CN207433832U - A kind of small-sized launching cradle of unmanned plane - Google Patents
A kind of small-sized launching cradle of unmanned plane Download PDFInfo
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- CN207433832U CN207433832U CN201721026046.6U CN201721026046U CN207433832U CN 207433832 U CN207433832 U CN 207433832U CN 201721026046 U CN201721026046 U CN 201721026046U CN 207433832 U CN207433832 U CN 207433832U
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- unmanned plane
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- launching cradle
- slideway
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Abstract
The utility model provides a kind of small-sized launching cradle of unmanned plane, belongs to unmanned air vehicle technique field.Purpose is to solve the problems, such as that unmanned aerial vehicle ejecting frame can not realize the adjustment of support angle in the prior art.The utility model provides a kind of small-sized launching cradle of unmanned plane, and including shot trolley, front support frame, rear support frame, the front support frame is A-frame, and the support angle of the A-frame is adjustable.The utility model designs a kind of small-sized launching cradle of unmanned plane, by the improvement of front support frame, realizes that support angle is adjustable, unmanned function is made to take off and realize the demand of special heading control under complicated surface condition.By being further improved for shot trolley structure, make launching cradle overall structure lighter, be more advantageous to control of taking off.
Description
Technical field
The utility model is related to unmanned air vehicle technique fields, particularly relate to a kind of small-sized launching cradle of unmanned plane.
Background technology
UAV referred to as " unmanned plane ", is manipulated using radio robot and the presetting apparatus provided for oneself
Not manned aircraft.Without cockpit on machine, but the equipment such as automatic pilot, presetting apparatus are installed.On ground, naval vessels or
Machine tool remote control station personnel are by equipment such as radars, to it into line trace, positioning, remote control, telemetering and Digital Transmission.It can be in radio
It takes off as conventional airplane or is launched with booster rocket under remote control, can also take aerial launch to by machine tool and fly.Recycling
When, the mode automatic Landing as conventional airplane landing mission can be used, can also be recycled by remote control parachute or block.It can
It is reused several times.It is widely used in aerial reconnaissance, monitoring, communication, antisubmarine, electronic interferences etc..
It is the most commonly used application of current unmanned plane to take photo by plane, and for unmanned plane when taking off, major way is that ejection type takes off, and is needed
To realize in current existing launching cradle, mainly having a pneumatic type and elastic force takes off two ways, the knot of pneumatic type by launching cradle
Structure is complicated, and cost is higher, and what unmanned plane of more taking photo by plane used is all that elastic force takes off form.
Due to the needs limited be subject to surface condition when taking off and heading controls, launching cradle is generally required
Support angle is adjustable, and existing launching cradle product due to the limitation of structure, can not realize the adjustment of support angle.
Utility model content
The technical problems to be solved in the utility model is that unmanned aerial vehicle ejecting frame can not realize support angle in the prior art
The problem of adjustment.
In order to solve the above technical problems, the utility model provides a kind of small-sized launching cradle of unmanned plane, including shot trolley, preceding
Supporting rack, rear support frame, the front support frame are A-frame, and the support angle of the A-frame is adjustable.
Further, the A-frame is connected by connecting axostylus axostyle with shot trolley front end, A-frame and connecting shaft
Bar is hinged, and articulated shaft is set with being connected axostylus axostyle angle of inclination, and three cradling pieces of A-frame are telescopic rod.
Further, the articulated shaft is in 70 degree to 80 degree of angle with the axis direction for being connected axostylus axostyle.
Further, angle locking knob and length locking wrench are additionally provided on the A-frame.
Further, the shot trolley includes slideway, coaster, hoisting mechanism, rubber band, rubber band bend wheel, /V
Block, coaster are mounted on slideway, and hoisting mechanism is mounted on slideway tail end, after rubber band bypasses rubber band bend wheel, both ends difference
Connect coaster and hoisting mechanism.
Further, the limited block includes two rubber blocks mounted on slideway front end.
Further, the slideway is made of channel steel, and slideway structure is accordion structure.
Further, the hoisting mechanism includes shaft, roll, handle, shaft connection handle, and roll is used to wind
Rubber band, shaft are engaged with roll by gear mechanism.
Further, it is additionally provided with locking bail on the gear of the shaft.
Further, the coaster is equipped with unmanned plane connection-peg and two inserted links, the afterbody of coaster are also connected with locking hole
Plate is locked and set on orifice plate there are two jack, and two inserted links are used for through jack and are inserted into slideway and lock coaster.
The above-mentioned technical proposal of the utility model has the beneficial effect that：
In said program, a kind of small-sized launching cradle of unmanned plane is designed, by the improvement of front support frame, realizes support angle
It is adjustable, unmanned function is made to take off and realize the demand of special heading control under complicated surface condition.Pass through bullet
Being further improved for vehicle structure is penetrated, makes launching cradle overall structure lighter, is more advantageous to control of taking off.
Description of the drawings
Fig. 1 is the overall structure diagram of the small-sized launching cradle of unmanned plane of the utility model；
Fig. 2 is the structure diagram of front support frame；
Fig. 3 is the structure diagram of limited block；
Fig. 4 is the structure diagram of coaster；
Fig. 5 is the top view of Fig. 4；
Fig. 6 is the exterior view of hoisting mechanism；
Fig. 7 is the cut-away view of hoist engine；
Fig. 8 is hoist engine shaft and the connection diagram of roll；
Fig. 9 is the overall structure figure of rubber band.
[main element symbol description]
1st, shot trolley；2nd, front support frame；3rd, rear support frame；4th, axostylus axostyle is connected；5th, articulated shaft；6th, angle locking knob；
7th, length locking wrench；8th, slideway；9th, coaster；10th, hoisting mechanism；11st, rubber band；12nd, rubber band bend wheel；13rd, limited block；
14th, shaft；15th, roll；16th, handle；17th, locking bail；18th, unmanned plane connection-peg；19th, inserted link；20th, orifice plate is locked.
Specific embodiment
In order to make the technical problems, technical solutions and advantages to be solved by the utility model clearer, below in conjunction with attached drawing
And specific embodiment is described in detail.
The utility model is solves the problems, such as that launching cradle can not realize that the adjustment of support angle designs in the prior art.
As shown in Figure 1 and Figure 2, in the present embodiment, the small-sized launching cradle of unmanned plane mainly includes shot trolley 1, front support frame
2nd, more than 3 part of rear support frame, rear support frame are formed for two cradling pieces.
Improvements essentially consist in the A-frame that front support frame 2 is arranged to adjustable angle.
Concrete structure is connected for the front end of shot trolley 1 by connecting axostylus axostyle 4 with front support frame 2, and front support frame 2 passes through hinge
Spindle 5 is hinged on connection axostylus axostyle, and articulated shaft 5 and the angle that the axis for being connected axostylus axostyle 4 is in 70 degree to 80 degree, is as tilted
It is intersecting, while front support frame is A-frame, the length of the cradling piece of A-frame is adjustable, rotation and branch by articulated shaft 5
The length adjustment of hack lever can make launcher be adapted to various ground environments, when unmanned plane, which needs to control, takes off direction, also can
It meets the requirements.
Angle locking knob 6 and length locking wrench 7 are additionally provided on A-frame, after Support Position is adjusted, is used for
Lock angle and stent pole length.
In the present embodiment, improvement also is made that the structure of shot trolley 1 so that product structure more lightness, more
Convenient for manipulation, while ensure the stability of flight.
Shot trolley 1 includes slideway 8, coaster 9, hoisting mechanism 10, rubber band 11, rubber band bend wheel 12, limited block 13.
8 channel steels of slideway are made, and for convenience of storing, slideway 8 may be configured as foldable structure, be packed up together with front support frame 2
Storage.
As shown in figure 3, limited block 13 is two rubber blocks mounted on 8 front end of slideway, the effect of limited block is to stop
The coaster 9 of advance, unmanned plane depart from the realization of coaster 9 and take off.
As shown in Figure 4, Figure 5, coaster 9 can slide on slideway 8, and unmanned plane connection-peg 18, unmanned plane are provided on coaster 9
It is inserted in above, locking orifice plate 20 has been also connected in the afterbody of coaster 9, lock on orifice plate 20 that there are two jacks, two inserted links 19 to insert
Enter in jack, lock coaster 9, after extracting inserted link, unmanned plane enters takeoff condition.
As shown in Fig. 6, Fig. 7, Fig. 8, the effect of hoisting mechanism 10 is tightening rubber band 11, is that rubber band 11 generates elastic force,
The power to take off is provided.
Hoisting mechanism 10 is included through the shaft 14 of engaged gears and roll 15, and roll 15 is used to wind rubber band
11,14 outside of shaft is connected to handle 16, and the locking bail 17 for locking, locking bail 17 and inserted link are also provided in shaft 14
19 use as the control unit that takes off.
As shown in figure 9, around rubber band bend wheel 12 among rubber band 11, one end is connected on coaster, other end winding
On roll 15, rubber band 11 is the actuating unit of launching cradle.
The above is the preferred embodiment of the utility model, it is noted that for the ordinary skill of the art
For personnel, on the premise of principle described in the utility model is not departed from, several improvements and modifications can also be made, these improvement
The scope of protection of the utility model is also should be regarded as with retouching.
Claims (6)
- A kind of 1. small-sized launching cradle of unmanned plane, including shot trolley, front support frame, rear support frame, which is characterized in that branch before described Support is A-frame, and the support angle of the A-frame is adjustable；Wherein, the A-frame is connected by connecting axostylus axostyle with shot trolley front end, and A-frame is hinged with being connected axostylus axostyle, hinge Spindle is set with being connected axostylus axostyle angle of inclination, and three cradling pieces of A-frame are telescopic rod；Wherein, the articulated shaft is in 70 degree to 80 degree of angle with the axis direction for being connected axostylus axostyle；Wherein, angle locking knob and length locking wrench are additionally provided on the A-frame；Wherein, the shot trolley includes slideway, coaster, hoisting mechanism, rubber band, rubber band bend wheel, limited block, coaster peace On slideway, hoisting mechanism be mounted on slideway tail end, rubber band bypass rubber band bend wheel after, both ends connect respectively coaster and Hoisting mechanism.
- 2. the small-sized launching cradle of unmanned plane according to claim 1, which is characterized in that the limited block includes being mounted on slideway Two rubber blocks of front end.
- 3. the small-sized launching cradle of unmanned plane according to claim 1, which is characterized in that the slideway is made of channel steel, slideway Structure is accordion structure.
- 4. the small-sized launching cradle of unmanned plane according to claim 1, which is characterized in that the hoisting mechanism include shaft, around Spool, handle, shaft connection handle, for winding rubber band, shaft is engaged roll with roll by gear mechanism.
- 5. the small-sized launching cradle of unmanned plane according to claim 4, which is characterized in that lock is additionally provided on the gear of the shaft Tight hook.
- 6. the small-sized launching cradle of unmanned plane according to claim 1, which is characterized in that the coaster is equipped with unmanned plane grafting Head and two inserted links, the afterbody of coaster are also connected with locking orifice plate, lock and are set on orifice plate there are two jack, two inserted links be used for through Jack is simultaneously inserted into latching coaster in slideway.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721026046.6U CN207433832U (en) | 2017-08-16 | 2017-08-16 | A kind of small-sized launching cradle of unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721026046.6U CN207433832U (en) | 2017-08-16 | 2017-08-16 | A kind of small-sized launching cradle of unmanned plane |
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| Publication Number | Publication Date |
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| CN207433832U true CN207433832U (en) | 2018-06-01 |
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| CN201721026046.6U Active CN207433832U (en) | 2017-08-16 | 2017-08-16 | A kind of small-sized launching cradle of unmanned plane |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112193430A (en) * | 2020-09-29 | 2021-01-08 | 浙江安防职业技术学院 | Multi-degree-of-freedom energy-saving unmanned aerial vehicle launching system |
-
2017
- 2017-08-16 CN CN201721026046.6U patent/CN207433832U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112193430A (en) * | 2020-09-29 | 2021-01-08 | 浙江安防职业技术学院 | Multi-degree-of-freedom energy-saving unmanned aerial vehicle launching system |
| CN112193430B (en) * | 2020-09-29 | 2022-06-03 | 浙江安防职业技术学院 | Multi-degree-of-freedom energy-saving unmanned aerial vehicle launching system |
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