CN108288416A - A kind of simulation aircraft fire protection control panel manipulation device - Google Patents
A kind of simulation aircraft fire protection control panel manipulation device Download PDFInfo
- Publication number
- CN108288416A CN108288416A CN201810234808.4A CN201810234808A CN108288416A CN 108288416 A CN108288416 A CN 108288416A CN 201810234808 A CN201810234808 A CN 201810234808A CN 108288416 A CN108288416 A CN 108288416A
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- Prior art keywords
- gear
- simulation
- tabletting
- triggering
- handle
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Links
- 238000004088 simulation Methods 0.000 title claims abstract description 70
- 230000007246 mechanism Effects 0.000 claims abstract description 78
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 claims abstract description 4
- 229910052802 copper Inorganic materials 0.000 claims abstract description 4
- 239000010949 copper Substances 0.000 claims abstract description 4
- 229910000831 Steel Inorganic materials 0.000 claims description 14
- 239000010959 steel Substances 0.000 claims description 14
- 125000006850 spacer group Chemical group 0.000 claims description 7
- 239000007787 solid Substances 0.000 claims description 4
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims 3
- 229910052742 iron Inorganic materials 0.000 claims 1
- 238000010586 diagram Methods 0.000 description 4
- 230000002265 prevention Effects 0.000 description 4
- 230000005611 electricity Effects 0.000 description 2
- 239000002360 explosive Substances 0.000 description 2
- 229910000639 Spring steel Inorganic materials 0.000 description 1
- 238000005094 computer simulation Methods 0.000 description 1
- 239000000686 essence Substances 0.000 description 1
- 238000000605 extraction Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 239000011148 porous material Substances 0.000 description 1
- 238000004064 recycling Methods 0.000 description 1
- 239000000837 restrainer Substances 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- 230000001960 triggered effect Effects 0.000 description 1
Classifications
-
- G—PHYSICS
- G09—EDUCATION; CRYPTOGRAPHY; DISPLAY; ADVERTISING; SEALS
- G09B—EDUCATIONAL OR DEMONSTRATION APPLIANCES; APPLIANCES FOR TEACHING, OR COMMUNICATING WITH, THE BLIND, DEAF OR MUTE; MODELS; PLANETARIA; GLOBES; MAPS; DIAGRAMS
- G09B9/00—Simulators for teaching or training purposes
- G09B9/02—Simulators for teaching or training purposes for teaching control of vehicles or other craft
- G09B9/08—Simulators for teaching or training purposes for teaching control of vehicles or other craft for teaching control of aircraft, e.g. Link trainer
- G09B9/28—Simulation of stick forces or the like
-
- G—PHYSICS
- G09—EDUCATION; CRYPTOGRAPHY; DISPLAY; ADVERTISING; SEALS
- G09B—EDUCATIONAL OR DEMONSTRATION APPLIANCES; APPLIANCES FOR TEACHING, OR COMMUNICATING WITH, THE BLIND, DEAF OR MUTE; MODELS; PLANETARIA; GLOBES; MAPS; DIAGRAMS
- G09B9/00—Simulators for teaching or training purposes
- G09B9/02—Simulators for teaching or training purposes for teaching control of vehicles or other craft
- G09B9/08—Simulators for teaching or training purposes for teaching control of vehicles or other craft for teaching control of aircraft, e.g. Link trainer
- G09B9/085—Special purpose teaching, e.g. alighting on water, aerial photography
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- Engineering & Computer Science (AREA)
- Theoretical Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Business, Economics & Management (AREA)
- Physics & Mathematics (AREA)
- Educational Administration (AREA)
- Educational Technology (AREA)
- General Physics & Mathematics (AREA)
- Management, Administration, Business Operations System, And Electronic Commerce (AREA)
- Railway Tracks (AREA)
Abstract
The present invention provides a kind of simulation aircraft fire protection control panel manipulation devices, it include the top tie plate disposed in parallel supported by multiple copper posts, the frame and three groups of operating mechanisms that middle part control circuit board and lower tie plate surround, three groups of operating mechanisms are distributed on frame, three groups of operating mechanisms control the fire extinguishing of three engines respectively, every group of operating mechanism includes handle mechanism, trigger position-limit mechanism, gear simulation mechanism and electromagnet, handle mechanism passes through frame to be connect successively with triggering position-limit mechanism and gear simulation mechanism, gear simulation mechanism is fixedly connected with triggering position-limit mechanism, electromagnet limits handle mechanism movement, the signal on fire that middle part control circuit board receives engine controls corresponding electromagnet running, the signal that middle part control circuit board receives triggering position-limit mechanism is sent to terminal simulation extinguishing action.The present invention really simulate aircraft engine it is on fire when extinguishing action and override needed for operation, and can get operating handle as actual airplane.
Description
Technical field
The invention belongs to flight simulation technology fields, manipulate and fill more particularly, to a kind of simulation aircraft fire protection control panel
It sets.
Background technology
Domestic flight student is when carrying out the training of the actions such as simulated engine in-flight fire by simulation softward, without mould
Quasi- operating device, can not experience the operation logic and override mode of actual airplane.In addition, external also have design simulation to manipulate dress
It sets, is composed using the part of some actual airplanes, although having reached the fire prevention operation of simulation actual airplane, but cost
Costliness, it is less economical.Therefore the manipulation device of fire prevention control panel a kind of economical and practical and that prototype can be simulated is needed.
Invention content
In view of this, the present invention is directed to propose a kind of simulation aircraft fire protection control panel manipulation device, main analog Boeing
The fire prevention control panel manipulation device of 737-800 aircrafts, it is consistent with logic with the operation of actual airplane, it really simulates winged
The operation needed for extinguishing action and override when machine engine fires, and can get the operating handle as actual airplane.
In order to achieve the above objectives, the technical proposal of the invention is realized in this way：
A kind of simulation aircraft fire protection control panel manipulation device includes being consolidated by the top disposed in parallel that multiple copper posts support
The frame and three groups of operating mechanisms that fixed board, middle part control circuit board and lower tie plate surround, operating mechanism described in three groups are uniformly distributed
On frame, operating mechanism described in three groups controls the fire extinguishing of three engines respectively, and operating mechanism described in every group includes handle
Mechanism, triggering position-limit mechanism, gear simulation mechanism and electromagnet, the handle mechanism pass through frame successively with triggering position restrainer
Structure is connected with gear simulation mechanism, and the triggering position-limit mechanism is fixedly connected with lower tie plate, the gear analog machine
Structure is fixedly connected with triggering position-limit mechanism, and the electromagnet limits handle mechanism movement, and the electromagnet is fixed on lower solid
On fixed board, the signal on fire that the middle part control circuit board receives engine controls corresponding electromagnet running, in described
The signal that portion's control circuit board receives triggering position-limit mechanism is sent to terminal simulation extinguishing action.
Further, the handle mechanism includes connection handle and manipulates block, and the connection handle sequentially passes through top
Fixed plate, middle part control circuit board and lower tie plate, the connection handle top are fixedly connected with block is manipulated, the company
Connecting handle is equipped with limit card slot with electromagnet corresponding position, and the lower part of the connection handle sequentially passes through triggering position-limit mechanism
With gear simulation mechanism.
Further, the triggering position-limit mechanism include triggering tabletting, left and right gear trigger switch, limited block and up and down
Gear trigger switch, the triggering tabletting are installed on connection handle, and the left and right gear trigger switch is installed in limit
The upper surface of block, and be arranged in the both sides of triggering tabletting, the trigger switch of gear up and down is installed in the lower surface of limited block,
And be arranged in the bottom of triggering tabletting, the limited block is equipped with triggering tabletting limiting slot, the triggering tabletting limiting slot
Slot bottom offer connection handle through hole and upper and lower gear trigger switch tabletting the first receiving opening.
Further, the gear simulation mechanism include gear simulated block, gear simulation fixed block, two springs, two
Steel ball and two anticreep tablettings, gear simulation fixed block are installed in the lower surface of limited block, and gear simulation is solid
Determine to be equipped with resettlement groove in the middle part of block, the gear simulated block is arranged in resettlement groove, and the middle part of the gear simulated block is equipped with
The perforative slotted hole of connection handle is accommodated, the both sides of the gear simulated block are arranged with waveform tooth, the gear
Simulated block both sides are offseted by a steel ball, a spring and an anticreep tabletting with corresponding waveform tooth.
Further, the anticreep tabletting described in two is separately fixed at the both sides of gear simulation fixed block, each described
The both ends of spring offset with the steel ball of respective side and anticreep tabletting respectively.
Further, the gear simulation fixed block is internally provided with the second receiving opening for placing spring and steel ball.
Further, the manipulation device further includes three override buttons, and each override button corresponds to one group of behaviour
Vertical mechanism, on three fixed top tie plates of override button.
Further, shape of the connection handle from connection triggering tabletting to end is adapted with oval pore size.
Further, the electromagnet is equipped with the spacer pin coordinated with limit card slot, is arranged on the spacer pin certainly
Resetting spring.
Further, the gear trigger switch up and down is fixed on the lower surface of limited block by connecting plate.
Compared with the existing technology, a kind of simulation aircraft fire protection control panel manipulation device of the present invention has following excellent
Gesture：
A kind of simulation aircraft fire protection control panel manipulation device of the present invention is prevented according to actual airplane operation logic
Fiery control panel manipulation device and the fire prevention control panel manipulation device shape and rotation angle phase one in actual airplane cockpit
It causes, can really simulate the operation of aircraft engine fire extinguishing control, training is made to have more authenticity, gear simulation mechanism is set
It sets, power when switching gear can be simulated so that when operation, obtain the operating handle as actual airplane, fidelity is high.
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 explosive view of simulation aircraft fire protection control panel manipulation device described in the embodiment of the present invention；
Fig. 2 is a kind of structural schematic diagram of simulation aircraft fire protection control panel manipulation device described in the embodiment of the present invention；
Fig. 3 is to be connected when not unlocking in a kind of simulation aircraft fire protection control panel manipulation device described in the embodiment of the present invention
The connection diagram of handle and electromagnet；
Fig. 4 be the embodiment of the present invention described in a kind of simulation aircraft fire protection control panel manipulation device in trigger position-limit mechanism
Structural schematic diagram；
Fig. 5 be the embodiment of the present invention described in a kind of simulation aircraft fire protection control panel manipulation device in limited block structure
Schematic diagram；
Fig. 6 is a kind of simulation aircraft fire protection control panel manipulation device middle gear simulation mechanism described in the embodiment of the present invention
Explosive view.
Reference sign：
1- manipulates block；2- override buttons；3- top tie plates；4- connection handles, 401- limit card slots；Control electricity in the middle part of 5-
Road plate, 6- lower tie plates, the left gear trigger switch of 7-, 8- trigger tabletting, 9- limited blocks；901- triggers tabletting limiting slot；
902- through holes；The first receiving openings of 903-；10- or more gear trigger switch；11- connecting plates；12- gear simulated blocks；1201-
Slotted hole；1202- waveform teeth；13- gears simulate fixed block；1301- resettlement grooves；The second receiving openings of 1302-；14- springs；
15- steel balls；16- anticreep tablettings；17- electromagnet；1701- spacer pins；The right gear trigger switch of 18-.
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 shown in figs 1 to 6, a kind of simulation aircraft fire protection control panel manipulation device, including by multiple copper post (not shown)
The frame and three groups of manipulations that top tie plate disposed in parallel 3, middle part control circuit board 5 and the lower tie plate 6 of support surround
Mechanism, operating mechanism is distributed on frame described in three groups, and operating mechanism described in three groups controls the fire extinguishing of three engines respectively, often
The group operating mechanism includes handle mechanism, triggering position-limit mechanism, gear simulation mechanism and electromagnet 17, the handle machine
Structure passes through frame to be connect successively with triggering position-limit mechanism and gear simulation mechanism, the triggering position-limit mechanism and lower tie plate
6 are fixedly connected, and the gear simulation mechanism is fixedly connected with triggering position-limit mechanism, and the electromagnet 17 limits handle mechanism
Movement, the electromagnet 17 are fixed on bottom plate 6, and the middle part control circuit board 5 receives the letter on fire of engine
Number corresponding electromagnet 17 of control operates, and the signal that the middle part control circuit board 5 receives triggering position-limit mechanism is sent to end
End simulation extinguishing action.
The handle mechanism includes connection handle 4 and manipulates block 1, and the connection handle 4 sequentially passes through top tie plate
3, middle part control circuit board 5 and lower tie plate 6,4 top of connection handle are fixedly connected with block 1 is manipulated, the company
Connecting handle 4 is equipped with limit card slot 401 with 17 corresponding position of electromagnet, and the lower part of the connection handle 4 sequentially passes through triggering
Position-limit mechanism and gear simulation mechanism.
The triggering position-limit mechanism includes triggering tabletting 8, left and right gear trigger switch 7 (18), limited block 9 and upper lower gear
Position trigger switch 10, the triggering tabletting 8 are installed on connection handle 4, and the left and right gear trigger switch 7 (18) is solid
It is located at the upper surface of limited block 9, and is arranged in the both sides of triggering tabletting 8, the trigger switch of gear up and down 10 is installed in limit
The lower surface of position block 9, and be arranged in the bottom of triggering tabletting 8, the limited block 9 is equipped with triggering tabletting limiting slot 901, institute
The slot bottom for the triggering tabletting limiting slot 901 stated offers the pressure of the through hole 902 and upper and lower gear trigger switch 10 of connection handle 4
First receiving opening 903 of piece.
The gear simulation mechanism includes gear simulated block 12, gear simulation 14, two, the spring steel ball of fixed block 13, two
15 and two anticreep tablettings 16, gear simulation fixed block 13 is installed in the lower surface of limited block 9, gear simulation
13 middle part of fixed block is equipped with resettlement groove 1301, and the gear simulated block 12 is arranged in resettlement groove 1301, the gear mould
The middle part of quasi- block 12 is equipped with the perforative slotted hole 1201 for accommodating connection handle 4, and the both sides of the gear simulated block 12 are symmetrical
Equipped with waveform tooth 1202,12 both sides of gear simulated block pass through a steel ball 15, a spring 14 and an anticreep tabletting 16
Offset with corresponding waveform tooth 1202, gear simulated block 12 by the undulated external structure of mechanical processing and combine spring 14,
The specific mechanical characteristic of the equal realizations of steel ball 15.
Anticreep tabletting 16 described in two is separately fixed at the both sides of gear simulation fixed block 13, each spring 14
Both ends offset respectively with the steel ball of respective side 15 and anticreep tabletting 16.
The gear simulation fixed block 13 is internally provided with the second receiving opening 1302 for placing spring 14 and steel ball 15.
The manipulation device further includes three override buttons 2, and each override button 2 corresponds to one group of operating mechanism,
On three override buttons 2 fixed top tie plate 3.
The connection handle 4 is adapted to the shape of end with 1201 size of slotted hole from connection triggering tabletting 8, connection
The connection rotation of handle 4 can be achieved with by slotted hole 1201 between handle 4 and gear simulated block 12 and drive 12 turns of gear simulated block
It is dynamic, it is fixedly connected between handle 4 and gear simulated block 12 without connecting, it is easy to disassemble, it is hardly damaged, recycling rate of waterused
It is high.
The electromagnet 17 is equipped with the spacer pin 1701 coordinated with limit card slot 401, is arranged on the spacer pin 1701
There are Self-resetting spring, electromagnet 17 to limit connection handle 4 by mechanical outline and pull up, when needed, electromagnet 17 is powered, limit
Pin 1701 shrinks to allow connection handle 4 to be extracted upwards；Later, pressing connects the Self-resetting of electromagnet 17 after handle 4
Spacer pin 1701 can be pressed into the limit card slot 401 of connection handle 4 by spring, to which limitation connection handle 4 is extracted again.
The gear trigger switch 10 up and down is fixed on the lower surface of limited block 9 by connecting plate 11.
When no signal on fire, connection handle 4 is lockked by electromagnet 17, prevents it from being extracted and being pushed down upwards up and down
Gear trigger switch 10 can not be rotated left and right by the structure in limited block 9.When middle part control circuit board 5 has received
When fiery signal, control electromagnet 17 unlocks, and connecting handle 4 at this time can be pulled out, and after connecting the extraction of handle 4, triggers tabletting 8
Gear trigger switch 10 up and down is no longer pushed down, middle part control circuit board 5 monitors feedback to the computer simulation cut-out oil after the signal
Road.After pulling out connection handle 4, connection handle 4 is pulled out to tabletting 8 is triggered other than limited block 9, to make connection handle 4 can
To be rotated left and right；Gear simulation mechanism can be driven to rotate together when rotating left and right connection handle；Gear simulation mechanism utilizes steel
Power when the waveform tooth 1202 of pearl 15, spring 14 and gear simulated block 12 simulates switching gear also limits connection handle 4
On specified gear；When connecting the rotation of handle 4, triggering tabletting 8 will be pressed into corresponding left and right gear trigger switch 7
(18), when middle part control circuit board 5 monitors this signal, corresponding signal will be sent to computer, to which simulation is started
Extinguishing chemical release in machine.If in-engine sensor could not be properly received the signal of engine fires, pressing can be passed through
2 compulsive unlocking electromagnet 17 of override button is to realize above-mentioned function.During engine fires or override button are pressed, electricity
Magnet 17 will unlock always, so as to pull out connection handle 4 at any time.
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 (10)
1. a kind of simulation aircraft fire protection control panel manipulation device, it is characterised in that：Include parallel being set by what multiple copper posts supported
The frame and three groups of operating mechanisms that top tie plate (3), middle part control circuit board (5) and the lower tie plate (6) set surround, three
The group operating mechanism is distributed on frame, and operating mechanism described in three groups controls the fire extinguishing of three engines respectively, described in every group
Operating mechanism includes that handle mechanism, triggering position-limit mechanism, gear simulation mechanism and electromagnet (17), the handle mechanism are worn
It crosses frame to connect with triggering position-limit mechanism and gear simulation mechanism successively, the triggering position-limit mechanism and lower tie plate (6)
It is fixedly connected, the gear simulation mechanism is fixedly connected with triggering position-limit mechanism, and the electromagnet (17) limits handle machine
Structure moves, and the electromagnet (17) is fixed on bottom plate (6), and the middle part control circuit board (5) receives engine
Signal on fire control the running of corresponding electromagnet (17), the middle part control circuit board (5) receives triggering position-limit mechanism
Signal is sent to terminal simulation extinguishing action.
2. a kind of simulation aircraft fire protection control panel manipulation device according to claim 1, it is characterised in that：The handle
Mechanism includes connection handle (4) and manipulates block (1), and the connection handle (4) sequentially passes through top tie plate (3), middle part control
Circuit board (5) processed and lower tie plate (6), the connection handle (4) top are fixedly connected with block (1) is manipulated, the company
Connecting handle (4) is equipped with limit card slot (401) with electromagnet (17) corresponding position, and the lower part of the connection handle (4) is successively
Across triggering position-limit mechanism and gear simulation mechanism.
3. a kind of simulation aircraft fire protection control panel manipulation device according to claim 2, it is characterised in that：The triggering
Position-limit mechanism includes triggering tabletting (8), left and right gear trigger switch (7) (18), limited block (9) and upper and lower gear trigger switch
(10), the triggering tabletting (8) is installed on connection handle (4), and the left and right gear trigger switch (7) (18) is fixed
Upper surface in limited block (9), and be arranged in the both sides of triggering tabletting (8), the trigger switch of gear up and down (10) is fixed
Lower surface in limited block (9), and be arranged in the bottom of triggering tabletting (8), the limited block (9) is equipped with triggering tabletting limit
Position slot (901), the slot bottom of the triggering tabletting limiting slot (901) offer the through hole (902) of connection handle (4) and upper and lower
The first receiving opening (903) of the tabletting of gear trigger switch (10).
4. a kind of simulation aircraft fire protection control panel manipulation device according to claim 3, it is characterised in that：The gear
Simulation mechanism includes gear simulated block (12), gear simulation fixed block (13), two springs (14), two steel balls (15) and two
Anticreep tabletting (16), gear simulation fixed block (13) are installed in the lower surface of limited block (9), and gear simulation is solid
Determine to be equipped with resettlement groove (1301) in the middle part of block (13), the gear simulated block (12) setting is described in resettlement groove (1301)
The middle part of gear simulated block (12) is equipped with the perforative slotted hole (1201) for accommodating connection handle (4), the gear simulated block
(12) both sides are arranged with waveform tooth (1202), and described gear simulated block (12) both sides pass through a steel ball (15), one
Spring (14) and an anticreep tabletting (16) offset with corresponding waveform tooth (1202).
5. a kind of simulation aircraft fire protection control panel manipulation device according to claim 4, it is characterised in that：Described in two
Anticreep tabletting (16) be separately fixed at the both sides of gear simulation fixed block (13), the both ends difference of the spring (14)
It offsets with the steel ball (15) of respective side and anticreep tabletting (16).
6. a kind of simulation aircraft fire protection control panel manipulation device according to claim 5, it is characterised in that：The gear
Simulation fixed block (13) is internally provided with the second receiving opening (1302) for placing spring (14) and steel ball (15).
7. a kind of simulation aircraft fire protection control panel manipulation device according to claim 1 or 6, it is characterised in that：It is described
Manipulation device further includes three override buttons (2), and each override button (2) corresponds to one group of operating mechanism, described in three
On the fixed top tie plate (3) of override button (2).
8. a kind of simulation aircraft fire protection control panel manipulation device according to claim 6, it is characterised in that the connection
Handle (4) is adapted from connection triggering tabletting (8) to the shape of end and slotted hole (1201) size.
9. a kind of simulation aircraft fire protection control panel manipulation device according to claim 7, it is characterised in that：The electromagnetism
Iron (17) is equipped with the spacer pin (1701) coordinated with limit card slot (401), and Self-resetting is arranged on the spacer pin (1701)
Spring.
10. a kind of simulation aircraft fire protection control panel manipulation device according to claim 9, it is characterised in that：On described
Lower gear trigger switch (10) is fixed on the lower surface of limited block (9) by connecting plate (11).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810234808.4A CN108288416B (en) | 2018-03-21 | 2018-03-21 | Control device for simulating fireproof control panel of airplane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810234808.4A CN108288416B (en) | 2018-03-21 | 2018-03-21 | Control device for simulating fireproof control panel of airplane |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN108288416A true CN108288416A (en) | 2018-07-17 |
| CN108288416B CN108288416B (en) | 2024-04-02 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810234808.4A Active CN108288416B (en) | 2018-03-21 | 2018-03-21 | Control device for simulating fireproof control panel of airplane |
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| Country | Link |
|---|---|
| CN (1) | CN108288416B (en) |
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| CN106289763A (en) * | 2016-08-22 | 2017-01-04 | 北京理工大学 | A kind of automatic unlocking mechanism for universal self shifter assay device |
| CN207097272U (en) * | 2016-08-24 | 2018-03-13 | 信阳泰蓝仿真科技有限公司 | One kind emulation fire extinguishing hydraulic fuel combination control box |
| CN208689778U (en) * | 2018-03-21 | 2019-04-02 | 哈尔滨莱特兄弟飞行技术有限公司 | A kind of simulation aircraft fire protection control panel manipulation device |
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