H83/00
- H01H71/10—Operating or release mechanisms
Abstract
The present invention provides a kind of emulation aircraft breakers, including by preceding cap, the hollow frame that post package lid and encapsulating shell surround, push and pull cap assembly, limit card block component, microswitch and solenoid valve, the push-and-pull cap assemblies pass through at the top of encapsulating shell, the limit card block component, microswitch and solenoid valve are arranged in hollow frame, the microswitch is arranged in the lower section of push-and-pull cap assembly, the folding of the push-and-pull cap assembly push-and-pull control microswitch, the limit card block module position is adapted with the push-and-pull cap assemblies for stretching into envelope part, the limit card block component is arranged in the top of solenoid valve, the limit card block component limitation push-and-pull cap assembly movement, the solenoid valve is installed in the bottom of encapsulating shell, microswitch and solenoid valve electrical connection.A kind of emulation aircraft breaker of the present invention, topology layout is compact, and appearance and size is small, can realize Manual press, extraction function and jump out function automatically, simulated effect is good.
Description
Technical field
The invention belongs to flight simulation technology fields, more particularly, to a kind of emulation aircraft breaker.
Background technology
In recent years, with the continuous development of air market, the demand to emulation simulator is also increasing, flight simulation mould
For quasi- device to true simulation aircraft true to nature, aircraft circuit breaker is an essential part.Since actual airplane has less then
Thirty or forty, at most up to a hundred huge breaker quantity, and single true aircraft circuit breaker price is more expensive so that flight
The cost of simulator is high.
It is current in the market there are no the emulation breaker specially used for simulating true aircraft circuit breaker, be substantially
It together makes a return journey use by existing multiple breakers, this has resulted in also increasing using the diversification of component, hugeization of volume
Big cost, thus develop it is a kind of imperative for flight simulator, inexpensive aircraft circuit breaker.
Invention content
In view of this, the present invention is directed to propose a kind of emulation aircraft breaker, can preferably meet Aircraft Simulator makes
With needs, solve the problems, such as to lack the dedicated emulated breaker of Aircraft Simulator in the market.
In order to achieve the above objectives, the technical proposal of the invention is realized in this way：
A kind of emulation aircraft breaker includes the hollow frame surrounded by preceding cap, post package lid and encapsulating shell, pushes and pulls
Cap assembly, limit card block component, microswitch and solenoid valve, the push-and-pull cap assembly pass through at the top of encapsulating shell, the limit
Position fixture block component, microswitch and solenoid valve are arranged in hollow frame, and microswitch setting is in push-and-pull cap assembly
Lower section, the folding of the described push-and-pull cap assembly push-and-pull control microswitch limit card block module position and stretches into envelope
The push-and-pull cap assembly for filling shell parts is adapted, and the limit card block component is arranged in the top of solenoid valve, the limiting card
Block assembly limitation push-and-pull cap assembly movement, the solenoid valve are installed in the bottom of encapsulating shell, the microswitch and electromagnetism
Valve is electrically connected.
Further, the push-and-pull cap assembly includes breaker cap, compression spring and push button shaft, and the push button shaft includes one
The upper pressing axis being arranged and lower grab, the lower grab eccentric setting, the compression spring is set in pressing axis, described
Upper pressing axis is equipped with the first limit hole, and the upper pressing axis passes through the mounting base at the top of encapsulating shell to be connect with breaker cap,
The upper pressing axis is connect by the first mounting post with mounting base, and first mounting post passes through the first limit hole.
Further, the limit card block component includes fixture block, fixture block tabletting and tension spring, and the fixture block includes integrally setting
The upper grab and lower position block set, the upper grab coordinate with lower grab, and the lower position block is equipped with inclined second
Limit hole, the encapsulating shell are equipped with fixture block close to the side of fixture block and move guide surface, and the lower position block is transported close to fixture block
The side of dynamic guide surface is the first inclined surface that guide surface cooperation is moved with fixture block, and the lower position block is with respect to the first inclined surface
Side be the second inclined surface, the fixture block guide surface, the first inclined surface, the second inclined surface and the second limit hole inclination side
It is connect to identical, described fixture block tabletting with the fixture block tabletting mounting base on encapsulating shell by two the second mounting posts, wherein one
A second mounting post passes through the second limit hole, and the second mounting post described in another offsets with the second inclined surface, described
Tension spring one end connect with the second mounting post described in another, the other end is connect with across the third mounting post of upper grab.
Further, the microswitch is connect by the 4th mounting post with the microswitch mounting base on encapsulating shell.
Further, it is equipped with compression spring in the mounting base and limits edge.
Further, the length of two second mounting posts and the 4th mounting post with preceding cap and post package lid it
Between distance it is equal.
Compared with the existing technology, a kind of emulation aircraft breaker of the present invention has the advantage that：Push and pull cap assembly
With the setting of limit card block component, the authenticity of emulation aircraft breaker operator is not only improved, but also realizes manual toggle operation
It is difunctional with automatically reseting, it is safe；Topology layout is compact, and appearance and size is small, can realize Manual press, extraction function
With jump out function automatically, simulated effect is good.
Description of the drawings
The attached drawing for constituting the part of the present invention is used to provide further understanding of the present invention, schematic reality of the invention
Example and its explanation are applied for explaining the present invention, is not constituted improper limitations of the present invention.In the accompanying drawings：
Fig. 1 is a kind of Structure explosion diagram of emulation aircraft breaker described in the embodiment of the present invention；
Fig. 2 is the structural representation of a kind of emulation aircraft breaker described in the embodiment of the present invention removed after preceding cap
Figure；
Fig. 3 is push button shaft structural schematic diagram in a kind of emulation aircraft breaker described in the embodiment of the present invention；
Fig. 4 is fixture block structural schematic diagram in a kind of emulation aircraft breaker described in the embodiment of the present invention；
Fig. 5 is a kind of pressing functional status figure of emulation aircraft breaker described in the embodiment of the present invention；
Fig. 6 is a kind of extraction function state diagram of emulation aircraft breaker described in the embodiment of the present invention；
Fig. 7 is that a kind of the automatic of emulation aircraft breaker described in the embodiment of the present invention jumps out functional status figure.
Reference sign：
1- post package lids, 2- encapsulating shells, 3- breaker caps, 4- compression springs, 5- push button shafts, the upper pressing axis of 501-；Block under 502-
Hook；The first limit holes of 503-；6- mounting bases, 7- fixture blocks, the upper grabs of 701-；702- lower position blocks；The first inclined surface 7021-；
The second inclined surface 7022-；The second limit holes of 703-；8- third mounting posts, 9- microswitches；The 4th mounting posts of 10-；11- tension springs；
12- fixture block tablettings；The second mounting posts of 13-；The first mounting posts of 14-；15- solenoid valves；16- caps；The movement guiding of 17- fixture blocks
Face；18- fixture block tabletting mounting bases；19- microswitch mounting bases.
Specific implementation mode
It should be noted that in the absence of conflict, the feature in embodiment and embodiment in the present invention can phase
Mutually combination.
The present invention will be described in detail below with reference to the accompanying drawings and embodiments.
As Figure 1-Figure 4, a kind of emulation aircraft breaker, including by preceding cap 16, post package lid 1 and encapsulating shell 2
Hollow frame, push-and-pull cap assembly, limit card block component, microswitch 9 and solenoid valve 15, the push-and-pull cap assembly surrounded is worn
2 top of encapsulating shell is crossed, the limit card block component, microswitch 9 and solenoid valve 15 are arranged in hollow frame, described
Microswitch 9 is arranged in the lower section of push-and-pull cap assembly, and the push-and-pull cap assembly push-and-pull controls the folding of microswitch 9, described
Limit card block module position and stretch into the push-and-pull cap assembly of 2 part of encapsulating shell and be adapted, the described limit card block component setting
In the top of solenoid valve 15, limit card block component limitation push-and-pull cap assembly movement, the solenoid valve 15 is installed in envelope
The bottom of shell 2 is filled, the microswitch 9 and solenoid valve 15 are electrically connected.
The push-and-pull cap assembly includes breaker cap 3, compression spring 4 and push button shaft 5, and the push button shaft 5 includes being wholely set
Upper pressing axis 501 and lower grab 502,502 eccentric setting of lower grab, the compression spring 4 be set in pressing axis 501
On, the upper pressing axis 501 is equipped with the first limit hole 503, and the upper pressing axis 501 passes through the peace at 2 top of encapsulating shell
Dress seat 6 is connect with breaker cap 3, and the upper pressing axis 501 is connect by the first mounting post 14 with mounting base 6, and described the
One mounting post 14 passes through the first limit hole 503.
The limit card block component includes fixture block 7, fixture block tabletting 12 and tension spring 11, and the fixture block 7 includes being wholely set
Upper grab 701 and lower position block 702, the upper grab 701 and lower grab 702 coordinate, set on the lower position block 702
There is inclined second limit hole 703, the encapsulating shell 2 is equipped with fixture block close to the side of fixture block 7 and moves guide surface 17, described
The side that lower position block 702 moves guide surface 17 close to fixture block is to move the first inclined surface that guide surface 17 coordinates with fixture block
7021, the lower position block 702 is the second inclined surface 7022, fixture block movement with respect to the side of the first inclined surface 7021
Guide surface 17, the first inclined surface 7021, the second inclined surface 7022 card identical, described with the inclined direction of the second limit hole 703
Block tabletting 12 is connect by two the second mounting posts 13 with the fixture block tabletting mounting base 18 on encapsulating shell 2, described in one of them
Second mounting post 13 passes through the second limit hole 703, the second mounting post 13 described in another to offset with the second inclined surface 7022, institute
11 one end of tension spring stated is connect with the second mounting post 13 described in another, the other end and the third mounting post 8 for passing through upper grab 701
Connection.
Microswitch 9 is connect by the 4th mounting post 10 with the microswitch mounting base 19 on encapsulating shell 2.
It is equipped with compression spring in mounting base 6 and limits edge, compression spring 4 is limited, to realize the automatic rebounding work(of push-and-pull cap assembly
Energy.
The length of two the second mounting posts 13 and the 4th mounting post 10 between preceding cap 16 and post package lid 1 away from
From equal, preceding cap 16 and post package lid 1 need to be only connected on encapsulating shell 2 by breaker can be by microswitch 9 and fixture block
The position of tabletting 12 is fixed, without being fixedly connected, easy assembly and disassembly.
Preceding cap 16, post package lid 1 and solenoid valve 15 are fixedly connected by screw with encapsulating shell 2.
It is fixedly connected by screw between push button shaft 5 and breaker cap 3.
Digital patch can also be set on breaker cap 3.
Fixture block move guide surface 17, the first inclined surface 7021, the second inclined surface 7022 and the second limit hole 703 inclination side
To being all 30 °, guiding fixture block 7 moves so that breaker can realize Manual press, manual-up pull out and jump out automatically function.
This breaker mainly emulates the pressing, extraction, auto-cutout function of breaker.
It is illustrated in figure 5 the pressing functional status figure of emulation aircraft breaker：Block when pushing and pulling cap assembly and being pressed downward
Block 7 is rotated clockwise around third mounting post 8, and lower grab 502 is fastened with upper grab 701, is limited by the pulling force effect of tension spring 11
The homing action of push button shaft 5, while upper pressing axis 501 presses microswitch 9, so that microswitch 9 is formed activation signal, by upper
State the on-state that breaker is completed in action.
It is illustrated in figure 6 the extraction function state diagram of emulation aircraft breaker：When breaker needs to extract manually,
Push-and-pull cap assembly is firmly extracted upwards, so that push button shaft 5 is moved upwards, to slowly release limit function with fixture block 7, fine motion is opened
It closes 9 and forms cut-off signal formation off-state.
It is illustrated in figure 7 the automatic of emulation aircraft breaker and jumps out functional status figure：It is formd after completing to press function
Signal is connected, when we need auto-cutout function at this time, solenoid valve 15 is fed back by the signal of microswitch 9 to be powered,
To push fixture block 7, fixture block 7 and the limit of push button shaft 5 is made to release, pushes and pulls cap assembly in this way and acted on certainly by the compression spring of compression spring 4
Dynamic rebound, forms off state.This function is mainly to a kind of automatic protection functions under abnormal circuit conditions.
The foregoing is merely illustrative of the preferred embodiments of the present invention, is not intended to limit the invention, all essences in the present invention
With within principle, any modification, equivalent replacement, improvement and so on should all be included in the protection scope of the present invention god.
Claims (6)
1. a kind of emulation aircraft breaker, it is characterised in that：Including by preceding cap (16), post package lid (1) and encapsulating shell (2)
Hollow frame, push-and-pull cap assembly, limit card block component, microswitch (9) and the solenoid valve (15) surrounded, the push-and-pull cap group
Part passes through at the top of encapsulating shell (2), and the limit card block component, microswitch (9) and solenoid valve (15) are arranged at middle empty frames
In frame, the microswitch (9) is arranged in the lower section of push-and-pull cap assembly, push-and-pull cap assembly push-and-pull control microswitch
(9) folding, the limit card block module position and the push-and-pull cap assembly for stretching into encapsulating shell (2) part are adapted, described
For the setting of limit card block component in the top of solenoid valve (15), limit card block component limitation push-and-pull cap assembly movement is described
Solenoid valve (15) be installed in the bottoms of encapsulating shell (2), the microswitch (9) and solenoid valve (15) electrical connection.
2. a kind of emulation aircraft breaker according to claim 1, it is characterised in that：The push-and-pull cap assembly includes open circuit
Device cap (3), compression spring (4) and push button shaft (5), the push button shaft (5) include the upper pressing axis (501) being wholely set and lower grab
(502), described lower grab (502) eccentric setting, the compression spring (4) are set in pressing axis (501), it is described on press
Last item (501) is equipped with the first limit hole (503), and the upper pressing axis (501) passes through the mounting base at the top of encapsulating shell (2)
(6) it is connect with breaker cap (3), the upper pressing axis (501) is connect by the first mounting post (14) with mounting base (6), institute
The first mounting post (14) stated passes through the first limit hole (503).
3. a kind of emulation aircraft breaker according to claim 2, it is characterised in that：The limit card block component includes card
Block (7), fixture block tabletting (12) and tension spring (11), the fixture block (7) include the upper grab (701) and lower position block being wholely set
(702), the upper grab (701) coordinates with lower grab (702), and the lower position block (702) is equipped with inclined second
Limit hole (703), the encapsulating shell (2) are equipped with fixture block movement guide surface (17), the lower limit close to the side of fixture block (7)
Position block (702) is to move the first inclined surface that guide surface (17) coordinates with fixture block close to the side of fixture block movement guide surface (17)
(7021), the lower position block (702) is the second inclined surface (7022) with respect to the side of the first inclined surface (7021), described
Fixture block move guide surface (17), the first inclined surface (7021), the second inclined surface (7022) and the second limit hole (703) inclination side
Pass through the fixture block tabletting mounting base on two the second mounting posts (13) and encapsulating shell (2) to identical, described fixture block tabletting (12)
(18) it connects, the second mounting post (13) described in one of them passes through the second limit hole (703), the second installation described in another
Column (13) offsets with the second inclined surface (7022), and the tension spring (11) one end connects with another described second mounting post (13)
It connects, the other end is connect with the third mounting post (8) across upper grab (701).
4. a kind of emulation aircraft breaker according to claim 3, it is characterised in that：The microswitch (9) passes through
Four mounting posts (10) are connect with the microswitch mounting base (19) on encapsulating shell (2).
5. a kind of emulation aircraft breaker according to claim 1 or 4, it is characterised in that：It is equipped in the mounting base (6)
Compression spring limits edge.
6. a kind of emulation aircraft breaker according to claim 5, it is characterised in that：Two second mounting posts (13)
It is equal with the distance between preceding cap (16) and post package lid (1) with the length of the 4th mounting post (10).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810213437.1A CN108597965B (en) | 2018-03-15 | 2018-03-15 | Simulated aircraft circuit breaker |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810213437.1A CN108597965B (en) | 2018-03-15 | 2018-03-15 | Simulated aircraft circuit breaker |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN108597965A true CN108597965A (en) | 2018-09-28 |
| CN108597965B CN108597965B (en) | 2023-12-12 |
Family
ID=63626354
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810213437.1A Active CN108597965B (en) | 2018-03-15 | 2018-03-15 | Simulated aircraft circuit breaker |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108597965B (en) |
Citations (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0325501A1 (en) * | 1988-01-20 | 1989-07-26 | Hager Electro S.A. | Automatic switches, in particular differential switches and circuit breakers |
| KR20030064428A (en) * | 2002-01-25 | 2003-08-02 | 민경옥 | Multifunction circuit breaker |
| CN101030508A (en) * | 2006-02-27 | 2007-09-05 | 富士电机机器制御株式会社 | Trip release device of an electric circuit breaker |
| CN102262965A (en) * | 2010-05-31 | 2011-11-30 | 维熹科技股份有限公司 | Microswitch |
| WO2013064635A1 (en) * | 2011-11-02 | 2013-05-10 | Eaton Industries Manufacturing Gmbh | Electromagnetic circuit breaker |
| CN104021956A (en) * | 2014-06-20 | 2014-09-03 | 成都翼胜科技有限责任公司 | Analogue switch and implementation method thereof |
| US20150132094A1 (en) * | 2013-11-13 | 2015-05-14 | Kubota Corporation | Working machine and method for operating working machine |
| CN105160961A (en) * | 2015-09-29 | 2015-12-16 | 哈尔滨莱特兄弟科技开发有限公司 | Simulation aircraft undercarriage analogue device |
| CN105810516A (en) * | 2014-12-29 | 2016-07-27 | 上海良信电器股份有限公司 | Circuit breaker opening/closing operation device |
| CN206265021U (en) * | 2016-12-13 | 2017-06-20 | 昆山航理机载设备股份有限公司 | Shutdown brake simulation handle |
-
2018
- 2018-03-15 CN CN201810213437.1A patent/CN108597965B/en active Active
Patent Citations (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0325501A1 (en) * | 1988-01-20 | 1989-07-26 | Hager Electro S.A. | Automatic switches, in particular differential switches and circuit breakers |
| KR20030064428A (en) * | 2002-01-25 | 2003-08-02 | 민경옥 | Multifunction circuit breaker |
| CN101030508A (en) * | 2006-02-27 | 2007-09-05 | 富士电机机器制御株式会社 | Trip release device of an electric circuit breaker |
| CN102262965A (en) * | 2010-05-31 | 2011-11-30 | 维熹科技股份有限公司 | Microswitch |
| WO2013064635A1 (en) * | 2011-11-02 | 2013-05-10 | Eaton Industries Manufacturing Gmbh | Electromagnetic circuit breaker |
| US20150132094A1 (en) * | 2013-11-13 | 2015-05-14 | Kubota Corporation | Working machine and method for operating working machine |
| CN104021956A (en) * | 2014-06-20 | 2014-09-03 | 成都翼胜科技有限责任公司 | Analogue switch and implementation method thereof |
| CN105810516A (en) * | 2014-12-29 | 2016-07-27 | 上海良信电器股份有限公司 | Circuit breaker opening/closing operation device |
| CN105160961A (en) * | 2015-09-29 | 2015-12-16 | 哈尔滨莱特兄弟科技开发有限公司 | Simulation aircraft undercarriage analogue device |
| CN206265021U (en) * | 2016-12-13 | 2017-06-20 | 昆山航理机载设备股份有限公司 | Shutdown brake simulation handle |
Also Published As
| Publication number | Publication date |
|---|---|
| CN108597965B (en) | 2023-12-12 |
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