CN204956949U - Light foldable unmanned aerial vehicle launcher - Google Patents
Light foldable unmanned aerial vehicle launcher Download PDFInfo
- Publication number
- CN204956949U CN204956949U CN201520736598.0U CN201520736598U CN204956949U CN 204956949 U CN204956949 U CN 204956949U CN 201520736598 U CN201520736598 U CN 201520736598U CN 204956949 U CN204956949 U CN 204956949U
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- launcher
- level
- unmanned plane
- folding
- flat pad
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Abstract
The utility model discloses a light foldable unmanned aerial vehicle launcher, include: a folding foot rest and a transmission platform are connected as an organic wholely before two the folding foot rests in back, one, and first mechanism includes: an activity folding mechanism, activity folding mechanism links with a tip moving phase of folding foot rest, a horizontal adjustment mechanism, including setting up the level(l)ing box in transmission platform below, transversely set up a level(l)ing lead screw in the box, the tip that the level(l)ing box was worn out to the level(l)ing lead screw is fixed with firsthand rocker, still be provided with a level(l)ing screw nut on the level(l)ing lead screw in the level(l)ing box, firsthand's rocker rotates drive level(l)ing lead screw rotation and drives level(l)ing screw nut and drives a rocking arm that is connected, the top of rocking arm sets up the transmission platform. The utility model discloses light foldable unmanned aerial vehicle launcher light in weight, collapsible, adaptable different places are to the multidirectional regulation of unmanned aerial vehicle launch angle.
Description
Technical field
The utility model relates to a kind of military training equipment, especially a kind of portable folding formula unmanned plane launcher.
Background technology
The aircraft such as the military unmanned plane of part, unmanned plane target drone can not rely on self power to take off, and need specialized equipment to assist, normally taking off of guarantee aircraft.
But the volume of current unmanned plane launcher is large, Heavy Weight, not collapsible, transport takes up room large, and carrying is heavy, adjusts loaded down with trivial details, to launch site environmental requirement high (ground must be smooth).
Open defect is there is for the actual combat of high maneuverability, transport space an inch of land is an inch of gold or rehearsal task.Gu, need to carry out improvement design again to unmanned plane launcher, reach lightweight, portability, adjustment simplification, be suitable for place variation, to meet the high standard combat duty requirement of army.
Summary of the invention
For the problems referred to above, the utility model portable folding formula unmanned plane launcher is lightweight, collapsible, can adapt to different place to the multidirectional adjustment of unmanned plane emission angle.
In order to realize foregoing invention object, portable folding formula unmanned plane launcher of the present utility model, is characterized in that, comprising:
Folding tripod, a front folding tripod and a flat pad after two, described rear folding tripod and front folding tripod are connected as a single entity by the first mechanism and described flat pad,
Wherein, described first mechanism comprises further:
One movable folding mechanism, an end of described movable folding mechanism and described folding tripod is movably connected;
One level(l)ing mechanism, comprise the Level tune casing be arranged on below described flat pad, horizontally set one Level tune leading screw in described casing, the end that described Level tune leading screw passes described Level tune casing is fixed with first-hand rocking bar, described Level tune leading screw in described Level tune casing is also provided with a Level tune feed screw nut, Level tune leading screw described in described first-hand rocking bar rotating drive rotates and drives Level tune adjusting screw nut to drive the rocking arm be connected, and the top of described rocking arm arranges described flat pad.
Reasonable, portable folding formula unmanned plane launcher of the present utility model, it is characterized in that, described launcher comprises further:
One emission angle regulating mechanism, be arranged between described flat pad and described front folding tripod, described transmitting luffing angle regulating mechanism comprises a luffing angle adjusting screw, described luffing angle regulates one end of screw mandrel to be fixedly connected with described flat pad by a clamping part, described luffing angle regulates the other end of screw mandrel to connect a gear case, described gear case is fixed on described front folding tripod, one group of intermeshing active umbrella tooth and driven umbrella teeth nut is comprised in described gear case, described driven umbrella teeth nut is set in described luffing angle and regulates on screw mandrel, second-hand's rocking bar that described active umbrella tooth connects stretches out described gear case, described active umbrella tooth and described driven umbrella teeth nut are vertically fixed in described gear case mutually.
Reasonable, portable folding formula unmanned plane launcher of the present utility model, it is characterized in that, described launcher comprises further:
One booster rocket tight pushing device, described booster rocket tight pushing device is arranged on the rear end of described flat pad, comprise the fixed part that is arranged on described flat pad lower end, one end of a booster rocket fixed jaw can be rotated around described fixed part, and the other end is provided with a groove for placing unmanned plane.
Reasonable, portable folding formula unmanned plane launcher of the present utility model, it is characterized in that, described launcher comprises further:
One hand lever, one end is connected to described fixed part, the other end extends to the afterbody of whole launcher, is fixed with a booster rocket top-fastener on the top of described hand lever, and there is a bayonet socket end of described booster rocket top-fastener, described booster rocket fixed jaw is fastened in institute's bayonet socket, hold out against described booster rocket fixed jaw, described booster rocket top-fastener is hollow, is inside provided with a spring, one end of described spring holds out against described booster rocket fixed jaw, and the other end props up a governing screw.
Reasonable, portable folding formula unmanned plane launcher of the present utility model, it is characterized in that, described launcher comprises further:
One stay hook, is arranged on the afterbody of described flat pad, and the barb that described hand lever afterbody is just blocked at the curved position of establishing of described stay hook locks mutually.
Reasonable, portable folding formula unmanned plane launcher of the present utility model, it is characterized in that, described launcher comprises further:
One holder firing mount, one end is fixed on described flat pad by a rotating mechanism, and the other end is in order to fixing unmanned plane.
Reasonable, portable folding formula unmanned plane launcher of the present utility model, it is characterized in that, described movable folding mechanism comprises a pinned connection.
Reasonable, portable folding formula unmanned plane launcher of the present utility model, it is characterized in that, described rotating mechanism comprises a fixed bearing block.
Due to holder firing mount and the supporting leg employing rectangular steel tube structure of the utility model portable folding formula launcher.Front leg strut and rear support leg adopt pinned connection mode to fold, and form gusseted after supporting leg launches to holder firing mount.Level(l)ing mechanism adopts leading screw to drive feed screw nut, feed screw nut to drive rocking arm to regulate.Leading screw regulating mechanism before pitch regulation then relies on launcher on folding feet adjusts, therefore convenient folding and transport, and is also conducive in use regulating.
Accompanying drawing explanation
Below, with reference to accompanying drawing, for those skilled in the art, to detailed description of the present utility model, above and other object of the present utility model, feature and advantage will be apparent.
Fig. 1 is the front schematic view that launcher of the present utility model is opened;
Fig. 2 is the birds-eye view of Fig. 1;
Fig. 3 is the partial schematic diagram of Fig. 1;
Fig. 4 is the right elevation of Fig. 3;
Fig. 5 is the structural representation of level(l)ing mechanism 4 in Fig. 3;
Fig. 6 is the structural representation launching luffing angle regulating mechanism 6 in Fig. 1;
Fig. 7 is the structural representation of booster rocket tight pushing device 3 in Fig. 1;
Fig. 8 is the structural representation of flat pad 2 and holder firing mount 1 in Fig. 1;
Fig. 9 is the structural representation after the utility model folds.
Reference numeral
1--holds in the palm firing mount
2--flat pad
3--booster rocket tight pushing device
4--level(l)ing mechanism
Folding tripod after 5--
6--launches luffing angle regulating mechanism
Folding tripod before 7--
8--movable folding mechanism
11--fixed bearing block
31--booster rocket fixed jaw
32--booster rocket top-fastener
33--spring
34--governing screw
35--stay hook
36--hand lever
37--fixed part
41--Level tune casing
42--swing arm
43--joystick
44--Level tune feed screw nut
45--Level tune leading screw
51--limiting stopper
61--clamping part
62--adjusting screw
63--gear case
64--joystick
65--is umbrella tooth initiatively
The driven umbrella teeth nut of 66--
Detailed description of the invention
Please refer to the structural representation of the of the present utility model collapsible unmanned plane launcher shown in Fig. 1 and Fig. 2.
Can recognize in this two schematic diagram, folding tripod 5 after launcher of the present utility model comprises two, a front folding tripod 7 and flat pad 2, after two, folding tripod 5 and a front folding tripod 7 are connected as a single entity by the first mechanism and flat pad 2, this first mechanism comprises movable folding mechanism 8 and a level(l)ing mechanism 4, movable folding mechanism 8 and folding tripod 5, the end of 7 is movably connected, preferably movable folding mechanism 8 adopts pinned connection, make three folding tripods can be with bearing pin fulcrum like this and fold, when expansion three folding tripod, gusseted can be formed to flat pad 2.This movable folding mechanism 8 is fixed on a sidepiece of level(l)ing mechanism 4.
Fig. 3 gives the annexation of movable folding mechanism 8 and level(l)ing mechanism 4.
Fig. 4 gives the local structure schematic diagram of Fig. 3 level(l)ing mechanism that right apparent direction is seen 4.
Fig. 5 illustrates separately the composition structure of level(l)ing mechanism 4 further, it comprises the Level tune casing 41 be arranged on below flat pad 2, horizontally set one Level tune leading screw 45 in casing 41, this leading screw 45 passes end winding support one joystick 43 of casing 41, leading screw 45 in casing 41 is also provided with a Level tune feed screw nut 44, along with operator is to the rotation of joystick 43, leading screw 45 is driven to rotate, drive Level tune feed screw nut 44 to drive the Rocker arm 42 be connected, the angle of this Rocker arm 42 determines the angle of flat pad 2.
Fig. 6 gives the structure of the transmitting luffing angle regulating mechanism 6 be arranged between flat pad 2 and front folding tripod 7, is the schematic diagram of the left side angle from Fig. 1.
In conjunction with two figure, this transmitting luffing angle regulating mechanism 6 comprises luffing angle adjusting screw 62, this luffing angle regulates one end of screw mandrel 62 to be fixedly connected with flat pad 2 by a clamping part 61, luffing angle regulates the other end of screw mandrel 62 to connect a gear case 63, this gear case 63 is fixed on front folding tripod 7, one group of intermeshing active umbrella tooth 65 and driven umbrella teeth nut 66 is comprised in this gear case 63, this driven umbrella teeth nut 66 is set in luffing angle and regulates on screw mandrel 62, the joystick 64 that initiatively umbrella tooth 65 connects stretches out gear case 63, initiatively umbrella tooth 65 and driven umbrella teeth nut 66 are vertically fixed in gear case 63 mutually.When operator shakes joystick 64, driven umbrella teeth nut 66 is driven to rotate by active umbrella tooth 65, thus drive luffing angle to regulate the knee-action of screw mandrel 62 on luffing angle, thus determine to be positioned at the luffing angle variation regulating flat pad 2 fixing on screw mandrel 62 end clamping part 61.Rotate joystick 64, main story or the reversion of driven umbrella teeth nut 66 can be controlled, thus accurately control the exposed length of luffing angle adjusting screw 62, ensure that the emission angle of unmanned plane on flat pad 2 reaches setting best.Have employed screw structure in this launcher pitching adjusting mechanism, because screw structure itself has locked, even if be subject to external force impact, also can not the angle set be had any impact.Launcher is made to have very strong stability.
Fig. 7 gives the detailed construction arranging booster rocket tight pushing device 3 in FIG.
This booster rocket tight pushing device 3 is arranged on the rear end of flat pad 2.This booster rocket tight pushing device 3 comprises the fixed part 37 that is arranged on flat pad 2 lower end, one booster rocket fixed jaw 31 one end can be rotated around fixed part 37, the other end is provided with groove can place rocket, in addition, one end of one hand lever 36 is also connected on fixed part 37, the other end extends to the afterbody of whole launcher, a booster rocket top-fastener 32 is fixed with on the top of this hand lever 36, there is a bayonet socket end of this top-fastener 32, booster rocket fixed jaw 31 is fastened in this bayonet socket, play the effect holding out against this fixed jaw 31, this booster rocket top-fastener 32 hollow, inside be provided with a spring 33, one end of spring 33 holds out against fixed jaw 31, the other end props up a governing screw 34.In addition, further illustrating the afterbody being arranged on flat pad 2 in figure has a stay hook 35, and the barb that hand lever 36 afterbody is just blocked at the curved position of establishing of stay hook 35 locks mutually.
During assembling, governing screw 34 is screwed in booster rocket top-fastener 32, then spring 33 is put into booster rocket top-fastener 32, and top-fastener 32 withstands booster rocket fixed jaw 31.
When hand lever 36 is strained by operator upward, the hook 35 that is just fixed of the barb on hand lever 36 catches on and prevents hand lever 36 resilience.Withstand booster rocket fixed jaw 31 by top-fastener 32, the size of pressure regulates decision by governing screw 34 and spring 33.
Booster rocket is designed under the state not having thrust can Automatic-falling, and after rocket does not start and burning completes, rocket does not have thrust, can Automatic-falling.But when emission state, jacking mechanism 3 must be used to make to hold rocket and to remain on the emission angle fixed, can't come off.So add jacking mechanism 3, ensure that rocket can promote unmanned plane with correct angle and enter predetermined flight track.
In addition, Fig. 8 furthermore present in Fig. 1 the structural representation of holding in the palm firing mount 1.
One end of this holder firing mount 1 is fixed on flat pad 2 by a rotating mechanism, and the rotating mechanism usually adopted is fixed bearing block 11, and the other end is in order to fixing unmanned plane.By side in Fig. 8 from left to right to during by external force, holder firing mount 1 can clockwise oscillation 90 °.
Unmanned plane is fixed on holder firing mount 1, when non-power state, unmanned plane by gravity and the elevation angle affect can be stable remain on holder firing mount 1 on motionless, when rocket works, unmanned plane travels forward, holder firing mount 1 rotates unmanned plane along the fixed bearing block 11 of bottom and departs from and be affected by gravity, and vertically drops.Complete fixing and detachment function in its simplest form.
Fig. 9 illustrate launcher of the present utility model fold after structure.
Because the utility model adopts flat pad 2 to be agent structure, foot rest 5 is connected with flat pad 2 by movable folding mechanism 8 with 7, when needs are folding, by whole launcher upset of the present utility model, first front foot frame 7 is adjusted to minimum, then two rear legs 5 is overturn folding fixing.When needs are opened, take out the launcher that folds, launcher is reversed, first two rear legs 5 is opened, then front foot frame 7 is regulated flush as rear leg 5, then overturn.
Size 2500*440*400mm after launcher of the present utility model is folding, is only about launcher and launches volume 1/3.
The utility model due to the foot rest occupying launcher larger space is designed to collapsible after, use less material can reach same result of use.Meanwhile, identical transport space, can only put down the launcher of an old edition in the past.And this launcher folding after, 3 can be put down, save transport space greatly, improve conveying efficiency, reduce traffic cost.
The beneficial effects of the utility model comprise following several aspect:
The first, owing to adopting such scheme, be of a size of long 2.5 meters of wide 0.44 meter of X of X after launcher can be made to fold high 0.4 meter.And the holder firing mount of the utility model portable folding formula launcher and supporting leg adopt rectangular steel tube structure, and therefore overall weight is 72 kilograms, eliminates the work of leveling land, be convenient to transport and carrying, the labour intensity reducing carrying and regulate.Meanwhile, the utility model unmanned plane launcher portable foldable.Supporting leg adopts the form of bearing pin to fold, and after folding, volume is beaten and significantly reduces.
The second, holder firing mount 1 of the present utility model and support foot rest adopt square steel pipe welded structure, and under the prerequisite ensureing structural strength, materials'use is less, and launcher overall weight is significantly declined.
3rd, more perspective regulates: the leading screw in transverse horizontal surge tank, screw, hinge ask the swing arm on firing mount to be interconnected with being welded on, and achieves transverse horizontal adjustment.
All embodiments are only for illustration of the utility model above, but not to restriction of the present utility model, person skilled in the relevant technique, when not departing from spirit and scope of the present utility model, can also make various conversion or change, therefore all equivalent technical schemes also should belong to category of the present utility model and should be limited by each claim.
Claims (8)
1. portable folding formula unmanned plane launcher, is characterized in that, comprising:
Folding tripod, a front folding tripod and a flat pad after two, described rear folding tripod and front folding tripod are connected as a single entity by the first mechanism and described flat pad,
Wherein, described first mechanism comprises further:
One movable folding mechanism, an end of described movable folding mechanism and described folding tripod is movably connected;
One level(l)ing mechanism, comprise the Level tune casing be arranged on below described flat pad, horizontally set one Level tune leading screw in described casing, the end that described Level tune leading screw passes described Level tune casing is fixed with first-hand rocking bar, described Level tune leading screw in described Level tune casing is also provided with a Level tune feed screw nut, Level tune leading screw described in described first-hand rocking bar rotating drive rotates and drives Level tune adjusting screw nut to drive the rocking arm be connected, and the top of described rocking arm arranges described flat pad.
2. portable folding formula unmanned plane launcher according to claim 1, it is characterized in that, described launcher comprises further:
One emission angle regulating mechanism, be arranged between described flat pad and described front folding tripod, described transmitting luffing angle regulating mechanism comprises a luffing angle adjusting screw, described luffing angle regulates one end of screw mandrel to be fixedly connected with described flat pad by a clamping part, described luffing angle regulates the other end of screw mandrel to connect a gear case, described gear case is fixed on described front folding tripod, one group of intermeshing active umbrella tooth and driven umbrella teeth nut is comprised in described gear case, described driven umbrella teeth nut is set in described luffing angle and regulates on screw mandrel, second-hand's rocking bar that described active umbrella tooth connects stretches out described gear case, described active umbrella tooth and described driven umbrella teeth nut are vertically fixed in described gear case mutually.
3. portable folding formula unmanned plane launcher according to claim 2, it is characterized in that, described launcher comprises further:
One booster rocket tight pushing device, described booster rocket tight pushing device is arranged on the rear end of described flat pad, comprise the fixed part that is arranged on described flat pad lower end, one end of a booster rocket fixed jaw can be rotated around described fixed part, and the other end is provided with a groove for placing unmanned plane.
4. portable folding formula unmanned plane launcher according to claim 3, it is characterized in that, described launcher comprises further:
One hand lever, one end is connected to described fixed part, the other end extends to the afterbody of whole launcher, is fixed with a booster rocket top-fastener on the top of described hand lever, and there is a bayonet socket end of described booster rocket top-fastener, described booster rocket fixed jaw is fastened in described bayonet socket, hold out against described booster rocket fixed jaw, described booster rocket top-fastener is hollow, is inside provided with a spring, one end of described spring holds out against described booster rocket fixed jaw, and the other end props up a governing screw.
5. portable folding formula unmanned plane launcher according to claim 4, it is characterized in that, described launcher comprises further:
One stay hook, is arranged on the afterbody of described flat pad, and the barb that described hand lever afterbody is just blocked at the curved position of establishing of described stay hook locks mutually.
6. portable folding formula unmanned plane launcher according to claim 5, it is characterized in that, described launcher comprises further:
One holder firing mount, one end is fixed on described flat pad by a rotating mechanism, and the other end is in order to fixing unmanned plane.
7. portable folding formula unmanned plane launcher according to claim 6, is characterized in that,
Described movable folding mechanism comprises a pinned connection.
8. portable folding formula unmanned plane launcher according to claim 7, is characterized in that,
Described rotating mechanism comprises a fixed bearing block.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520736598.0U CN204956949U (en) | 2015-09-22 | 2015-09-22 | Light foldable unmanned aerial vehicle launcher |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520736598.0U CN204956949U (en) | 2015-09-22 | 2015-09-22 | Light foldable unmanned aerial vehicle launcher |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204956949U true CN204956949U (en) | 2016-01-13 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520736598.0U Expired - Fee Related CN204956949U (en) | 2015-09-22 | 2015-09-22 | Light foldable unmanned aerial vehicle launcher |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204956949U (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106828962A (en) * | 2016-12-27 | 2017-06-13 | 航天神舟飞行器有限公司 | Rocket assist formula high-speed unmanned aerial vehicle trigger mechanism |
| CN108128477A (en) * | 2017-12-22 | 2018-06-08 | 航天神舟飞行器有限公司 | A kind of adjustable rocket bracket of rato formula unmanned plane launcher |
| WO2019127565A1 (en) * | 2017-12-30 | 2019-07-04 | 深圳市富斯科技有限公司 | Aircraft launcher |
| CN114427804A (en) * | 2022-02-07 | 2022-05-03 | 四川中陆嘉诚科技有限公司 | Automatic shooting fixer for launching vehicle |
-
2015
- 2015-09-22 CN CN201520736598.0U patent/CN204956949U/en not_active Expired - Fee Related
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106828962A (en) * | 2016-12-27 | 2017-06-13 | 航天神舟飞行器有限公司 | Rocket assist formula high-speed unmanned aerial vehicle trigger mechanism |
| CN108128477A (en) * | 2017-12-22 | 2018-06-08 | 航天神舟飞行器有限公司 | A kind of adjustable rocket bracket of rato formula unmanned plane launcher |
| CN108128477B (en) * | 2017-12-22 | 2024-07-09 | 航天神舟飞行器有限公司 | Rocket bracket with adjustable rocket boosting take-off type unmanned aerial vehicle launching cradle |
| WO2019127565A1 (en) * | 2017-12-30 | 2019-07-04 | 深圳市富斯科技有限公司 | Aircraft launcher |
| CN114427804A (en) * | 2022-02-07 | 2022-05-03 | 四川中陆嘉诚科技有限公司 | Automatic shooting fixer for launching vehicle |
| CN114427804B (en) * | 2022-02-07 | 2023-08-29 | 四川中陆嘉诚科技有限公司 | Automatic shooting fixer for launching vehicle |
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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: 20190925 Address after: Room 101, Building 18, 3333 Huaning Road, Minhang District, Shanghai 201108 Patentee after: Shanghai Penlun Aviation Technology Co., Ltd. Address before: 200949 Shanghai city Baoshan District Feiyun Road No. 18 Patentee before: SHANGHAI NANXUN AVIATION TECHNOLOGY CO., LTD. |
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| 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: 20160113 Termination date: 20200922 |