CN203410624U - Small-sized hand-thrown unmanned aerial vehicle - Google Patents
Small-sized hand-thrown unmanned aerial vehicle Download PDFInfo
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- CN203410624U CN203410624U CN201320464220.0U CN201320464220U CN203410624U CN 203410624 U CN203410624 U CN 203410624U CN 201320464220 U CN201320464220 U CN 201320464220U CN 203410624 U CN203410624 U CN 203410624U
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- unmanned plane
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- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims abstract description 25
- 229910052799 carbon Inorganic materials 0.000 claims abstract description 25
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims abstract description 15
- 229910052782 aluminium Inorganic materials 0.000 claims abstract description 15
- 238000007789 sealing Methods 0.000 claims description 8
- 238000005266 casting Methods 0.000 claims description 7
- 238000010521 absorption reaction Methods 0.000 claims description 4
- 239000003365 glass fiber Substances 0.000 claims description 4
- 239000003822 epoxy resin Substances 0.000 claims description 3
- 210000003205 muscle Anatomy 0.000 claims description 3
- 229920000647 polyepoxide Polymers 0.000 claims description 3
- 238000001179 sorption measurement Methods 0.000 abstract 1
- 230000006835 compression Effects 0.000 description 8
- 238000007906 compression Methods 0.000 description 8
- 230000009102 absorption Effects 0.000 description 3
- 238000010586 diagram Methods 0.000 description 3
- 230000005540 biological transmission Effects 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 238000009434 installation Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 230000008569 process Effects 0.000 description 2
- 239000004677 Nylon Substances 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
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- 230000005611 electricity Effects 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 230000007246 mechanism Effects 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
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Abstract
The utility model relates to a small-sized hand-thrown unmanned aerial vehicle. The small-sized hand-thrown unmanned aerial vehicle comprises a nose, a body, wings, an empennage, a propeller, a carbon pipe and an aluminum pipe, wherein the nose is connected with the front end of the body in a magnetic adsorption manner; the wings are fixed at the top of the body and are placed in a bilaterally symmetrical manner; the aluminum pipe extends out of the rear end of the body and is connected with the carbon pipe; the propeller is connected with the tail part of the body; the wings adopt detachable wings with thin arm design; the carbon pipe is connected with the empennage; a parachute placing box is arranged on the surface of the wings. The small-sized hand-thrown unmanned aerial vehicle has the benefits that the weight of the unmanned aerial vehicle is reduced; the unmanned aerial vehicle is convenient to carry, relatively stable in connection, relatively stable in landing and relatively simple to operate.
Description
Technical field
The utility model relates to a kind of small-sized hand and throws unmanned plane, belongs to the fields such as aviation flight, Aerial photography, aerial reconnaissance.
Background technology
Fixed-wing class unmanned plane occupies very high ratio in unmanned plane market at present, a high level has also been arrived in the development of fixed-wing class unmanned plane, particularly large aircraft is as global hawk of the U.S. etc., general small-sized fixed-wing class unmanned plane is because self structure is generally limited by the impact of site factors, carry also inconvenience, major part is also confined to model plane level.
Utility model content
Technical problem to be solved in the utility model is to provide a kind of small-sized hand and throws unmanned plane, has overcome and has carried inconvenience, complex operation, the excessive shortcoming of conducting oneself with dignity.
The technical scheme that the utility model solves the problems of the technologies described above is as follows: a kind of small-sized hand is thrown unmanned plane, comprise head, fuselage, wing, empennage, screw propeller, carbon pipe and aluminum pipe, described head magnetic absorption is connected to described front fuselage, described wing is fixed on described fuselage top, become symmetrical mode to place, described back body extends described aluminum pipe, described aluminum pipe is connected with described carbon pipe, described carbon pipe is connected with described empennage, described wing is for adopting the detachable wing of thin arm design, described carbon pipe is connected with described empennage, described aerofoil surface is provided with parachute box.
Further, described fuselage is comprised of cabin, and described engine room inside is provided with rib, and there is detouchable sealing side plate described fuselage both sides.
Further, removable wing body, the wing of being divided into of described wing, described wing is connected to it the described wing by the buckle between pipe link.
Further, described empennage comprises the flat wing of tail and the perpendicular wing of tail, and the flat wing of described tail is connected with described carbon pipe by connecting bushing, and the perpendicular wing of described tail is connected with carbon pipe by buckle.
Further, described wing inside is provided with bar shaped muscle, and described wing wing arm outside face scribbles glass fibre and epoxy resin and posts one deck honeycomb paper.
Further, described parachute box is provided with gamp and umbellule two parts, and described umbellule is on described gamp.
Further, described afterbody is equipped with the propeller of rearmounted mode.
Further, described connecting bushing comprises permanent seat, fixed block, transverse axis, V-arrangement arm, described permanent seat one end is fixedly connected with carbon pipe, the described permanent seat other end has casting lug thereon with holes, described transverse axis is through the hole on described casting lug thereon, arm bottom and one end of described V-arrangement are provided with hole, and the borehole jack of described V-arrangement arm one end is at described transverse axis middle part, and described transverse axis two ends are fixed on the both ends of the surface of described fixed block.
Further, described fixed block is spill fixed block, and described fixed block both ends of the surface are provided with perforate, and described fixed block bottom is provided with groove, and described groove both sides are provided with screw.
Further, described fuselage interior is provided with motor, and described motor is brshless DC motor.
The beneficial effects of the utility model are: reduced the weight of unmanned plane, made to carry more convenient, connected more firmly, landed more stable, operated simpler.
Accompanying drawing explanation
Fig. 1 is that small-sized hand of the present utility model is thrown unmanned plane structural scheme of mechanism;
Fig. 2 is that small-sized hand of the present utility model is thrown unmanned aerial vehicle body both sides side plate work schematic diagram;
Fig. 3 is that small-sized hand of the present utility model is thrown unmanned plane buckle structure schematic diagram;
Fig. 4 is that small-sized hand of the present utility model is thrown unmanned plane parachute position view;
Fig. 5 is that small-sized hand of the present utility model is thrown unmanned plane connecting bushing structural representation;
Fig. 6 is the structural representation that small-sized hand of the present utility model is thrown unmanned plane V-arrangement arm;
Fig. 7 is that small-sized hand of the present utility model is thrown unmanned plane fixed-block-architecture (FBA) schematic diagram;
In accompanying drawing, the list of parts of each label representative is as follows:
1, head, 2, fuselage, 3, parachute box, 4, aluminum pipe, 5, carbon pipe, 6, the perpendicular wing of tail, 7, the flat wing of tail, 8, screw propeller, 9, wing, 10, wing body, 11, wing, 12, umbellule, 13, gamp, 14, buckle, 15, permanent seat, 16, arm, 17, transverse axis, 18, fixed block, 19, compression link, 20, spring, 21, pull bar, 22, sealing side plate, 23, empennage, 24, pull bar connecting panel, 25, casting lug thereon, 26, the first hole, the 27, second hole, 28, groove, 29, screw, 30 perforates.
The specific embodiment
Below in conjunction with accompanying drawing, principle of the present utility model and feature are described, example, only for explaining the utility model, is not intended to limit scope of the present utility model.
As shown in Figure 1 and Figure 2, small-sized hand of the present utility model throws that unmanned plane comprises head 1 and the fuselage 2 being connected with head 1 magnetic absorption, wing 9, screw propeller 8, empennage 23, carbon pipe 5 and the aluminum pipe 4 of the afterbody that is threaded with carbon pipe 5, fuselage 2 front end magnetic absorptions are connecting head 1, wing 9 is fixed on fuselage 2 both sides, upper end, become symmetrical mode to place, an aluminum pipe 4 is extended in fuselage 2 rear ends, and aluminum pipe 4 is threaded with carbon pipe 5, and carbon pipe 5 is connected with empennage 23.
Described fuselage 2 comprises preposition cabin, built-in cabin, preposition cabin is used for placing camera, built-in cabin comprises sealed cabin, battery sealed cabin and being placed with flies control, radio station, GPS GPS device, sonar equipment, magnetometer, steering wheel, steering wheel plate, emitter receptor, the equipment sealed cabin of airborne equipment power supply etc., there is demountable sealing side plate 22 fuselage 2 both sides, this sealing side plate is provided with two pull bar connecting panels 24 that be arranged in parallel towards the one side of engine room inside, pull bar 21 is mobilizable through described pull bar connecting panel 24, the two ends of C type compression link 19 are fixedly connected with pull bar 21, one end of compression link 19 is between two pull bar connecting panels 24, other one end of compression link 19 is positioned at the outside of two pull bar connecting panels 24, spring 20 is set on pull bar 21, at compression link 19 in the one end between two pull bar connecting panels 24 with between the pull bar connecting panel 24 between compression link 19, when pull bar 21 pulls to the right, drive is fixedly connected on compression link 19 on pull bar 21 Compress Spring 20 that moves right, now pull bar 21 left ends separate with fuselage interior, now just can pull down or open sealing side plate 22, when sealing side plate 22 in opening, loosening pull bar 21, spring 20 elastic resets drive compression links 19 and pull bar 21 to left movement, and pull bar 21 is combined with fuselage interior, and sealing side plate 22 just can be in loading onto or closed condition.
As Figure 1 and Figure 4, described fuselage 2 upper ends are fixed with wing 9, the afterbody of fuselage 2 is equipped with rear-mounted screw propeller 8, screw propeller 8 is driven by the motor room that is positioned at fuselage upper back, the upper surface of wing 9 is provided with parachute box 3, and the switching of parachute box is controlled by spring and steering wheel, when umbrella box is closed, steering wheel arm gear presses off a mouthful side, spring-compressed; When umbrella box is opened, steering wheel arm gets out of the way opening one side spring and relies on elastic force that upper cover is flicked, and parachute ejects umbrella box.Parachute in parachute box 3 has umbellule 12 and gamp 13, and umbellule 12 is above gamp 13, and in landing process, umbellule takes the lead in ejecting into opening and drives gamp to open again, and avoids residual around screw propeller 8.
As shown in Figure 1, Figure 3, removable wing body 10 and the wing 11 of being divided into of described wing 9, between wing 9 and fuselage 2, by nylon screw, fix, between wing body 10 and wing 11, be to connect by the pipe link with buckle 14, during connection, the spring installation pressurized of buckle 11 inside shrinks inwards, and the extruding that after card is good, buckle 11 is subject to disappears, and spring installation automatic spring and wing body 10 and wing 11 complete fixing.Wing 9 the insides are provided with the muscle of strip, and one deck honeycomb paper has also been pasted in the thin arm outside of wing 9 except scribbling glass fibre, epoxy resin.
As shown in Figure 1, shown in Figure 5, an aluminum pipe 4 is given prominence in described fuselage 2 rear ends, and aluminum pipe 4 and carbon pipe 5 adopt and be threaded, and described aluminum pipe 4 is with in carbon pipe 5, wherein the external diameter of one is identical with the internal diameter of another one, and the flat wing 7 of described tail is connected by connecting bushing with carbon pipe 5.Little one end of permanent seat 15 of described connecting bushing is fixedly connected on the rear end of carbon pipe 5, and one end that permanent seat 15 is large is provided with porose casting lug thereon 25, as shown in Figure 7, fixed block 18 is a spill piece, in the middle of the bottom of spill piece, be provided with groove 28, the both sides of described groove 28 are provided with the screw 29 with the flat wing 7 of tail for connection fixing block 18, and described fixed block 18 both sides end faces are provided with the perforate 30 being fixedly connected with transverse axis 17 two ends, as shown in Figure 6, arm 16 is V-arrangement arm, one end of described V-arrangement arm 16 is provided with the first hole 26, described V-arrangement arm 16 bottoms are provided with the second hole 27 being enclosed within on transverse axis 17, the other end of described V-arrangement arm 16 is through the groove 28 of fixed block 25 bottoms, described the first hole 26 connects the steering wheel of fuselage interior by connecting rod, described steering wheel is controlled and is driven the flat wing of tail to change, make the flat wing of tail directly as rudder face, control hand and throw the lifting of unmanned plane in flight course, transverse axis 17 is through the hole on casting lug thereon 25 and the second hole 27 of V-arrangement arm 16 bottoms, the two ends of transverse axis 17 are fixedly connected with the perforate 30 of fixed block 18 both sides end faces.
Its working process is: by people, with hand, unmanned plane is dished out, unmanned plane is taken off, air engineer controls emitter receptor and the data transmission radio station in unmanned plane cabin by service platform, make it complete relevant flight orders, during unmanned plane landing, air engineer operates the box that releases a parachute, and first the umbellule in parachute box scatters and reach mode of operation, then drive gamp smooth opening, complete the safe falling of unmanned plane.
Fuselage of the present utility model, wing adopt glass fiber material to make, and fuselage, wing centre portion adopt hollow shell structure.The motor adopting is that to have cal val, volume, noise all very little, but reliable and stable brshless DC motor.By electricity, adjust the alternating signal of output to rotarily drive aircraft front end blade flying power is provided.
The utility model total technical index is as shown in table 1.
Table 1 total technical index
| Sequence number | Title | |
|
| 1 | | 3kg | |
| 2 | Oad mm(length) | 2380×1655×560 | |
| 3 | | 1h | |
| 4 | Cruising speed | 60km/ |
|
| 5 | Working temperature range | -10℃～55 |
|
| 6 | Environment takes off | Earth's surface wind-force is at 3～4 |
|
| 7 | Adapt to weather | Light rain, |
|
| 8 | Working relative humidity | 95%RH(ambient temperature is 25 ℃) | |
| 9 | Remote controller operating temperature | -10℃～55 |
|
| 10 | Remote controller size (mm) | 210 * 200 * 100(length * wide * height) | |
| 11 | Data transmission radio station operating temperature | -40℃～85℃ |
The foregoing is only preferred embodiment of the present utility model, not in order to limit the utility model, all within spirit of the present utility model and principle, any modification of doing, be equal to replacement, improvement etc., within all should being included in protection domain of the present utility model.
Claims (10)
1. a small-sized hand is thrown unmanned plane, it is characterized in that, comprise head, fuselage, wing, empennage, screw propeller, carbon pipe and aluminum pipe, described head magnetic absorption is connected to described front fuselage, described wing is fixed on described fuselage top, become symmetrical mode to place, described back body extends described aluminum pipe, described aluminum pipe is connected with described carbon pipe, described screw propeller is connected with described afterbody, described wing is for adopting the detachable wing of thin arm design, and described carbon pipe is connected with described empennage, and described aerofoil surface is provided with parachute box.
2. a kind of small-sized hand according to claim 1 is thrown unmanned plane, it is characterized in that, described fuselage is comprised of cabin, and described engine room inside is provided with rib, and there is detouchable sealing side plate described fuselage both sides.
3. a kind of small-sized hand according to claim 1 is thrown unmanned plane, it is characterized in that, and removable wing body, the wing of being divided into of described wing, described wing is connected to it the described wing by the buckle between pipe link.
4. a kind of small-sized hand according to claim 1 is thrown unmanned plane, it is characterized in that, described empennage comprises the flat wing of tail and the perpendicular wing of tail, and the flat wing of described tail is connected with described carbon pipe by connecting bushing, and the perpendicular wing of described tail is connected with carbon pipe by buckle.
5. a kind of small-sized hand according to claim 1 is thrown unmanned plane, it is characterized in that, described wing inside is provided with bar shaped muscle, and described wing wing arm outside face scribbles glass fibre and epoxy resin and posts one deck honeycomb paper.
6. a kind of small-sized hand according to claim 1 is thrown unmanned plane, it is characterized in that, described parachute box is provided with gamp and umbellule two parts, and described umbellule is on described gamp.
7. a kind of small-sized hand according to claim 1 is thrown unmanned plane, it is characterized in that, described afterbody is equipped with the propeller of rearmounted mode.
8. a kind of small-sized hand according to claim 4 is thrown unmanned plane, it is characterized in that, described connecting bushing comprises permanent seat, fixed block, transverse axis, V-arrangement arm, described permanent seat one end is fixedly connected with carbon pipe, the described permanent seat other end has casting lug thereon with holes, and described transverse axis is through the hole on described casting lug thereon, and bottom and one end of described V-arrangement arm are provided with hole, the borehole jack of described V-arrangement arm one end is at described transverse axis middle part, and described transverse axis two ends are fixed on the both ends of the surface of described fixed block.
9. a kind of small-sized hand according to claim 8 is thrown unmanned plane, it is characterized in that, described fixed block is spill fixed block, and described fixed block both ends of the surface are provided with perforate, and described fixed block bottom is provided with groove, and described groove both sides are provided with screw.
10. a kind of small-sized hand according to claim 1 is thrown unmanned plane, it is characterized in that, described fuselage interior is provided with motor, and described motor is brshless DC motor.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320464220.0U CN203410624U (en) | 2013-07-31 | 2013-07-31 | Small-sized hand-thrown unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320464220.0U CN203410624U (en) | 2013-07-31 | 2013-07-31 | Small-sized hand-thrown unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203410624U true CN203410624U (en) | 2014-01-29 |
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ID=49973535
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201320464220.0U Expired - Fee Related CN203410624U (en) | 2013-07-31 | 2013-07-31 | Small-sized hand-thrown unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN203410624U (en) |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104691736A (en) * | 2015-03-12 | 2015-06-10 | 江苏艾锐泰克无人飞行器科技有限公司 | Fixed-wing unmanned aerial vehicle |
| WO2015122939A1 (en) * | 2014-02-14 | 2015-08-20 | The Boeing Company | Aircraft fuselage constructed of aircraft fuselage sections screwed together |
| CN105388901A (en) * | 2014-08-26 | 2016-03-09 | 鹦鹉股份有限公司 | Method of dynamic control of a rotary- wing drone in throw start |
| CN105836102A (en) * | 2016-06-07 | 2016-08-10 | 广州天海翔航空科技有限公司 | High-performance small plateau unmanned reconnaissance aerial vehicle |
| CN106043660A (en) * | 2016-06-07 | 2016-10-26 | 广州天海翔航空科技有限公司 | High-performance unmanned aerial vehicle applicable to seaside salt mist area |
| CN107487447A (en) * | 2017-07-14 | 2017-12-19 | 广东黄赛航空科技有限公司 | A kind of unmanned plane |
-
2013
- 2013-07-31 CN CN201320464220.0U patent/CN203410624U/en not_active Expired - Fee Related
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2015122939A1 (en) * | 2014-02-14 | 2015-08-20 | The Boeing Company | Aircraft fuselage constructed of aircraft fuselage sections screwed together |
| CN105388901A (en) * | 2014-08-26 | 2016-03-09 | 鹦鹉股份有限公司 | Method of dynamic control of a rotary- wing drone in throw start |
| CN104691736A (en) * | 2015-03-12 | 2015-06-10 | 江苏艾锐泰克无人飞行器科技有限公司 | Fixed-wing unmanned aerial vehicle |
| CN105836102A (en) * | 2016-06-07 | 2016-08-10 | 广州天海翔航空科技有限公司 | High-performance small plateau unmanned reconnaissance aerial vehicle |
| CN106043660A (en) * | 2016-06-07 | 2016-10-26 | 广州天海翔航空科技有限公司 | High-performance unmanned aerial vehicle applicable to seaside salt mist area |
| CN105836102B (en) * | 2016-06-07 | 2018-06-08 | 广州天海翔航空科技有限公司 | A kind of high performance mini plateau scounting aeroplane |
| CN107487447A (en) * | 2017-07-14 | 2017-12-19 | 广东黄赛航空科技有限公司 | A kind of unmanned plane |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20140129 |