CN205916345U - Small -size fixed wing uavs launching cradle - Google Patents
Small -size fixed wing uavs launching cradle Download PDFInfo
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- CN205916345U CN205916345U CN201620827964.8U CN201620827964U CN205916345U CN 205916345 U CN205916345 U CN 205916345U CN 201620827964 U CN201620827964 U CN 201620827964U CN 205916345 U CN205916345 U CN 205916345U
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Abstract
The utility model belongs to the technical field of unmanned air vehicle technique and specifically relates to a small -size fixed wing uavs launching cradle, including telescopic tripod mechanism with set up the unmanned aerial vehicle supporting mechanism in tripod mechanism upper end, the unmanned aerial vehicle supporting mechanism includes that bolt, T shape three way connection, carbon pipe and the spacing piece of wing are released fast to supporting seat, stay tube, T shape, the bilateral symmetry of supporting seat is provided with two first pin joint holes, the both sides of supporting seat still the symmetry be provided with two with the parallel second pin joint hole in first pin joint hole, the one end of stay tube is at first pin joint hole department and supporting seat pin joint, and T shape is released the bolt fast and is inserted second pin joint hole and make the stay tube can not fall down, T shape three way connection's perpendicular straight joint is connected to the other end of stay tube, and the carbon pipe is connected respectively to T shape three way connection's two hydraulic -couplings, the spacing piece of wing is cantilever structure, is used for being in the wing card between spacing piece of wing and the carbon pipe. The utility model discloses but fast assembly, small and conveniently carry.
Description
Technical field
This utility model is related to unmanned air vehicle technique field, especially a kind of small-sized fixed-wing unmanned aerial vehicle ejecting frame.
Background technology
Fixed-wing unmanned plane is generally used for the air taskings such as collection of data, aerial mapping, border patrol, police investigation.Can
Realize military surveillance, the multipurpose function such as Disaster Assessment, mapping are taken photo by plane, meteorological detection, aeroplane photography, town planning, simultaneously
Can be used for the non-military task such as flight test, aerial mapping.For more gyroplane, fixed-wing unmanned plane have efficiency high,
Working area is wide, boat duration and can more flexibly execute task.Take-off venue due to fixed-wing unmanned plane requires, because
This has very high requirement for body ejection mode, not only convenient and practical, and reliability and efficiency high.
Unmanned aerial vehicle ejecting frame is mainly responsible for successfully launching unmanned plane lift-off, thus taking off of safety, is stored up using rubber band
And can discharge and unmanned aerial vehicle ejecting is gone out, because having simple and practical, the saving unmanned plane energy itself, increasing airborne hours etc.
Advantage and extensively applied.Existing unmanned aerial vehicle ejecting frame is generally divided into ground and is used alone and is used alone two kinds of feelings with vehicle-mounted
Condition, assembly and disassembly process is complicated, makes troubles to the use of unmanned aerial vehicle ejecting frame；And the cylinder framework of launching cradle is mostly
Monoblock type and spliced, all relatively difficult in transport and erection.
Utility model content
The purpose of this utility model is to overcome existing unmanned aerial vehicle ejecting frame heaviness, be inconvenient to carry and assemble lacking of difficulty
Fall into, a kind of small-sized fixed-wing unmanned aerial vehicle ejecting frame portable, easy to assembly is provided.
This utility model solves its technical problem and be the technical scheme is that
A kind of small-sized fixed-wing unmanned aerial vehicle ejecting frame is it is characterised in that including telescopic spider mechanism and being arranged on
The unmanned plane supporting mechanism of described spider mechanism upper end；Described spider mechanism includes axis；Described unmanned plane supporting mechanism
Including support base, support tube, t shape quick release latch, t shape three way cock, carbon pipe and wing banking stop；Described support base center
It is fixed on the upper end of described axis, the both sides of described support base are symmetrically arranged with two first pin joint holes, the both sides of described support base
Also it is symmetrically arranged with two second pin joint holes parallel with described first pin joint hole, and the described second pin joint hole position in left side is in a left side
The upper left side in the described first pin joint hole of side, the upper right in the described second pin joint hole position on the right side described first pin joint hole in right side
Side；One end of described support tube at described first pin joint hole with described support base pin joint, the insertion of described t shape quick release latch
Described second pin joint hole supports described support tube not fall；The other end of described support tube connects vertically connecing of t shape three way cock
Head, two horizontal joints of described t shape three way cock connect carbon pipe respectively；Described wing banking stop is cantilever design, and one end is fixed
On the top of carbon pipe, the other end is inclined upwardly, for being stuck in wing between described wing banking stop and carbon pipe.
Further, described small-sized fixed-wing unmanned aerial vehicle ejecting frame also includes antenna mount, and described support base has antenna
Frame mounting blocks, the both sides of described antenna mount mounting blocks have flange, and described antenna mount is had the card being adapted with described flange
Groove.
Further, described spider mechanism also includes leg, strut and the fixed seat being fixed on described axis；Three
Described leg respectively with described fixed seat pin joint, at the middle part of described leg, other end pin joint exists one end pin joint of described strut
The bottom of described axis.
Further, described spider mechanism also includes fixing bolt, described fixing bolt pass through described fixed seat and with
Described axis is vertical, by tightening described fixing bolt, described fixed seat is fixed on axis, unscrewing described fixing bolt makes
Fixed seat moves up and down along described axis.
Further, described axis includes inner tube and the outer tube being set in outside said inner tube, and described outer tube is arranged on institute
State the bottom of inner tube, a bolt passes through the top of described outer tube and holds out against said inner tube, and inner tube is pulled out not from outer tube
Same length, then screwed in place bolt inner tube is fixed with outer tube.
Further, the bottom of described leg has the 3rd pin joint hole, passes through described 3rd pin joint hole by a pin
Step on switch with foot and described leg and described foot are stepped on switch fixation.
Compared with prior art, this utility model apparently has the advantages that
1st, during small-sized fixed-wing unmanned aerial vehicle ejecting frame dismounting of the present utility model, carbon pipe is pulled up from t shape three way cock, so
After pull up t shape quick release latch, support tube is fallen, finally packs up spider mechanism, can be by small-sized fixed-wing launching cradle
Quickly pack up, and small volume, light weight, be convenient for carrying.
2nd, small-sized fixed-wing unmanned aerial vehicle ejecting frame of the present utility model easily assemble, structure simple, greatly reduce cost,
And the preparation before unmanned plane during flying greatly reduces.
3rd, the antenna mount of installation antenna is detachably arranged on launching cradle and sets it is not necessary to being separately provided antenna again and installing
Standby, realize a frame multiplex.
4th, this utility model adopts folding spider mechanism, launching cradle Stability Analysis of Structures, and height adjustable.
5th, the bottom connecting pin of the leg of this utility model spider steps on switch, and foot is stepped on switch and fixed with ground, so that
Unmanned aerial vehicle ejecting frame is fixed, and one end of rubber band fixes on the ground, and the other end has two joints, and one of joint and foot are stepped on
Switch connects, and the ejection of another joint and unmanned plane abdominal part links and connects, and strains rubber band, then discharges foot and steps on the rubber on switch
Unmanned aerial vehicle ejecting is gone out by rubber band joint.Unmanned aerial vehicle ejecting reliability is high, and only need to fly handss one man operation can complete unmanned
The ejection of machine.
Brief description
With reference to the accompanying drawings and examples this utility model is further illustrated.
Fig. 1 is this utility model embodiment three-dimensional structure diagram；
Fig. 2 is this utility model embodiment front view；
Fig. 3 is support base front view；
Fig. 4 is that antenna mount mounting blocks are connected diagram with antenna mount；
Fig. 5 is this utility model embodiment to be stepped on switch with foot and is connected diagram.
In figure, 11, axis, 12, fixed seat, 13, leg, the 131, the 3rd pin joint hole, 14, strut, 15, fixing bolt, 16,
Bolt, 21, support base, the 211, first pin joint hole, the 212, second pin joint hole, 22, support tube, 23, t shape quick release inserts
Pin, 24, t shape three way cock, 241, vertical joint, 242, horizontal joint, 25, carbon pipe, 26, wing banking stop, 3, antenna mount peace
Dress block, 31, flange, 4, antenna mount, 41, draw-in groove, 5, foot step on switch, 6, pin, 7, fot screw.
Specific embodiment
In order that technical problem, technical scheme and beneficial effect that this utility model is solved become more apparent, below
In conjunction with drawings and Examples, this utility model is further elaborated.It should be appreciated that described herein be embodied as
Example only in order to explain this utility model, is not used to limit this utility model.
Of the present utility model description in it is to be understood that term " radially ", " axial ", " on ", D score, " top ",
The orientation of instruction such as " bottom ", " interior ", " outward " or position relationship are based on orientation shown in the drawings or position relationship, merely to just
In description this utility model and simplification description, rather than the device of instruction or hint indication or element must have specific side
Position, with specific azimuth configuration and operation, therefore it is not intended that to restriction of the present utility model.In description of the present utility model
In, unless otherwise stated, " multiple " are meant that two or more.
In description of the present utility model, it should be noted that unless otherwise clearly defined and limited, term " peace
Dress ", " setting ", " connection " should be interpreted broadly, for example, it may be being fixedly connected or being detachably connected, or integratedly
Connect；Can be to be joined directly together it is also possible to be indirectly connected to by intermediary.For the ordinary skill in the art,
Concrete meaning in this utility model for the above-mentioned term can be understood as the case may be.
Small-sized fixed-wing unmanned aerial vehicle ejecting frame as shown in Figure 1-Figure 3, including telescopic spider mechanism and being arranged on
The unmanned plane supporting mechanism of spider mechanism upper end.Spider mechanism is similar to camera trivets, scalable, foldable.Three feet
Frame mechanism includes 11, three legs 13 of axis, strut 14 and the fixed seat 12 being fixed on axis 11, fixed seat 12 can on move down
Dynamic, by through fixed seat 12 and fixed seat 12 is fixed by a fixing bolt 15 vertical with axis 11 with axis 11, logical
Cross and tighten fixing bolt 15 fixed seat 12 is fixed on axis 11, unscrewing fixing bolt 15 can make fixed seat 12 along along axis 11
Lower movement.Three legs 13 respectively with fixed seat 12 pin joint, one end pin joint of strut 14 is in the middle part of leg 13, other end pin joint
Bottom in axis 11.Axis 11 is Collapsible structure, and including inner tube and the outer tube being set in outside inner tube, outer tube is arranged on
The bottom of inner tube, bolt 16 passes through the top of outer tube to hold out against inner tube, inner tube is pulled out from outer tube different length, then
Inner tube is fixed by screwed in place bolt 16 with outer tube.
Unmanned plane supporting mechanism include support base 21, support tube 22, t shape quick release latch 23, t shape three way cock 24,
Carbon pipe 25 and wing banking stop 26；Support base 21 center is fixed on the upper end of axis 11, and support base 21 structure, referring to Fig. 3, supports
The both sides of seat 21 are symmetrically arranged with two first pin joint holes 211, and the both sides of support base 21 are also symmetrically arranged with two and the first pin joint
The second parallel pin joint hole 212 of hole 211, and the second pin joint hole 212 in left side is located at the upper left in the first pin joint hole 211 in left side
Side, the second pin joint hole 212 on right side is located at the upper right side in the first pin joint hole 211 on right side；One end of support tube 22 is in the first pin
Connect at hole 211 and support base 21 pin joint, t shape quick release latch 23 inserts the second pin joint hole 212 makes support tube 22 not fall out；
The other end of support tube 22 connects the vertical joint 241 of t shape three way cock 24,242 points of two horizontal joint of t shape three way cock 24
Lian Jie not carbon pipe 25；Wing banking stop 26 is cantilever design, and one end is fixed on the top of carbon pipe 25, and the other end is inclined upwardly, and uses
Wing is stuck between described wing banking stop 26 and carbon pipe 25.
The small-sized fixed-wing unmanned aerial vehicle ejecting frame of this utility model embodiment also includes antenna mount 4, and antenna is passed through antenna
Frame 4 is erected on launching cradle, referring to Fig. 1 and Fig. 4, support base 21 has antenna mount mounting blocks 3, and the two of antenna mount mounting blocks 3
Side has flange 31, and antenna mount 4 is had the draw-in groove 41 being adapted with flange 31, and flange 31 is slipped in draw-in groove 41, you can will
Antenna mount 4 is arranged on support base 21.Antenna mount 4 is detachably arranged on launching cradle it is not necessary to other antenna mount is installed
Equipment, realizes a frame multiplex.
Referring to Fig. 5, the bottom of leg 13 has the 3rd pin joint hole 131, passes through the 3rd pin joint hole 131 by a pin 6
Step on switch 5 with foot and leg 13 and foot are stepped on switch 5 fixation.
Specifically, before unmanned plane takes off, three legs 13 of launching cradle are strutted, by adjust fixed seat 12 height and in
The total height of the length adjustment launching cradle of axle 11, rotates up support tube 22, t shape quick release latch 23 is inserted second simultaneously
Pin joint hole 212, makes support tube 22 be located at the top of t shape quick release latch 23, without falling, then t shape three way cock 24
Two horizontal joints 242 on insert a carbon pipe 25 respectively, penetrate the 3rd pin joint hole 131 He of leg 13 bottom with pin 6
Foot steps on the pin joint portion on switch 5, launching cradle and foot is stepped on switch 5 and is fixed together, finally with fot screw 7, foot is stepped on switch 5
Fix on the ground.
One end of rubber band is fixed on the ground by a fot screw, and the other end has two joints, one of joint
It is connected to foot and steps on switch 5, the ejection that another joint is connected on unmanned plane ventral hooks.When unmanned plane needs to take off, will
Unmanned plane is placed on carbon pipe 25, and trailing edge is snapped between wing banking stop 26 and carbon pipe 25, strains rubber band, then steps on
Foot is stepped on switch 5 and is discharged connected joint, and unmanned aerial vehicle ejecting is gone out by rubber band.
Pack up during launching cradle it is only necessary to unload carbon pipe 25, pull up t shape quick release latch 23, support tube 22 is put down, so
Afterwards spider mechanism is packed up, the launching cradle small volume after packing up, be convenient for carrying.
Above-mentioned is enlightenment according to desirable embodiment of the present utility model, by above-mentioned description, relevant staff
Various change and modification can be carried out in the range of without departing from this utility model technological thought completely.This practicality
Content that new technical scope is not limited in description is it is necessary to determine it according to right technical
Scope.
Claims (6)
1. a kind of small-sized fixed-wing unmanned aerial vehicle ejecting frame is it is characterised in that including telescopic spider mechanism and being arranged on institute
State the unmanned plane supporting mechanism of spider mechanism upper end；Described spider mechanism includes axis (11)；Described unmanned plane supports machine
Structure includes support base (21), support tube (22), t shape quick release latch (23), t shape three way cock (24), carbon pipe (25) and machine
Wing banking stop (26)；Described support base (21) center is fixed on the upper end of described axis (11), the both sides of described support base (21)
It is symmetrically arranged with two first pin joint holes (211), the both sides of described support base (21) are also symmetrically arranged with two and sell with described first
Connect the second parallel pin joint hole (212) of hole (211), and the described second pin joint hole (212) in left side is located at described the first of left side
The upper left side in pin joint hole (211), the described second pin joint hole (212) on right side is located at the described first pin joint hole (211) on right side
Upper right side；One end of described support tube (22) is in described first pin joint hole (211) place and described support base (21) pin joint, described t
Shape quick release latch (23) inserts described second pin joint hole (212) makes described support tube (22) not fall out；Described support tube
(22) the other end connects the vertical joint (241) of t shape three way cock (24), and two levels of described t shape three way cock (24) connect
Head (242) connects carbon pipe (25) respectively；Described wing banking stop (26) is cantilever design, and one end is fixed on the upper of carbon pipe (25)
Portion, the other end is inclined upwardly, for being stuck in wing between described wing banking stop (26) and carbon pipe (25).
2. small-sized fixed-wing unmanned aerial vehicle ejecting frame according to claim 1 is it is characterised in that described small-sized fixed-wing is unmanned
Machine launching cradle also includes antenna mount (4), and described support base (21) has antenna mount mounting blocks (3), described antenna mount mounting blocks
(3) both sides have flange (31), and described antenna mount (4) is had the draw-in groove (41) being adapted with described flange (31).
3. small-sized fixed-wing unmanned aerial vehicle ejecting frame according to claim 1 is it is characterised in that described spider mechanism also wraps
Include leg (13), strut (14) and the fixed seat (12) being fixed on described axis (11)；Three described legs (13) respectively with
Described fixed seat (12) pin joint, at the middle part of described leg (13), other end pin joint is in institute for one end pin joint of described strut (14)
State the bottom of axis (11).
4. small-sized fixed-wing unmanned aerial vehicle ejecting frame according to claim 3 is it is characterised in that described spider mechanism also wraps
Include fixing bolt (15), described fixing bolt (15) is through described fixed seat (12) and vertical with described axis (11), by twisting
Tightly described fixed seat (12) is fixed on axis (11) described fixing bolt (15), and unscrewing described fixing bolt (15) makes admittedly
Reservation (12) moves up and down along described axis (11).
5. small-sized fixed-wing unmanned aerial vehicle ejecting frame according to claim 3 is it is characterised in that described axis (11) inclusion is interior
Manage and be set in the outer tube outside said inner tube, described outer tube is arranged on the bottom of said inner tube, and a bolt (16) passes through
The top of described outer tube simultaneously holds out against said inner tube, inner tube is pulled out from outer tube different length, then screwed in place bolt (16)
Inner tube is fixed with outer tube.
6. the small-sized fixed-wing unmanned aerial vehicle ejecting frame according to any one of claim 3-5 is it is characterised in that described leg
(13) bottom has the 3rd pin joint hole (131), passes through described 3rd pin joint hole (131) and foot to step on switch by a pin (6)
(5) described leg (13) and described foot are stepped on switch (5) fixing.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620827964.8U CN205916345U (en) | 2016-08-01 | 2016-08-01 | Small -size fixed wing uavs launching cradle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620827964.8U CN205916345U (en) | 2016-08-01 | 2016-08-01 | Small -size fixed wing uavs launching cradle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205916345U true CN205916345U (en) | 2017-02-01 |
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ID=57870051
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620827964.8U Active CN205916345U (en) | 2016-08-01 | 2016-08-01 | Small -size fixed wing uavs launching cradle |
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| CN (1) | CN205916345U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106005467A (en) * | 2016-08-01 | 2016-10-12 | 天峋（常州）智能科技有限公司 | Small fixed wing unmanned aerial vehicle ejector rack |
| US11279481B2 (en) | 2017-05-12 | 2022-03-22 | Phirst Technologies, Llc | Systems and methods for tracking, evaluating and determining a response to emergency situations using unmanned airborne vehicles |
-
2016
- 2016-08-01 CN CN201620827964.8U patent/CN205916345U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106005467A (en) * | 2016-08-01 | 2016-10-12 | 天峋（常州）智能科技有限公司 | Small fixed wing unmanned aerial vehicle ejector rack |
| US11279481B2 (en) | 2017-05-12 | 2022-03-22 | Phirst Technologies, Llc | Systems and methods for tracking, evaluating and determining a response to emergency situations using unmanned airborne vehicles |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20221228 Address after: Room 2211, 22nd Floor, Block D, Zhizhen Building, No. 7 Zhichun Road, Haidian District, Beijing 100088 Patentee after: TIANXUN INNOVATION (BEIJING) TECHNOLOGY CO.,LTD. Address before: 213000 A1, Changzhou science and education center, 18, Changwu Middle Road, Wujin District, Changzhou, Jiangsu. Patentee before: VOLITATION (CHANGZHOU) INTELLIGENT TECHNOLOGY CO.,LTD. |