CN208349925U - A kind of quick device from cabin of simulated missile - Google Patents
A kind of quick device from cabin of simulated missile Download PDFInfo
- Publication number
- CN208349925U CN208349925U CN201820654051.XU CN201820654051U CN208349925U CN 208349925 U CN208349925 U CN 208349925U CN 201820654051 U CN201820654051 U CN 201820654051U CN 208349925 U CN208349925 U CN 208349925U
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- CN
- China
- Prior art keywords
- lever
- shaft
- screw
- cabin
- sliding block
- 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.)
- Expired - Fee Related
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- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
The utility model provides a kind of simulated missile quickly device from cabin, belong to weapon simulated training instrument technical field, mainly solve the problems, such as in simulated missile 0.5 second from cabin, including cylinder, transmission mechanism, lever mechanism and the slide block mechanism being made of sliding block and movable slider, its main feature is that: the transmission mechanism includes lead screw and rectangular screw, and the lead screw is arranged bearing by both ends and is fixed in the cylinder；The lever mechanism includes lever seat, lever and shaft, the lever is provided through the via hole of shaft at fulcrum, the shaft is fixed on the lever seat, the lever is movably connected on lever seat by shaft, using shaft as boundary on lever, lever is divided into quarter butt and stock two parts, wherein quarter butt part is connect by pin shaft with sliding block, and stem portion is connect by pin shaft with rectangular screw；The sliding block is linked into an integrated entity by screw and the movable slider for making identification contact in place discharge or connect.
Description
Technical field
The utility model belongs to weapon simulated training instrument technical field, and in particular to a kind of simulated missile is quickly from cabin
Device.
Background technique
A kind of simulation trainer for substitution that we develop now, the training aids will simulate true bullet engine ignition, hair
It penetrates and from cabin whole state.
Hair frame (transmitter) is led in simulation trainer loading, is carried out analog transmissions training after reaching designated place and height, is pressed
After dynamic MISSILE LAUNCHING button, guided missile is in 0.5 second " fly away from " transmitter, hit that makes a return voyage after set objective
Because guided missile will fly away from transmitter, and simulation trainer is to want Reusability not after really playing successful launch
Really leave transmitter, thus just face one how simulated missile fly away from state project we should guarantee simulator
Being reliably fixed in the transmitter will also show the screen display guided missile no longer transmitter in emission state after aircraft transmitting
In correct status otherwise, display state be the Missile Fault, fail from cabin
Simulated missile is very simple from cabin, but wants in simulated missile 0.5 second from cabin to be then a big problem guided missile cannot
It is dynamic, guided missile stowage of making an issue of on contact can only be identified in guided missile, identification contact is jacked up, and for guided missile from cabin, we can only do one
The sliding block that can be moved up and down is allowed to fall, and discharges identification switch, and electric signal is made to reach display panel, expresses guided missile from cabin
With inclined plane slide block mechanism, sliding block needs tension spring when falling, in the cylinder of a diameter 60mm, should sliding block it is enough
Greatly to cover the identification contact of seven sticking positions, there is sufficient space just somewhat unable to do what one wishes to place spring again, tension spring is too small, draws
Power and curtailment are very easy to failure to cope with
With cam slide mechanism, it is desired to there is accurate step motor control and motor cannot be too high-power, otherwise 7
Platform moves at the same time electric current greatly to the unbearable of power supply on aircraft and stepper motor just starts to have step-out phenomenon, does not accomplish accurate
90 degree of rotation.
Summary of the invention
The purpose of this utility model is to solve the problems, such as that simulation is true to play engine ignition, transmitting and from cabin whole state, mention
For a kind of quick device from cabin of simulated missile.
To achieve the goals above, the technical solution of the utility model is:
A kind of quick device from cabin of simulated missile, including cylinder, transmission mechanism, lever mechanism and by sliding block and activity
The slide block mechanism that sliding block is constituted, its main feature is that: the transmission mechanism includes lead screw and rectangular screw, and the lead screw is set by both ends
Bearing is set to be fixed in the cylinder；The lever mechanism includes lever seat, lever and shaft, and the lever is arranged at fulcrum
There is the via hole across shaft, the shaft is fixed on the lever seat, and the lever is movably connected in lever seat by shaft
On, using shaft as boundary on lever, lever is divided into quarter butt and stock two parts, wherein quarter butt part passes through pin shaft and sliding block
Connection, stem portion are connect by pin shaft with rectangular screw；The sliding block passes through screw and is used to make to identify that contact is released in place
The movable slider put or connected links into an integrated entity.
The beneficial effects of the utility model are:
The use laborsaving lever mechanism and lead-screw drive mechanism of the utility model use thick stick using most economical power of motor
Bar amplifies its power effect, has accomplished that small machine completes the effect that big task is got twice the result with half the effort, solve in simulated missile 0.5 second from
The state in cabin.
Detailed description of the invention
Fig. 1 is that the utility model stereochemical structure casts aside schematic diagram；
Fig. 2 is the utility model simulated missile from storehouse status diagram；
Fig. 3 is the utility model simulated missile status diagram in place.
In figure: 1-lever seat；2-levers；3-rectangular screws；4-lead screws；5-shafts；6-sliding blocks；7-activities
Sliding block；8-cylinders.
Specific embodiment
Specific embodiment of the present utility model is described in detail below in conjunction with attached drawing
As shown in Figure 1, Figure 2 and Figure 3, a kind of simulated missile quickly device from cabin, including cylinder 8, transmission mechanism, lever
Mechanism and the slide block mechanism being made of sliding block 6 and movable slider 7, its main feature is that: the transmission mechanism includes lead screw 4 and rectangular
Screw 3, the lead screw 4 are arranged bearing by both ends and are fixed in the cylinder 8；The lever mechanism includes lever seat 1, lever
2 and shaft 5, the lever 2 via hole of shaft 5 is provided through at fulcrum, the shaft 5 is fixed on the lever seat 1,
The lever 2 is movably connected on lever seat 1 by shaft 5, with shaft 5 is boundary on lever 2, lever 2 is divided for quarter butt and
Stock two parts, wherein quarter butt part is connect by pin shaft with sliding block 6, and stem portion is connect by pin shaft with rectangular screw 3；
The sliding block 6 is linked into an integrated entity by screw and the movable slider 7 for making identification contact in place discharge or connect.
The lever mechanism includes being arranged symmetrically two sets of lever mechanisms in lead screw two sides along 4 direction of lead screw.
Utility model works process:
Motor drives lead screw 4 by shaft coupling pin, and the rotation of lead screw 4 drives rectangular screw 3 to be moved forward or rearward.It is rectangular
2 stock of lever, 5 rotation around the shaft counterclockwise is driven when screw 3 moves forward.2 quarter butt of lever, which rotates down, pulls movable slider 7
It moves down, makes to identify that contact discharges in place, realize from cabin.
Conversely, driving 2 stock of lever to rotate clockwise about shaft 5 when rectangular screw 3 moves backward.2 quarter butt of lever is upward
Rotation pushes movable slider 7 to move up, and makes to identify that contact is connected in place, realizes that guided missile is in place.
Claims (2)
1. a kind of quick device from cabin of simulated missile, including cylinder (8), transmission mechanism, lever mechanism and by sliding block (6) and
The slide block mechanism that movable slider (7) is constituted, it is characterized in that: the transmission mechanism includes lead screw (4) and rectangular screw (3), it is described
Lead screw (4) is arranged bearing by both ends and is fixed in the cylinder (8)；The lever mechanism includes lever seat (1), lever (2)
And shaft (5), the lever (2) are provided through the via hole of shaft (5) at fulcrum, the shaft (5) is fixed on the thick stick
On pole socket (1), the lever (2) is movably connected on lever seat (1) by shaft (5), is with shaft (5) on lever (2)
Lever (2) is divided into quarter butt and stock two parts by boundary, and wherein quarter butt part is connect by pin shaft with sliding block (6), stem portion
It is connect by pin shaft with rectangular screw (3)；The sliding block (6) is by screw and for making to identify contact release in place or connect
Movable slider (7) link into an integrated entity.
2. the quick device from cabin of simulated missile according to claim 1, it is characterized in that: the lever mechanism includes along silk
Thick stick (4) direction, in two sets of lever mechanisms that lead screw two sides are arranged symmetrically.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820654051.XU CN208349925U (en) | 2018-05-04 | 2018-05-04 | A kind of quick device from cabin of simulated missile |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820654051.XU CN208349925U (en) | 2018-05-04 | 2018-05-04 | A kind of quick device from cabin of simulated missile |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208349925U true CN208349925U (en) | 2019-01-08 |
Family
ID=64886823
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820654051.XU Expired - Fee Related CN208349925U (en) | 2018-05-04 | 2018-05-04 | A kind of quick device from cabin of simulated missile |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208349925U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108413807A (en) * | 2018-05-04 | 2018-08-17 | 山西华洋吉禄科技股份有限公司 | A kind of simulated missile is quickly from the device in cabin |
-
2018
- 2018-05-04 CN CN201820654051.XU patent/CN208349925U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108413807A (en) * | 2018-05-04 | 2018-08-17 | 山西华洋吉禄科技股份有限公司 | A kind of simulated missile is quickly from the device in cabin |
| CN108413807B (en) * | 2018-05-04 | 2023-10-03 | 山西华洋吉禄科技股份有限公司 | Device for simulating missile to leave cabin rapidly |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20190108 Termination date: 20210504 |