CN208530867U - A kind of continuous catapult-launching gear of side arm-type multiple degrees of freedom unmanned plane - Google Patents
A kind of continuous catapult-launching gear of side arm-type multiple degrees of freedom unmanned plane Download PDFInfo
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- CN208530867U CN208530867U CN201820870313.6U CN201820870313U CN208530867U CN 208530867 U CN208530867 U CN 208530867U CN 201820870313 U CN201820870313 U CN 201820870313U CN 208530867 U CN208530867 U CN 208530867U
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- sliding slot
- pedestal
- motor
- ejection
- telescopic rod
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Abstract
The utility model discloses a kind of continuous catapult-launching gear of side arm-type multiple degrees of freedom unmanned plane, belonging to includes adjustment mechanism, ejection mechanism, transport mechanism and control module；Adjustment mechanism includes base station, turntable, pedestal, side arm, overarm, first motor, driving gear, the first electric telescopic rod and the second electric telescopic rod；Ejection mechanism includes sliding slot, sliding block, first position sensor, second position sensor, telescoping mechanism and electromagnet；Transport mechanism includes the second motor, home roll axis, from roll shaft and conveyer belt.The utility model realizes the continuous batch ejection of Shipborne UAV, in the case where unmanned interference, automatically grab unmanned plane, adjust the direction of the launch and angle, continuously launched, solve the problems, such as deck unmanned aerial vehicle ejecting can only single ejection and ejection cycle it is long, while also solving the problems, such as in ejection process based on being difficult to change direction of ejection.
Description
Technical field
The utility model relates to unmanned plane fields more particularly to a kind of side arm-type multiple degrees of freedom unmanned plane continuously to launch dress
It sets.
Background technique
Traditional unmanned aerial vehicle ejecting frame is generally positioned on ground or carrier loader, under the set ejection angle of attack, by people
Unmanned plane is erected in the motorcycle above launching cradle by power, and coaster drives unmanned plane to fast forward through until taking off, and later, is slided
Vehicle resets, and next frame unmanned plane, which is carried on, to be come, and continues to launch operation.Whole process must have staff's participation, and each bullet
A frame unmanned plane can only be emitted by penetrating, and EJECTION INTERVAL is longer.
In addition, wind speed and wind direction are the factor for having to consider, tradition on sea when carrying out ejection operation above deck
Unmanned aerial vehicle ejecting frame carries out being difficult to change direction of ejection and flip angle when ejection operation above deck, this is just significantly reduced
The efficiency that deck is fought.
Utility model content
Technical problem to be solved in the utility model is to provide a kind of side for defect involved in background technique
The arm-type continuous catapult-launching gear of multiple degrees of freedom unmanned plane.
The utility model uses following technical scheme to solve above-mentioned technical problem:
A kind of continuous catapult-launching gear of side arm-type multiple degrees of freedom unmanned plane, comprising adjustment mechanism, ejection mechanism, transport mechanism and
Control module；
The adjustment mechanism includes base station, turntable, pedestal, side arm, overarm, first motor, driving gear, first electronic stretches
Contracting bar and the second electric telescopic rod；
The turntable is cylindrical, and lower end surface is connected by bearing with the pedestal, being capable of the relatively described pedestal freedom
Rotation, and a circle rack gear is circumferentially on the side wall of turntable；
The first motor is arranged on the base station, and the shaft of output shaft and the driving gear is connected, the master
Rack gear engagement on moving gear and the table side, the first motor is for controlling the turntable rotation；
The pedestal setting is fixedly linked with the turntable on the turntable；
Described side arm one end and the pedestal are hinged, and one end of the other end and the overarm is hinged, the overarm it is another
End and the ejection mechanism are connected；
First electric telescopic rod one end and the pedestal are hinged, the other end and described side walls hinged, for adjusting
State the angle between side arm and the pedestal；
Second electric telescopic rod one end and the overarm are hinged, and the other end and the pedestal are hinged, for adjusting
State the angle between overarm and the side wall；
The ejection mechanism includes sliding slot, sliding block, first position sensor, second position sensor, telescoping mechanism and electricity
Magnet；
The sliding slot and the other end of the overarm are connected, and the angle of the sliding slot and horizontal plane is more than or equal to preset
Angle threshold；
The sliding block is arranged in the sliding slot, can be free to slide in the sliding slot；
The sliding slot both ends are equipped with the stop mechanism for preventing the sliding block from skidding off；
The first position sensor, second position sensor are separately positioned on the both ends of the sliding slot, and described first
Sensor is set for incuding the end whether sliding block is in sliding slot, second position sensor is for incuding the sliding block
Whether the head end of the sliding slot is in；
On the slide block, telescopic end and the electromagnet are connected for the telescoping mechanism setting；
The transport mechanism is used to for unmanned plane being sent to immediately below the sliding block, comprising the second motor, home roll axis, from roller
Axis and conveyer belt；
The output shaft of second motor and the home roll axis are connected, for driving the home roll axis to rotate；
The home roll axis by the transmission belt and it is described from roll shaft be drivingly connected；
The control module respectively with the first motor, the first electric telescopic rod, the second electric telescopic rod, first position
Sensor, second position sensor, telescoping mechanism, electromagnet, the second motor are electrically connected.
As a kind of further prioritization scheme of continuous catapult-launching gear of side arm-type multiple degrees of freedom unmanned plane of the utility model, institute
Stating preset angle threshold is 30 °.
The workflow of the utility model is as follows:
Step 1), control module control the work of the second motor, the unmanned plane on conveyer belt are sent to immediately below sliding block, this
When sliding block be in the end of sliding slot；
Step 2, control module control telescoping mechanism work, electromagnet are lowered on unmanned plane；
Step 3), control mould can control work of electromagnet, unmanned plane are adsorbed on electromagnet；
Step 4), control module controls telescoping mechanism and shrinks, so that electromagnet is close to sliding block；
Step 6), control module control first motor, the first electric telescopic rod, the work of the second electric telescopic rod, pass through tune
Turn over platform, side arm, overarm adjust to the launch angle of unmanned plane；
Step 7), unmanned plane during flying, band movable slider slide in sliding slot, and when sliding block reaches the head end of sliding slot, second is passed
Sensor passes information to the control module, and control module control electromagnet stops working, and unmanned plane transmitting is completed；
Step 8), control module control turntable, side arm, overarm reset；
Step 9), sliding block are slid by self gravity to the end of sliding slot.
The utility model compared with the prior art by using the above technical solution, has following technical effect that
1. realizing the ejection of unmanned plane continuous batch, solve the problems, such as that traditional unmanned aerial vehicle ejector ejection cycle is longer；
2. direction of ejection and angle can be adjusted at any time when ejection, solves and different wind directions are difficult to wind speed above deck
The problem of adjusting the direction of the launch.
3. realizing the unmanned interference of automation, saves supernumerary person when battleship deck is fought and transfer.
Detailed description of the invention
Fig. 1 is the structural schematic diagram of the utility model；
Fig. 2 is the structural schematic diagram that adjustment mechanism and sliding slot match in the utility model；
Fig. 3 is the structural schematic diagram of transmission device in the utility model.
In figure, 1- base station, 2- pedestal, 3- side arm, 4- overarm, the first electric telescopic rod of 5-, the second electric telescopic rod of 6-, 7-
Sliding slot, 8- sliding block, 9- telescoping mechanism, 10- electromagnet, 11- conveyer belt, the second motor of 12-, 13- unmanned plane.
Specific embodiment
The technical solution of the utility model is described in further detail with reference to the accompanying drawing:
The utility model can be embodied in many different forms, and should not be assumed that be limited to the embodiments described herein.
On the contrary, it is thorough and complete to these embodiments are provided so that the disclosure, and this reality will be given full expression to those skilled in the art
With novel range.In the accompanying drawings, for the sake of clarity it is exaggerated component.
As shown in Figure 1, the utility model discloses a kind of continuous catapult-launching gear of side arm-type multiple degrees of freedom unmanned plane, comprising adjusting
Complete machine structure, ejection mechanism, transport mechanism and control module.
As shown in Fig. 2, the adjustment mechanism include base station, turntable, pedestal, side arm, overarm, first motor, driving gear,
First electric telescopic rod and the second electric telescopic rod；
The turntable is cylindrical, and lower end surface is connected by bearing with the pedestal, being capable of the relatively described pedestal freedom
Rotation, and a circle rack gear is circumferentially on the side wall of turntable；
The first motor is arranged on the base station, and the shaft of output shaft and the driving gear is connected, the master
Rack gear engagement on moving gear and the table side, the first motor is for controlling the turntable rotation；
The pedestal setting is fixedly linked with the turntable on the turntable；
Described side arm one end and the pedestal are hinged, and one end of the other end and the overarm is hinged, the overarm it is another
End and the ejection mechanism are connected；
First electric telescopic rod one end and the pedestal are hinged, the other end and described side walls hinged, for adjusting
State the angle between side arm and the pedestal；
Second electric telescopic rod one end and the overarm are hinged, and the other end and the pedestal are hinged, for adjusting
State the angle between overarm and the side wall.
The ejection mechanism includes sliding slot, sliding block, first position sensor, second position sensor, telescoping mechanism and electricity
Magnet；
The sliding slot and the other end of the overarm are connected, and the angle of the sliding slot and horizontal plane is more than or equal to preset
Angle threshold；
The sliding block is arranged in the sliding slot, can be free to slide in the sliding slot；
The sliding slot both ends are equipped with the stop mechanism for preventing the sliding block from skidding off；
The first position sensor, second position sensor are separately positioned on the both ends of the sliding slot, and described first
Sensor is set for incuding the end whether sliding block is in sliding slot, second position sensor is for incuding the sliding block
Whether the head end of the sliding slot is in；
On the slide block, telescopic end and the electromagnet are connected for the telescoping mechanism setting.
As shown in figure 3, the transport mechanism is used to for unmanned plane being sent to immediately below the sliding block, comprising the second motor,
Home roll axis, from roll shaft and conveyer belt；
The output shaft of second motor and the home roll axis are connected, for driving the home roll axis to rotate；
The home roll axis by the transmission belt and it is described from roll shaft be drivingly connected；
The control module respectively with the first motor, the first electric telescopic rod, the second electric telescopic rod, first position
Sensor, second position sensor, telescoping mechanism, electromagnet, the second motor are electrically connected.
As a kind of further prioritization scheme of continuous catapult-launching gear of side arm-type multiple degrees of freedom unmanned plane of the utility model, institute
Stating preset angle threshold is 30 °.
The workflow of the utility model is as follows:
Step 1), control module control the work of the second motor, the unmanned plane on conveyer belt are sent to immediately below sliding block, this
When sliding block be in the end of sliding slot；
Step 2, control module control telescoping mechanism work, electromagnet are lowered on unmanned plane；
Step 3), control mould can control work of electromagnet, unmanned plane are adsorbed on electromagnet；
Step 4), control module controls telescoping mechanism and shrinks, so that electromagnet is close to sliding block；
Step 6), control module control first motor, the first electric telescopic rod, the work of the second electric telescopic rod, pass through tune
Turn over platform, side arm, overarm adjust to the launch angle of unmanned plane；
Step 7), unmanned plane during flying, band movable slider slide in sliding slot, and when sliding block reaches the head end of sliding slot, second is passed
Sensor passes information to the control module, and control module control electromagnet stops working, and unmanned plane transmitting is completed；
Step 8), control module control turntable, side arm, overarm reset；
Step 9), sliding block are slid by self gravity to the end of sliding slot.
Those skilled in the art can understand that unless otherwise defined, all terms used herein (including skill
Art term and scientific term) there is meaning identical with the general understanding of those of ordinary skill in the utility model fields
Justice.It should also be understood that those terms such as defined in the general dictionary should be understood that with upper with the prior art
The consistent meaning of meaning hereinafter, and unless defined as here, will not with idealization or meaning too formal come
It explains.
Above-described specific embodiment, to the purpose of this utility model, technical scheme and beneficial effects carried out into
One step is described in detail, it should be understood that being not used to limit the foregoing is merely specific embodiment of the present utility model
The utility model processed, within the spirit and principle of the utility model, any modification, equivalent substitution, improvement and etc. done,
It should be included within the scope of protection of this utility model.
Claims (2)
1. a kind of continuous catapult-launching gear of side arm-type multiple degrees of freedom unmanned plane, which is characterized in that comprising adjustment mechanism, ejection mechanism,
Transport mechanism and control module；
The adjustment mechanism includes base station, turntable, pedestal, side arm, overarm, first motor, driving gear, the first electric telescopic rod
With the second electric telescopic rod；
The turntable is cylindrical, and lower end surface is connected by bearing with the pedestal, can the relatively described pedestal be freely rotated,
And a circle rack gear is circumferentially on the side wall of turntable；
The first motor is arranged on the base station, and the shaft of output shaft and the driving gear is connected, the driving tooth
Rack gear engagement on wheel and the table side, the first motor is for controlling the turntable rotation；
The pedestal setting is fixedly linked with the turntable on the turntable；
Described side arm one end and the pedestal are hinged, and one end of the other end and the overarm is hinged, the other end of the overarm and
The ejection mechanism is connected；
First electric telescopic rod one end and the pedestal are hinged, the other end and described side walls hinged, for adjusting the side
Angle between arm and the pedestal；
Second electric telescopic rod one end and the overarm are hinged, and the other end and the pedestal are hinged, described outstanding for adjusting
Angle between beam and the side wall；
The ejection mechanism includes sliding slot, sliding block, first position sensor, second position sensor, telescoping mechanism and electromagnet；
The sliding slot and the other end of the overarm are connected, and the angle of the sliding slot and horizontal plane is more than or equal to preset angle
Threshold value；
The sliding block is arranged in the sliding slot, can be free to slide in the sliding slot；
The sliding slot both ends are equipped with the stop mechanism for preventing the sliding block from skidding off；
The first position sensor, second position sensor are separately positioned on the both ends of the sliding slot, and the first position passes
Sensor is for incuding the end whether sliding block is in sliding slot, and whether second position sensor is for incuding the sliding block
Head end in the sliding slot；
On the slide block, telescopic end and the electromagnet are connected for the telescoping mechanism setting；
The transport mechanism is used to for unmanned plane being sent to immediately below the sliding block, comprising the second motor, home roll axis, from roll shaft and
Conveyer belt；
The output shaft of second motor and the home roll axis are connected, for driving the home roll axis to rotate；
The home roll axis by the conveyer belt and it is described from roll shaft be drivingly connected；
The control module is sensed with the first motor, the first electric telescopic rod, the second electric telescopic rod, first position respectively
Device, second position sensor, telescoping mechanism, electromagnet, the second motor are electrically connected.
2. the continuous catapult-launching gear of side arm-type multiple degrees of freedom unmanned plane according to claim 1, which is characterized in that described default
Angle threshold be 30 °.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820870313.6U CN208530867U (en) | 2018-06-06 | 2018-06-06 | A kind of continuous catapult-launching gear of side arm-type multiple degrees of freedom unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820870313.6U CN208530867U (en) | 2018-06-06 | 2018-06-06 | A kind of continuous catapult-launching gear of side arm-type multiple degrees of freedom unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208530867U true CN208530867U (en) | 2019-02-22 |
Family
ID=65381163
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820870313.6U Withdrawn - After Issue CN208530867U (en) | 2018-06-06 | 2018-06-06 | A kind of continuous catapult-launching gear of side arm-type multiple degrees of freedom unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208530867U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108750134A (en) * | 2018-06-06 | 2018-11-06 | 南京航空航天大学 | A kind of continuous catapult-launching gear of side arm-type multiple degrees of freedom unmanned plane |
-
2018
- 2018-06-06 CN CN201820870313.6U patent/CN208530867U/en not_active Withdrawn - After Issue
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108750134A (en) * | 2018-06-06 | 2018-11-06 | 南京航空航天大学 | A kind of continuous catapult-launching gear of side arm-type multiple degrees of freedom unmanned plane |
| CN108750134B (en) * | 2018-06-06 | 2023-09-26 | 南京航空航天大学 | Continuous catapulting device of side arm type multi-degree-of-freedom unmanned aerial vehicle |
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| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| AV01 | Patent right actively abandoned | ||
| AV01 | Patent right actively abandoned | ||
| AV01 | Patent right actively abandoned |
Granted publication date: 20190222 Effective date of abandoning: 20230926 |
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| AV01 | Patent right actively abandoned |
Granted publication date: 20190222 Effective date of abandoning: 20230926 |