CN206050071U - It is a kind of to lift easily unmanned plane - Google Patents
It is a kind of to lift easily unmanned plane Download PDFInfo
- Publication number
- CN206050071U CN206050071U CN201620982175.1U CN201620982175U CN206050071U CN 206050071 U CN206050071 U CN 206050071U CN 201620982175 U CN201620982175 U CN 201620982175U CN 206050071 U CN206050071 U CN 206050071U
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- unmanned plane
- wing
- thermal insulation
- insulation board
- connecting tube
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Abstract
This utility model discloses a kind of lifting easily unmanned plane, including fixed-wing unmanned plane body and the vertical lift wing, the first mortise is provided with the fixed-wing unmanned plane body, the fixed-wing unmanned plane is originally provided with the angular mounting hole that three ends are interconnected in vivo, the angular mounting hole is connected with insert port, the insert port is distributed in triangular shape, the vertical lift wing includes connecting tube, elbow, motor, electricity mediation elevating screw, the first tenon matched with the first mortise and the shape memory alloy strip matched with angular mounting hole are provided with the connecting tube；The lifting is affected less by landform when easily unmanned plane is lifted.
Description
Technical field
This utility model is related to a kind of lifting easily unmanned plane.
Background technology
UAV referred to as " unmanned plane ", is manipulated using radio robot and the presetting apparatus provided for oneself
Not manned aircraft.Without driving cabin on machine, but the equipment such as automatic pilot, presetting apparatus are installed.On ground, naval vessels or
Machine tool remote control station personnel by the equipment such as radar, which is tracked, is positioned, remote control, remote measurement and Digital Transmission.Can be in radio
As conventional airplane take off or launched with booster rocket under remote control, also aerial input can be taken to by machine tool and be flown.Reclaim
When, the mode automatic Landing as conventional airplane landing mission is can use, also can be passed through remote control parachute or block is reclaimed.Can
Repetitiousness is using multiple.It is widely used in the aspects such as photography, military affairs, transport development, hydraulic engineering, ecological Studies and urban planning.
But the unmanned plane lifting for being currently used in various aspects needs harsher landform, lifts very dumb.
Utility model content
When the technical problems to be solved in the utility model is to provide a kind of lifting by landform the less lifting of impact just
Prompt unmanned plane.
To solve the above problems, this utility model is adopted the following technical scheme that：
A kind of lifting easily unmanned plane, including fixed-wing unmanned plane body and the vertical lift wing, the fixed-wing nobody
The first mortise is provided with machine body, the fixed-wing unmanned plane is originally provided with the inclination installation that three ends are interconnected in vivo
Hole, the angular mounting hole are connected with insert port, and the insert port is distributed in triangular shape, and the vertical lift wing includes connection
Pipe, elbow, electric mechanical, electrical mediation elevating screw, be provided with the connecting tube the first tenon for matching with the first mortise and
The shape memory alloy strip matched with angular mounting hole.
Preferably, the fixed-wing unmanned plane body include fuselage, wing, empennage, dynamical system, control system and
Accumulator, dynamical system by brushless electric machine, it is brushless electricity reconcile propelling screws, control system by rudder, elevator, fly control,
Attitude transducer, gps antenna and electronic compass composition.
Preferably, the angular mounting hole and the first mortise are respectively positioned on wing lower surface, with certain concealment effect,
The impact of outward appearance is less.
Preferably, shape memory alloy strip can be inserted by the tapered uncovered structure of the insert port with convenient use person
In angular mounting hole.
Preferably, the shape memory alloy strip includes linkage section and tilting section, the linkage section is embedded in connection
Pipe is arranged, and Stability Analysis of Structures is connected firmly.
Preferably, the gradient of the angular mounting hole is identical with the gradient of tilting section, angular mounting hole with incline
The compatible degree of section is high, and structure can be caused more stable, can prevent tilting section from shake occurring in angular mounting hole.
Preferably, the connecting tube both ends of the surface are provided with the second mortise, described elbow one end is provided with the second tenon,
The connecting tube and elbow pass through the second tenon and the second mortise connects, and connecting tube is combined with each other support mutually, stress with elbow
Stability Analysis of Structures reliability.
Preferably, reinforcement is provided with the connecting tube, the reinforcement is provided with one or more, the reinforcement
It is distributed in the shape of a spiral, the midpoint of the reinforcement is respectively positioned on same straight line, the reinforcement is hollow setting, not only can be carried
The intensity of connecting tube is risen, and weight amplification is little.
Preferably, thermal insulation board is provided with the elbow, the thermal insulation board is parallel with the upper surface of elbow, it is described every
Hot plate is bonded with elbow, and the motor is located in the middle part of the upper surface of thermal insulation board, and the electricity is transposed in the lower surface of thermal insulation board, described
Motor is connected with elevating screw, and the motor and electricity are adjusted and be detachably connected with thermal insulation board, and the motor and thermal insulation board are in
Cylinder is arranged, and the motor is perpendicular with thermal insulation board, and simple structure, good stability can be prevented to fixed-wing unmanned plane sheet
The balance of body is affected.
Preferably, the vertical lift wing is provided with two, the vertical lift wing is symmetric.
The beneficial effects of the utility model are：Being provided by the vertical lift wing allows fixed-wing unmanned plane to be hung down
Straight takeoff and landing, lifts flexible compared with traditional unmanned plane, is affected less by surface state, when can close after rise
The motor of the vertical lift wing is closed, is then flown using the dynamical system of fixed-wing unmanned plane body itself, manipulation is flexible, and
And electric energy can be effectively saved, while having used the mode of dual fixation to connect fixed-wing unmanned plane body and the vertical lift wing
Connect, structural stability is good, effectively can prevent from occurring in flight course shake, the situation that comes off and loosen and cause entirety
Balance be affected, additionally, angular mounting hole and the first mortise are respectively positioned on wing lower surface, with certain hiding effect
Really, the impact of outward appearance is less, the tapered uncovered structure of insert port, can incline shape memory alloy strip insertion with convenient use person
In installing hole, shape memory alloy strip includes linkage section and tilting section, and the linkage section is embedded in connecting tube setting, and structure is steady
It is fixed, it is connected firmly, the gradient of angular mounting hole is identical with the gradient of tilting section, the compatible degree of angular mounting hole and tilting section
Height, can cause structure more stable, can prevent tilting section from shake occurring in angular mounting hole, and connecting tube both ends of the surface are all provided with
The second mortise is equipped with, elbow one end is provided with the second tenon, and connecting tube and elbow pass through the second tenon and the connection of the second mortise, even
Adapter is combined with each other support mutually with elbow, and force structure is reliable and stable, and reinforcement is provided with connecting tube, and reinforcement is helically
Shape is distributed, and the midpoint of reinforcement is located along the same line, and reinforcement is hollow setting, not only can lift the intensity of connecting tube,
And weight amplification is little, in elbow, be provided with thermal insulation board, the thermal insulation board is parallel with the upper surface of elbow, the thermal insulation board with
Elbow is bonded, and the motor is located in the middle part of the upper surface of thermal insulation board, and the electricity is transposed in the lower surface of thermal insulation board, the motor with
Elevating screw connects, and the motor and electricity are adjusted and be detachably connected with thermal insulation board, and the motor and thermal insulation board are in cylinder
Arrange, the motor is perpendicular with thermal insulation board, and simple structure, good stability can prevent from putting down fixed-wing unmanned plane body
Weighing apparatus property is affected.
Description of the drawings
For the technical scheme being illustrated more clearly that in this utility model embodiment, below will be to needed for embodiment description
Accompanying drawing to be used is briefly described, it should be apparent that, drawings in the following description are only some realities of the present utility model
Example is applied, for those of ordinary skill in the art, on the premise of not paying creative work, can be with according to these accompanying drawings
Obtain other accompanying drawings.
Fig. 1 is a kind of overall structure diagram for lifting easily unmanned plane of this utility model；
Fig. 2 is a kind of partial sectional view of the vertical lift wing for lifting easily unmanned plane of this utility model；
Fig. 3 is a kind of partial sectional view for lifting the easily fixed-wing unmanned plane body of unmanned plane of this utility model；
Fig. 4 is a kind of partial structural diagram for lifting the easily connecting rod of unmanned plane of this utility model；
Fig. 5 is that a kind of distribution for lifting the easily insert port of the fixed-wing unmanned plane body of unmanned plane of this utility model is shown
It is intended to；
Fig. 6 is a kind of structural representation for lifting the easily fixed-wing unmanned plane body of unmanned plane of this utility model；
Fig. 7 is a kind of front view for lifting the easily connecting tube of unmanned plane of this utility model；
Fig. 8 is a kind of front view for lifting the easily elbow of unmanned plane of this utility model；
Fig. 9 is a kind of structural representation for lifting the easily shape memory alloy strip of unmanned plane of this utility model；
Figure 10 is a kind of connection for lifting the easily dynamical system of unmanned plane, control system and accumulator of this utility model
Block diagram.
Specific embodiment
Embodiment 1
It is as Figure 1-5, a kind of to lift easily unmanned plane, including fixed-wing unmanned plane body 1 and the vertical lift wing 2,
The first mortise 3 is provided with the fixed-wing unmanned plane body 1, in the fixed-wing unmanned plane body 1, three ends is provided with
The angular mounting hole 4 being interconnected, the angular mounting hole 4 are connected with insert port 5, and the insert port 5 is distributed in triangular shape, institute
State the vertical lift wing 2 and include connecting tube 6, elbow 7, motor 8, electricity tune 9 and elevating screw 10, arrange in the connecting tube 6
There are the first tenon 11 matched with the first mortise 3 and the shape memory alloy strip 12 matched with angular mounting hole 4, by setting
Being equipped with the vertical lift wing 2 allows fixed-wing unmanned plane body 1 to carry out vertical and landing takeoff, compared with traditional unmanned plane
Lifting is flexible, is affected less by surface state, and the motor 8 of the vertical lift wing 2 can be closed after rise, then using solid
Determine 1 dynamical system of itself of wing unmanned plane body to be flown, manipulation is flexible, and can effectively save electric energy, while making
With the mode of dual fixation by fixed-wing unmanned plane body and vertical lift wing connection, structural stability is good, can be effective
Prevent from occurring in flight course shake, the situation that comes off and loosen and cause overall balance to be affected.
The present embodiment has the beneficial effect that：Being provided by the vertical lift wing allows fixed-wing unmanned plane to carry out vertically
Takeoff and landing, lifts flexible compared with traditional unmanned plane, is affected less by surface state, when can close after rise
The motor of the vertical lift wing, is then flown using the dynamical system of fixed-wing unmanned plane body itself, and manipulation is flexible, and
Electric energy can be effectively saved, while having used the mode of dual fixation to connect fixed-wing unmanned plane body and the vertical lift wing
Connect, structural stability is good, effectively can prevent from occurring in flight course shake, the situation that comes off and loosen and cause entirety
Balance be affected.
Embodiment 2
It is as shown in figs 1-9, a kind of to lift easily unmanned plane, including fixed-wing unmanned plane body 1 and the vertical lift wing 2,
The first mortise 3 is provided with the fixed-wing unmanned plane body 1, in the fixed-wing unmanned plane body 1, three ends is provided with
The angular mounting hole 4 being interconnected, the angular mounting hole 4 are connected with insert port 5, and the insert port 5 is distributed in triangular shape, institute
State the vertical lift wing 2 and include connecting tube 6, elbow 7, motor 8, electricity tune 9 and elevating screw 10, arrange in the connecting tube 6
There are the first tenon 11 matched with the first mortise 3 and the shape memory alloy strip 12 matched with angular mounting hole 4, it is described solid
Determine wing unmanned plane body 1 and include fuselage 13, wing 14, empennage 15, dynamical system, control system and accumulator, dynamical system
By brushless electric machine, it is brushless electricity reconcile propelling screws constitute, control system by rudder, elevator, fly control, attitude transducer,
Gps antenna and electronic compass composition, the angular mounting hole 4 and the first mortise 3 are respectively positioned on 14 lower surface of wing, with certain
Concealment effect, the impact of outward appearance are less, 5 tapered uncovered structure of the insert port, can close shape memory with convenient use person
In the insertion angular mounting hole 4 of gold bar 12, the shape memory alloy strip 12 includes linkage section 16 and tilting section 17, the connection
16 sections are embedded in connecting tube 6 and arrange, and Stability Analysis of Structures is connected firmly, the gradient of the angular mounting hole 4 and inclining for tilting section 17
Gradient is identical, and angular mounting hole 4 is high with the compatible degree of tilting section 17, and structure can be caused more stable, tilting section can be prevented
17 there is shake in angular mounting hole 4, and 6 both ends of the surface of the connecting tube are provided with the second mortise 18, and 7 one end of the elbow sets
It is equipped with the second tenon 19, the connecting tube 6 and elbow 7 passes through the second tenon 19 and the second mortise 18 connects, connecting tube 6 and elbow
7 are combined with each other support mutually, and force structure is reliable and stable, and reinforcement 20 is provided with the connecting tube 6, and the reinforcement is arranged
There is one or more, the reinforcement 20 is distributed in the shape of a spiral, the midpoint of the reinforcement 20 is respectively positioned on same straight line, it is described to add
Strong muscle 20 is hollow setting, not only can lift the intensity of connecting tube, and weight amplification is little, overall balance is affected compared with
It is few, is provided with thermal insulation board 21 in the elbow 7, the thermal insulation board 21 is parallel with the upper surface of elbow 7, the thermal insulation board 21 and
Elbow 7 is bonded, and the motor 8 is located in the middle part of the upper surface of thermal insulation board 21, and the electricity adjusts 9 lower surfaces for being located at thermal insulation board 21, institute
State motor 8 to be connected with elevating screw 10, the motor 8 and electricity adjust 9 to be detachably connected with thermal insulation board 21,8 He of the motor
, in cylinder setting, the motor 8 is perpendicular with thermal insulation board 21, simple structure, good stability, and it is right to prevent for thermal insulation board 21
The balance of fixed-wing unmanned plane body 1 is affected, and is provided by being vertically moved up or down the wing 2 and causes the fixed-wing unmanned plane 1 can be with
Vertical and landing takeoff is carried out, is lifted flexibly compared with traditional unmanned plane, is affected less by surface state, after rise
The motor 8 of the vertical lift wing 2 can be closed, is then flown using 1 dynamical system of itself of fixed-wing unmanned plane body, be grasped
Control is flexible, and can effectively save electric energy, while having used the mode of dual fixation by fixed-wing unmanned plane body and having hung down
Straight elevating plane connection, structural stability are good, can effectively prevent the situation for shake occur in flight course, coming off and loosen
And cause overall balance to be affected.
The present embodiment has the beneficial effect that：Being provided by the vertical lift wing allows fixed-wing unmanned plane to carry out vertically
Takeoff and landing, lifts flexible compared with traditional unmanned plane, is affected less by surface state, when can close after rise
The motor of the vertical lift wing, is then flown using the dynamical system of fixed-wing unmanned plane body itself, and manipulation is flexible, and
Electric energy can be effectively saved, while having used the mode of dual fixation to connect fixed-wing unmanned plane body and the vertical lift wing
Connect, structural stability is good, effectively can prevent from occurring in flight course shake, the situation that comes off and loosen and cause entirety
Balance be affected, angular mounting hole and the first mortise are respectively positioned on wing lower surface, with certain concealment effect, outward appearance
Impact it is less, shape memory alloy strip can be inserted angular mounting hole with convenient use person by the tapered uncovered structure of insert port
Interior, shape memory alloy strip includes linkage section and tilting section, and the linkage section is embedded in connecting tube setting, and Stability Analysis of Structures connects
Connect firmly, the gradient of angular mounting hole is identical with the gradient of tilting section, angular mounting hole is high with the compatible degree of tilting section, can
So that structure is more stable, can prevent tilting section from shake occurring in angular mounting hole, connecting tube both ends of the surface are provided with
Second mortise, elbow one end are provided with the second tenon, and connecting tube and elbow pass through the second tenon and the connection of the second mortise, connecting tube
Support mutually is combined with each other with elbow, force structure is reliable and stable, and reinforcement is provided with connecting tube, and reinforcement divides in the shape of a spiral
Cloth, the midpoint of reinforcement are located along the same line, and reinforcement is hollow setting, not only can lift the intensity of connecting tube, and
Weight amplification is little, and thermal insulation board is provided with elbow, and the thermal insulation board is parallel with the upper surface of elbow, the thermal insulation board and elbow
Bonding, the motor are located in the middle part of the upper surface of thermal insulation board, and the electricity is transposed in the lower surface of thermal insulation board, the motor and lifting
Propeller connects, and the motor and electricity are adjusted and be detachably connected with thermal insulation board, and the motor and thermal insulation board are in cylinder setting,
The motor is perpendicular with thermal insulation board, simple structure, good stability, can prevent from receiving the balance of fixed-wing unmanned plane body
To impact.
When mounted：First by 12 straightening of shape memory alloy strip in connecting tube 6, then slowly insert fixed-wing nobody
In the angular mounting hole 4 of machine body 1, until the first tenon 11 is completely inserted in the first mortise 3, be fixed then the wing nobody
Machine body 1 and connecting tube, till shape memory alloy strip 12 is restored to the original state completely so that shape memory alloy strip 12 is good
Catch fixed-wing unmanned plane body 1, you can.
The above, specific embodiment only of the present utility model, but protection domain of the present utility model do not limit to
In this, any change or replacement expected without creative work should all be covered within protection domain of the present utility model.
Claims (10)
- It is 1. a kind of to lift easily unmanned plane, it is characterised in that：It is including fixed-wing unmanned plane body and the vertical lift wing, described solid Determine on wing unmanned plane body, to be provided with the first mortise, the fixed-wing unmanned plane is originally provided with what three ends were interconnected in vivo Angular mounting hole, the angular mounting hole are connected with insert port, and the insert port is distributed in triangular shape, the vertical lift wing bag Containing connecting tube, elbow, electric mechanical, electrical mediation elevating screw, matched with the first mortise in the connecting tube, is provided with One tenon and the shape memory alloy strip matched with angular mounting hole.
- It is 2. according to claim 1 to lift easily unmanned plane, it is characterised in that：The fixed-wing unmanned plane body is included There are fuselage, wing, empennage, dynamical system, control system and accumulator.
- It is 3. according to claim 2 to lift easily unmanned plane, it is characterised in that：The angular mounting hole and the first mortise It is respectively positioned on wing lower surface.
- It is 4. according to claim 3 to lift easily unmanned plane, it is characterised in that：The tapered open knot of the insert port Structure.
- It is 5. according to claim 4 to lift easily unmanned plane, it is characterised in that：The shape memory alloy strip includes Linkage section and tilting section, the linkage section are embedded in connecting tube setting.
- It is 6. according to claim 5 to lift easily unmanned plane, it is characterised in that：The gradient of the angular mounting hole with The gradient of tilting section is identical.
- It is 7. according to claim 6 to lift easily unmanned plane, it is characterised in that：The connecting tube both ends of the surface are provided with Second mortise, described elbow one end are provided with the second tenon, and the connecting tube and elbow pass through the second tenon and the second mortise company Connect.
- It is 8. according to claim 7 to lift easily unmanned plane, it is characterised in that：Reinforcement is provided with the connecting tube Muscle, the reinforcement are provided with one or more, and the reinforcement is distributed in the shape of a spiral, and the midpoint of the reinforcement is respectively positioned on same On straight line, the reinforcement is hollow setting.
- It is 9. according to claim 8 to lift easily unmanned plane, it is characterised in that：Thermal insulation board is provided with the elbow, The thermal insulation board is parallel with the upper surface of elbow, and the thermal insulation board is bonded with elbow, and the motor is located at the upper end of thermal insulation board Middle face, the electricity are transposed in the lower surface of thermal insulation board, and the motor is connected with elevating screw, the motor and electricity adjust with Thermal insulation board is detachably connected, and, in cylinder setting, the motor is perpendicular with thermal insulation board for the motor and thermal insulation board.
- It is 10. according to claim 9 to lift easily unmanned plane, it is characterised in that：The vertical lift wing is provided with two It is individual.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620982175.1U CN206050071U (en) | 2016-08-30 | 2016-08-30 | It is a kind of to lift easily unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620982175.1U CN206050071U (en) | 2016-08-30 | 2016-08-30 | It is a kind of to lift easily unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206050071U true CN206050071U (en) | 2017-03-29 |
Family
ID=58377903
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620982175.1U Withdrawn - After Issue CN206050071U (en) | 2016-08-30 | 2016-08-30 | It is a kind of to lift easily unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206050071U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106240812A (en) * | 2016-08-30 | 2016-12-21 | 广州三飞航空科技有限公司 | One lifts unmanned plane easily |
-
2016
- 2016-08-30 CN CN201620982175.1U patent/CN206050071U/en not_active Withdrawn - After Issue
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106240812A (en) * | 2016-08-30 | 2016-12-21 | 广州三飞航空科技有限公司 | One lifts unmanned plane easily |
| CN106240812B (en) * | 2016-08-30 | 2018-08-03 | 广州三飞航空科技有限公司 | It is a kind of to lift easily unmanned plane |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| AV01 | Patent right actively abandoned | ||
| AV01 | Patent right actively abandoned |
Granted publication date: 20170329 Effective date of abandoning: 20180803 |