CN205010465U - Unmanned aerial vehicle - Google Patents
Unmanned aerial vehicle Download PDFInfo
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- CN205010465U CN205010465U CN201520558642.3U CN201520558642U CN205010465U CN 205010465 U CN205010465 U CN 205010465U CN 201520558642 U CN201520558642 U CN 201520558642U CN 205010465 U CN205010465 U CN 205010465U
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Abstract
The utility model relates to an unmanned aerial vehicle, include: fuselage group connects the casing including a casing and a first pivotal part, first pivotal part, and first pivotal part has one at least buckling part, tail group connects the foot piece including a foot piece and a second pivotal part, second pivotal part, and the first pivotal part of second pivotal part pin joint has one two at least buckling part, and the 2nd buckling part can break away from a ground lock joint buckling part, and the foot piece can be put for the casing pivot. Unmanned aerial vehicle has a flight position and a position of folding up, lies in the flight position as unmanned aerial vehicle, and tail group is for fuselage group's pivot pendulum and make the 2nd a buckling part lock joint buckling part, lies in the position of folding up as unmanned aerial vehicle, and tail group is for fuselage group's pivot pendulum and make the 2nd buckling part break away from a buckling part.
Description
Technical field
The utility model relates to a kind of unmanned vehicle, refer in particular to a kind of can the unmanned vehicle of rapid-assembling and folding.
Background technology
With reference to the power system of the model of an airplane of No. 7789340th, US Patent, the wing (wing114) that the opposite side that wherein model of an airplane (flyingmodelairplane100) has a fuselage (fuselage102), a wing (wing108) and is connected to this fuselage also extends.One first power unit is arranged at the back of this wing (108) and has a motor (motor116) and a screw propeller rotated relative to this motor (propeller118).One second power unit is arranged at the back of this wing (114) and has a motor (120) and a screw propeller rotated relative to this motor (122).One empennage (tail104) is connected to this fuselage.This aircraft comprises the wing (112) that a wing (106) and being arranged at this wing (108) below is arranged at this wing (114) below.These two wings (106,108) are connected to each other by means of one first strut member (strut110), and these two wings (112,114) are connected to each other by means of this second strut member (strut111).This first power unit is arranged between this fuselage and this first strut member, and this second power unit is arranged between this fuselage and this second strut member.This aircraft more comprises a yaw rudder (rudder200) and an elevating rudder (elevator202), and this yaw rudder and this elevating rudder rely on a long pole (member204) to be connected to this fuselage respectively.
The above-mentioned model of an airplane cannot be disassembled and folding easily, makes user the model of an airplane cannot be positioned in automobile and carrying extremely arbitrary place, and then brings inconvenience.
Utility model content
The utility model be that unmanned vehicle cannot be disassembled and folding easily for the technical matters solved, unmanned vehicle cannot be positioned in automobile by user and carrying to arbitrary place, and then to bring inconvenience.
For achieving the above object, the technical solution adopted in the utility model is:
A kind of unmanned vehicle, it is characterized in that, it comprises:
One fuselage group, it comprises a housing and one first pivotal part, and this first pivotal part connects this housing, and this first pivotal part has at least one first engaging portion;
One tail group, it comprises a foot piece and one second pivotal part, this second pivotal part connects this foot piece, this this first pivotal part of the second pivotal part pivot joint also has at least one second engaging portion, this at least one second engaging portion is this at least one first engaging portion of snapping separatably, and this foot piece can be put relative to this housing pivot.
Described unmanned vehicle, wherein: this first pivotal part has two the first engaging portion and a groove, these two the first engaging portion are arranged at the two opposite sides of this groove respectively, this second pivotal part has two the second engaging portion and a convex extension part, these two second engaging portion are arranged at this convex extension part two opposite sides respectively, this this groove of convex extension part pivot joint, these two second engaging portion are these two first engaging portion of snapping separatably.
Described unmanned vehicle, wherein: this first pivotal part has one first perforation, this first perforation runs through this first pivotal part and is communicated with this groove, this second pivotal part has one second perforation, this second perforation runs through this convex extension part, one wears part wears this first perforation and second to bore a hole with this, and this second pivotal part can wear part for putting relative to this first pivotal part pivot in axle center with this.
Described unmanned vehicle, wherein: this housing has an accommodation space, one opening and two registration masts, this accommodation space of this open communication, these two registration masts to be arranged in this accommodation space and to lay respectively at this opening two opposite sides, this first pivotal part has two location flanges and is placed in this accommodation space, and the groove of this first pivotal part is towards this opening, these two location flanges lay respectively at this first pivotal part two opposite sides, this groove is between these two location flanges, these two location flange one of them recline these two registration masts one of them, another this registration mast and another this location flange reclines.
Described unmanned vehicle, wherein, also comprise two wing groups, each this wing group comprises the one first plate wing, the one second plate wing, one first conjunction and one second conjunction, these two the first plate wings are arranged at this housing two opposite sides respectively, this first conjunction and this first plate wing of each this wing group are connected to each other, and this second conjunction and this second plate wing of each this wing group are connected to each other, and this second conjunction of each this wing group is connected mutually separatably with this first conjunction.
Described unmanned vehicle, wherein: each this wing group comprises at least two brace panels, these at least two brace panels one of them be arranged at this first plate wing and connect this first conjunction, another this brace panel is arranged at this second plate wing and connects this second conjunction, each this brace panel is carbon fiber board, and each this first plate wing and each this second plate wing are respectively the poly-mer of foaming.
Described unmanned vehicle, wherein: each this first conjunction arranges a positioning groove, each this second conjunction arranges one convex section, the convex section of positioning groove departing from ground and connect each this first conjunction of each this second conjunction, the rectangular in cross-section of each this positioning groove, and each this cross section of convex section corresponds respectively to the cross section of each this positioning groove and rectangular.
Described unmanned vehicle, wherein: this foot piece has a connected section away from one end of this second pivotal part, this tail group comprises an elevating rudder and a yaw rudder, this elevating rudder and this yaw rudder are connected the connected section of this foot piece respectively separatably, the connected section of this foot piece arranges two nose bar portions and one first drive division, this first driving part is between these two nose bar portions, this first drive division stretches into this elevating rudder separatably, this elevating rudder comprises two attaching partss, these two attaching partss have a stretch section and a tank respectively, these two tanks are arranged at these two stretch sections respectively and rely on the elastic deformation of these two stretch sections respectively and connect this two nose bar portions separatably, this first drive division can pass two attaching partss of this elevating rudder relative to this second pivotal part pivot pendulum can with these two nose bar portions for axle center be put relative to this foot piece pivot.
Described unmanned vehicle, wherein: the connected section of this foot piece arranges one second drive division, this yaw rudder comprises one and protrudes out post and a guide pillar, this protrudes out the connected section that post stretches into this foot piece separatably, this guide pillar connects this second drive division separatably, and this second drive division can be passed this guide pillar relative to this second pivotal part pivot pendulum and drive this yaw rudder to protrude out post for putting relative to this foot piece pivot in axle center with this.
Described unmanned vehicle, wherein: this foot piece has a shaft, this shaft is between this connected section and this second pivotal part, and the cross section of this shaft is rounded.
Compared with prior art, the advantage adopting the utility model of technique scheme to have is: this unmanned vehicle has a flight position and a collapsed position, when this unmanned vehicle is positioned at this flight position, this tail group makes this fuselage group and this tail group lay respectively at this unmanned vehicle opposite end relative to this fuselage group pivot pendulum, this this at least one first engaging portion of at least one second engaging portion snapping, user can operate this unmanned vehicle in airflight.When this unmanned vehicle is positioned at this collapsed position, this tail group makes this at least one second engaging portion depart from this at least one first engaging portion relative to this fuselage group pivot pendulum, and this unmanned vehicle can be positioned in automobile by user easily.User only must pull this tail group relative to this fuselage group pivot pendulum, can easily and rapidly this unmanned vehicle is converted in this flight position and this collapsed position.
Accompanying drawing explanation
Fig. 1 is the stereo appearance figure of the utility model unmanned vehicle;
Fig. 2 is the partial exploded view that Fig. 1 gets;
Fig. 3 is another partial exploded view that Fig. 1 gets;
Fig. 4 is the part sectional view that Fig. 1 gets;
Fig. 5 is another part sectional view that Fig. 1 gets, and represents that unmanned vehicle is positioned at flight position;
Fig. 6 is the continuity of Fig. 5, represents that the tail group of unmanned vehicle is converted into collapsed position relative to fuselage group pivot pendulum by flight position along arrow;
Fig. 7 is the use schematic diagram of the utility model unmanned vehicle.
Description of reference numerals: 10-fuselage group; 11-housing; 111-accommodation space; 112-opening; 113-registration mast; 12-first pivotal part; 121-first engaging portion; 122-groove; 123-first bores a hole; 124-locates flange; 1241-arc groove; 20-tail group; 21-foot piece; 211-connected section; 2111-nose bar portion; 2112-first drive division; 2113-second drive division; 212-shaft; 22-second pivotal part; 221-second engaging portion; 222-convex extension part; 223-second bores a hole; 23-elevating rudder; 231-attaching parts; 2311-stretch section; 2312-tank; 232-connecting element; 2321-cylinder portion; 233-lifter plate; 24-yaw rudder; 241-protrudes out post; 242-guide pillar; 30-wing group; The 31-first plate wing; The 32-second plate wing; 33-first conjunction; 331-positioning groove; 34-second conjunction; Convex section of 341-; 35-brace panel; A-wears part; B-sky claps device.
Detailed description of the invention
With reference to figure 1, the utility model unmanned vehicle comprises fuselage group 10, tail group 20 and two wing groups 30.This this fuselage group 10 of tail group 20 pivot joint, and these two wing groups 30 are arranged at the two opposite sides of this fuselage group 10 along Y-axis respectively.This unmanned vehicle has a flight position and a collapsed position, when this unmanned vehicle is positioned at this flight position, this tail group 20 makes this fuselage group 10 arrange along X-axis with this tail group 20 relative to this fuselage group 10 pivot pendulum, and user can operate this unmanned vehicle in airflight.When this unmanned vehicle is positioned at this collapsed position, this tail group 20 makes this fuselage group 10 arrange along Z axis with this tail group 20 relative to this fuselage group 10 pivot pendulum, and this unmanned vehicle can be positioned in automobile by user easily.
Referring to figs. 2 to 5, this fuselage group 10 comprises housing 11 and one first pivotal part 12, and this first pivotal part 12 connects this housing 11.This housing 11 has accommodation space 111, opening 112 and two registration masts 113.The accommodation space 111 of this housing 11 extends along X-axis, and this opening 112 is communicated with this accommodation space 111, and these two registration masts 113 to be arranged in this accommodation space 111 and to lay respectively at the two opposite sides of this opening 112 along Y-axis.This first pivotal part 12 have at least one first engaging portion 121, groove 122,1 first bore a hole 123 and two locate flange 124, in the present embodiment, this first pivotal part 12 has two the first engaging portion 121.These two the first engaging portion 121 are arranged at the two opposite sides along Y-axis of this groove 122 respectively, this first perforation 123 extends along Y-axis and runs through this first pivotal part 12 and be communicated with this groove 122, these two the first engaging portion 121 are positioned at this first pivotal part 12 one end along Z axis, and this first perforation 123 is positioned at this first pivotal part 12 one end away from these two the first engaging portion 121, these two location flanges 124 lay respectively at the two opposite sides of this first pivotal part 12 along Y-axis, and this groove 122 is between these two location flanges 124, these two location flange 124 one of them recline these two registration masts 113 one of them, another this location flange 124 reclines another this registration mast 113, this groove 122 is towards this opening 112.In the present embodiment, this two registration masts 113 respectively rounded perpendicular to Z axis cross section, and these two location flanges 124 have an arc groove 1241 respectively, the cross section of these two arc grooves 1241 corresponds to the cross section of these two registration masts 113 respectively, make these two arc grooves 1241 one of them recline these two registration masts 113 one of them, another this registration mast 113 and another this arc groove 1241 reclines, this first pivotal part 12 is fixed in the accommodation space 111 of this housing 11.
This tail group 20 comprises foot piece 21,1 second pivotal part 22, elevating rudder 23 and a yaw rudder 24, this second pivotal part 22 is arranged at this foot piece 21, this elevating rudder 23 is arranged at this foot piece 21 separatably with this yaw rudder 24, this elevating rudder 23 extends along Y-axis, and this yaw rudder 24 extends along Z axis, this this first pivotal part 12 of the second pivotal part 22 pivot joint, makes this tail group 20 can put relative to this fuselage group 10 pivot.This foot piece 21 has connected section 211 and a shaft 212, this shaft 212 is between this connected section 211 and this second pivotal part 22, this elevating rudder 23 is arranged at this connected section 211 respectively separatably with this yaw rudder 24, in the present embodiment, this shaft 212 is rounded perpendicular to the cross section of X-axis, makes this shaft 212 can carry equipment easily.This connected section 211 has two nose bar portion 2111,1 first drive division 2112 and one second drive divisions 2113, these two nose bar portions 2111 are arranged at this connected section 211 two opposite sides and extend away from each other along Y-axis, this first drive division 2112 is between these two nose bar portions 2111 and extend along X-axis, this first drive division 2112 can be put relative to this second pivotal part 22 pivot, this second drive division 2113 is positioned at the side of this connected section 211 along Z axis, and this second drive division 2113 can be put relative to this second pivotal part 22 pivot.This second pivotal part 22 has at least one second engaging portion 221, convex extension part 222 and one second and bores a hole 223, and in the present embodiment, this second pivotal part 22 has two the second engaging portion 221.These two the second engaging portion 221 are arranged at this convex extension part 222 respectively along Y-axis two opposite sides, this second perforation 223 runs through this convex extension part 222 along Y-axis, this convex extension part 222 can be put relative to this groove 122 pivot, and makes these two the second engaging portion 221 snapping these two the first engaging portion 121 separatably.One wears part A wears this first perforation 123 and second bores a hole 223 with this, make this second pivotal part 22 can wear part A for putting relative to this first pivotal part 12 pivot in axle center with this, in the present embodiment, this wears part A is bolt, and utilizes nut to be fixed on this first perforation 123 second to bore a hole 223 with this.
This elevating rudder 23 comprises two attaching parts 231, connecting element 232 and lifter plates 233, and these two attaching partss 231 connect this connecting element 232 respectively, and this lifter plate 233 is connected to each other with this connecting element 232.These two attaching partss 231 have stretch section 2311 and a tank 2312 respectively away from one end of this connecting element 232, these two tanks 2312 are arranged at these two stretch sections 2311 respectively and rely on the elastic deformation of these two stretch sections 2311 respectively and connect this two nose bar portions 2111 separatably, and these two attaching partss 231 can be put relative to this foot piece 21 pivot with these two nose bar portions 2111.This connecting element 232 has a portion 2321, the cross section in this portion 2321 is circular and extends along X-axis, this portion 2321 is between these two attaching partss 231 and stretch into this lifter plate 233, and this first drive division 2112 stretches into this portion 2321 separatably and this elevating rudder 23 can be driven to put relative to this foot piece 21 pivot for axle center with these two nose bar portions 2111.This yaw rudder 24 comprises one and protrudes out post 241 and a guide pillar 242, this protrudes out the connected section 211 that post 241 stretches into this foot piece 21 separatably, this connected section 211 protruding out post 241 and this foot piece 21 not must instrument can easily and fast assembling-disassembling, this guide pillar 242 connects this second drive division 2113 separatably, and this second drive division 2113 can be passed this guide pillar 242 and drive this yaw rudder 24 to protrude out post 241 put relative to this foot piece 21 pivot for axle center with this.
These two wing groups 30 comprise the one first plate wing 31, the 1 second plate wing 32,1 first conjunction 33,1 second conjunction 34 and at least two brace panels 35 respectively, these two wing groups 30 are roughly the same in structure, therefore one of them is described in detail with these two wing groups 30.This the first plate wing 31, this first conjunction 33, this second conjunction 34 and this second plate wing 32 are along Y-axis sequential, and this first conjunction 33 connects this first plate wing 31, this second conjunction 34 connects this second plate wing 32, this second conjunction 34 connects this first conjunction 33 separatably, this the first plate wing 31 connects this housing 11, these at least two brace panels 35 one of them be arranged at this first plate wing 31 one of them also connect this first conjunction 33 along Z axis two opposite sides, another this brace panel 35 is arranged at this second plate wing 32, and along Z axis two opposite sides, one of them also connects this second conjunction 34.In the present embodiment, each this wing group 30 comprises four brace panels 35, this four brace panel 35 wherein two be arranged at this first plate wing 31 along Z axis two opposite sides, another two these brace panels 35 are arranged at this second plate wing 32 along Z axis two opposite sides, each this brace panel 35 is carbon fiber board, this four brace panel 35 is strengthened the aerofoil profile intensity of this first plate wing 31 and this second plate wing 32 respectively and makes this first plate wing 31 not yielding with this second plate wing 32, and then increase the buoyancy of this wing group 30, and this first plate wing 31 is the poly-mer of foaming with this second plate wing 32.This first conjunction 33 arranges a positioning groove 331, this second conjunction 34 arranges one convex section 341, this convex section 341 is stretched into this positioning groove 331 separatably, this positioning groove 331 can easily and dismounting rapidly with this convex section 341, structure by means of this wing group 30 reduces the storage space of this unmanned vehicle, in the present embodiment, the cross section of this positioning groove 331 is rectangular respectively, and this cross section of convex section 341 is rectangular corresponding to the cross section of this positioning groove 331.
Continue with reference to figure 2, Fig. 5 and Fig. 6, this unmanned vehicle has a flight position and a collapsed position, when this unmanned vehicle is positioned at this flight position, this convex extension part 222 is put towards arrow reversing sense relative to this groove 122 pivot, and make these two the second engaging portion 221 snappings these two the first engaging portion 121, this fuselage group 10 arranges along X-axis with this tail group 20, this elevating rudder 23 and this yaw rudder 24 are assembled to the connected section 211 of this foot piece 21, and these two the second plate wings 32 are assembled to these two the first plate wings 31 respectively.When this unmanned vehicle is positioned at this collapsed position, this convex extension part 222 is put along the direction of arrow relative to relative to this groove 122 pivot, and make these two the second engaging portion 221 depart from these two the first engaging portion 121, this fuselage group 10 arranges along Z axis with this tail group 20, this elevating rudder 23 and this yaw rudder 24 depart from the connected section 211 of this foot piece 21, and these two the second plate wings 32 depart from these two the first plate wings 31 respectively.
With reference to figure 7, when this unmanned vehicle is positioned at this flight position, one empty clap device B can easily carry in the shaft 212 of this foot piece 21.When user operates unmanned vehicle flight, this sky bat device B being arranged at this foot piece 21 can carry out photographing or taking pictures.
In sum, the utility model unmanned vehicle has the following advantages:
1. when this unmanned vehicle is positioned at this flight position, this convex extension part 222 is put relative to this groove 122 pivot, and make these two the second engaging portion 221 snappings these two the first engaging portion 121, this fuselage group 10 arranges along X-axis with this tail group 20, this elevating rudder 23 and this yaw rudder 24 are assembled to the connected section 211 of this foot piece 21, these two the second plate wings 32 are assembled to these two the first plate wings 31 respectively, and user can operate this unmanned vehicle in airflight.When this unmanned vehicle is positioned at this collapsed position, this convex extension part 222 is put relative to this groove 122 pivot, and make these two the second engaging portion 221 depart from these two the first engaging portion 121, this fuselage group 10 arranges along Z axis with this tail group 20, this elevating rudder 23 and this yaw rudder 24 depart from the connected section 211 of this foot piece 21, these two the second plate wings 32 depart from these two the first plate wings 31 respectively, and this unmanned vehicle can be positioned in automobile by user easily.
2. user only must pull this tail group 20 and puts relative to this fuselage group 10 pivot, these two the first engaging portion 121 are made to fasten with these two the second engaging portion 221 or depart from mutually, and the first plate wing 31 of these two wing groups 30 and the second plate wing 32 are assembled or depart from mutually, this elevating rudder 23 and this yaw rudder 24 are assembled or depart from this foot piece 21, can easily and rapidly this unmanned vehicle is converted in this flight position and this collapsed position.
3. this first plate wing 31 relying on each this wing group 30 is the poly-mer of foaming with this second plate wing 32, each this brace panel 35 is carbon fiber board, this four brace panel 35 is strengthened the aerofoil profile intensity of this first plate wing 31 and this second plate wing 32 respectively and makes this first plate wing 31 not yielding with this second plate wing 32, and then increase the buoyancy of each this wing group 30, and each this wing group 30 expendable weight and there is firm structure, make this unmanned vehicle can reduce energy resource consumption in time flying, and in time landing, each this wing group 30 can bear the shock of a fall power.
Claims (10)
1. a unmanned vehicle, is characterized in that, it comprises:
One fuselage group, it comprises a housing and one first pivotal part, and this first pivotal part connects this housing, and this first pivotal part has at least one first engaging portion;
One tail group, it comprises a foot piece and one second pivotal part, this second pivotal part connects this foot piece, this this first pivotal part of the second pivotal part pivot joint also has at least one second engaging portion, this at least one second engaging portion is this at least one first engaging portion of snapping separatably, and this foot piece can be put relative to this housing pivot.
2. unmanned vehicle as claimed in claim 1, it is characterized in that: this first pivotal part has two the first engaging portion and a groove, these two the first engaging portion are arranged at the two opposite sides of this groove respectively, this second pivotal part has two the second engaging portion and a convex extension part, these two second engaging portion are arranged at this convex extension part two opposite sides respectively, this this groove of convex extension part pivot joint, these two second engaging portion are these two first engaging portion of snapping separatably.
3. unmanned vehicle as claimed in claim 2, it is characterized in that: this first pivotal part has one first perforation, this first perforation runs through this first pivotal part and is communicated with this groove, this second pivotal part has one second perforation, this second perforation runs through this convex extension part, one wears part wears this first perforation and second to bore a hole with this, and this second pivotal part can wear part for putting relative to this first pivotal part pivot in axle center with this.
4. unmanned vehicle as claimed in claim 2, it is characterized in that: this housing has an accommodation space, one opening and two registration masts, this accommodation space of this open communication, these two registration masts to be arranged in this accommodation space and to lay respectively at this opening two opposite sides, this first pivotal part has two location flanges and is placed in this accommodation space, and the groove of this first pivotal part is towards this opening, these two location flanges lay respectively at this first pivotal part two opposite sides, this groove is between these two location flanges, these two location flange one of them recline these two registration masts one of them, another this registration mast and another this location flange reclines.
5. the unmanned vehicle according to any one of Claims 1-4, it is characterized in that, also comprise two wing groups, each this wing group comprises the one first plate wing, the one second plate wing, one first conjunction and one second conjunction, these two the first plate wings are arranged at this housing two opposite sides respectively, this first conjunction and this first plate wing of each this wing group are connected to each other, this second conjunction and this second plate wing of each this wing group are connected to each other, and this second conjunction of each this wing group is connected mutually separatably with this first conjunction.
6. unmanned vehicle as claimed in claim 5, it is characterized in that: each this wing group comprises at least two brace panels, these at least two brace panels one of them be arranged at this first plate wing and connect this first conjunction, another this brace panel is arranged at this second plate wing and connects this second conjunction, each this brace panel is carbon fiber board, and each this first plate wing and each this second plate wing are respectively the poly-mer of foaming.
7. unmanned vehicle as claimed in claim 5, it is characterized in that: each this first conjunction arranges a positioning groove, each this second conjunction arranges one convex section, the convex section of positioning groove departing from ground and connect each this first conjunction of each this second conjunction, the rectangular in cross-section of each this positioning groove, and each this cross section of convex section corresponds respectively to the cross section of each this positioning groove and rectangular.
8. unmanned vehicle as claimed in claim 5, it is characterized in that: this foot piece has a connected section away from one end of this second pivotal part, this tail group comprises an elevating rudder and a yaw rudder, this elevating rudder and this yaw rudder are connected the connected section of this foot piece respectively separatably, the connected section of this foot piece arranges two nose bar portions and one first drive division, this first driving part is between these two nose bar portions, this first drive division stretches into this elevating rudder separatably, this elevating rudder comprises two attaching partss, these two attaching partss have a stretch section and a tank respectively, these two tanks are arranged at these two stretch sections respectively and rely on the elastic deformation of these two stretch sections respectively and connect this two nose bar portions separatably, this first drive division can pass two attaching partss of this elevating rudder relative to this second pivotal part pivot pendulum can with these two nose bar portions for axle center be put relative to this foot piece pivot.
9. unmanned vehicle as claimed in claim 8, it is characterized in that: the connected section of this foot piece arranges one second drive division, this yaw rudder comprises one and protrudes out post and a guide pillar, this protrudes out the connected section that post stretches into this foot piece separatably, this guide pillar connects this second drive division separatably, and this second drive division can be passed this guide pillar relative to this second pivotal part pivot pendulum and drive this yaw rudder to protrude out post for putting relative to this foot piece pivot in axle center with this.
10. unmanned vehicle as claimed in claim 8, it is characterized in that: this foot piece has a shaft, this shaft is between this connected section and this second pivotal part, and the cross section of this shaft is rounded.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520558642.3U CN205010465U (en) | 2015-07-29 | 2015-07-29 | Unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520558642.3U CN205010465U (en) | 2015-07-29 | 2015-07-29 | Unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205010465U true CN205010465U (en) | 2016-02-03 |
Family
ID=55209079
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520558642.3U Expired - Fee Related CN205010465U (en) | 2015-07-29 | 2015-07-29 | Unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205010465U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106275376A (en) * | 2016-08-31 | 2017-01-04 | 北京奇正数元科技股份有限公司 | A kind of center framework of small-sized unmanned plane |
| CN106945816A (en) * | 2017-03-01 | 2017-07-14 | 北京天恒长鹰科技股份有限公司 | Deformable unmanned plane and its deformable component |
| CN109260721A (en) * | 2018-11-08 | 2019-01-25 | 重庆大学 | A kind of model rocket of pinpoint landing |
-
2015
- 2015-07-29 CN CN201520558642.3U patent/CN205010465U/en not_active Expired - Fee Related
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106275376A (en) * | 2016-08-31 | 2017-01-04 | 北京奇正数元科技股份有限公司 | A kind of center framework of small-sized unmanned plane |
| CN106275376B (en) * | 2016-08-31 | 2018-05-04 | 北京奇正数元科技股份有限公司 | A kind of center framework of small-sized unmanned plane |
| CN106945816A (en) * | 2017-03-01 | 2017-07-14 | 北京天恒长鹰科技股份有限公司 | Deformable unmanned plane and its deformable component |
| CN106945816B (en) * | 2017-03-01 | 2019-03-15 | 北京天恒长鹰科技股份有限公司 | Deformable unmanned plane and its deformable component |
| CN109260721A (en) * | 2018-11-08 | 2019-01-25 | 重庆大学 | A kind of model rocket of pinpoint landing |
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Granted publication date: 20160203 Termination date: 20180729 |