CN206202704U - The modular removable formula nacelle of unmanned plane - Google Patents
The modular removable formula nacelle of unmanned plane Download PDFInfo
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- CN206202704U CN206202704U CN201621292919.3U CN201621292919U CN206202704U CN 206202704 U CN206202704 U CN 206202704U CN 201621292919 U CN201621292919 U CN 201621292919U CN 206202704 U CN206202704 U CN 206202704U
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- electricity
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- radome fairing
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- floor
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Abstract
The utility model discloses a kind of modular removable formula nacelle of unmanned plane, it uses modularized design, it is overall to be connected by latch with the outer section of wing, the inner segment wing respectively, the nacelle adjusts part to constitute by power section, support section, wing connection point and electricity, power section and wing connection are separately mounted to the front-end and back-end of support section, and electricity adjusts the inside for being partially installed on support section.It is of the present utility model to be beneficial in that：Nacelle has been designed to modularization, Demountable by the utility model, not only can very easily be repaired and be changed, and modular design is more beneficial for debugging.
Description
Technical field
The utility model is related to a kind of nacelle, and in particular to a kind of modular removable formula power of unmanned plane is short
Cabin, belongs to unmanned air vehicle technique field.
Background technology
The dynamical system of unmanned plane is used for providing thrust for the flight of unmanned plane, is particularly significant during unmanned aerial vehicle design is manufactured
A part.
Due to the dynamical system of existing unmanned plane be connected firmly with body together with, so can actually making to unmanned plane
With many inconvenience are brought, for example：
(1) unmanned plane is when different task is performed, it may be necessary to change different dynamical systems, such as：In plateau flight,
Need to change the dynamical system of more high thrust, connected firmly with body due to the dynamical system of unmanned plane together with, so needs are whole
Operated on individual body, it is impossible to be rapidly completed replacing.
(2) when wanting the design development on existing unmanned plane, such as：Remodeling turns into the power VUAV that verts,
Together with being connected firmly with body due to the dynamical system of unmanned plane, so successfully remodeling is not easy to accomplish.
Utility model content
To solve the deficiencies in the prior art, the purpose of this utility model is to provide a kind of modular removable of unmanned plane
Formula nacelle.
In order to realize above-mentioned target, the utility model is adopted the following technical scheme that：
The modular removable formula nacelle of a kind of unmanned plane, it is characterised in that use modularized design, overall difference
It is connected by latch with the outer section of wing, the inner segment wing, the nacelle is by power section (10), support section (20), wing connection
(30) and electricity is divided to adjust part (40) composition, power section (10) and wing connection to divide (30) to be separately mounted to support section (20)
Front-end and back-end, electricity adjust part (40) installed in the inside of support section (20), wherein,
Foregoing support section (20) includes：It is radome fairing (201) on support section, right floor (202), bearing (203), spacing
Block (204), the first wire casing (205), the second wire casing (206), steering wheel (207), steering wheel frame (208), rocking arm (209), connecting rod
(210), radome fairing (212) under left floor (211) and support section, wherein,
Foregoing limited block (204) is fixedly connected by screw with left floor (211) and right floor (202), aforementioned bearings
(203) be respectively pressed into the groove of left floor (211) and right floor (202), for power section (10) clamping, foregoing connecting rod
(210) on rocking arm (209), foregoing rocking arm (209) on the output shaft of steering wheel (207), lead to by foregoing steering wheel (207)
Cross screw to be fixedly mounted on steering wheel frame (208), foregoing first wire casing (205) is connected on the second wire casing (206), foregoing second
Wire casing (206) is connected on steering wheel frame (208), and foregoing steering wheel frame (208) is with left floor (211) and right floor (202) by spiral shell
Silk is fixedly connected, and radome fairing (212) is screwed and is connected under radome fairing (201) and support section on foregoing support section
On left floor (211) and right floor (202)；
Foregoing wing connection point (30) includes：Radome fairing (301), wing connect frame (302), connecting portion on coupling part
Divide radome fairing (304) under rear radome fairing (303) and coupling part, wherein,
Radome fairing (303) point behind radome fairing (304) and coupling part under radome fairing (301), coupling part on coupling part
Be not screwed connected above frame (302) installed in wing, below and rear end.
The modular removable formula nacelle of foregoing a kind of unmanned plane, it is characterised in that previous power part (10)
Including：Motor (101) and motor cabinet (102), wherein,
Aforementioned motor (101) is screwed and is installed in motor cabinet (102), on the outer wall of aforementioned motor seat (102)
Jump ring (103) and rotating shaft (104) are provided with, in the bearing (203) of aforementioned rotation axis (104) insertion support section (20), foregoing card
Spring (103) is stuck in rotating shaft (104).
A kind of modular removable formula nacelle of foregoing unmanned plane, it is characterised in that foregoing support section (20)
It is screwed with wing connection point (30) and is installed together.
The modular removable formula nacelle of foregoing a kind of unmanned plane, it is characterised in that foregoing electricity adjusts part (40)
Including：Electricity adjusts installing plate (401), upper strata heat conductive silica gel (402), electricity to adjust (403), lower floor's heat conductive silica gel (404) and electricity to adjust lid
(405), wherein,
Foregoing upper strata heat conductive silica gel (402) and lower floor's heat conductive silica gel (404) are attached to the both sides up and down that electricity adjusts (403) respectively,
Foregoing electricity is adjusted installing plate (401) and electricity to adjust lid (405) to be screwed and is installed together, and electricity adjusts installing plate (401) in upper, electricity
Tune lid (405) posts the electric of heat conductive silica gel and adjusts (403) to be positioned over by electricity tune installing plate (401) and electricity tune lid (405) institute shape under
Into cavity in.
The modular removable formula nacelle of foregoing a kind of unmanned plane, it is characterised in that foregoing electricity adjusts part (40)
It is screwed on the left floor (211) and right floor (202) of support section (20).
It is of the present utility model to be beneficial in that：Nacelle has been designed to modularization, detachable by the utility model
Structure, not only can very easily be repaired and be changed, and modular design is more beneficial for debugging.
Brief description of the drawings
Fig. 1 is the composition schematic diagram of modular removable formula nacelle of the present utility model；
Fig. 2 is the explosive view of modular removable formula nacelle of the present utility model；
Fig. 3 is the structural representation after modular removable formula nacelle assembling of the present utility model is finished；
Fig. 4 is the final assembly figure of modular removable formula nacelle of the present utility model.
The implication of reference in figure：10- power sections, 20- support sections, 30- wing connections point, 40- electricity tune portion
Point, 101- motors, 102- motor cabinets, 103- jump rings, 104- rotating shafts, radome fairing, the right floors of 202-, 203- on 201- support sections
Bearing, 204- limited blocks, the wire casings of 205- first, the wire casings of 206- second, 207- steering wheels, 208- steering wheels frame, 209- rocking arms, 210- connect
Radome fairing under the left floor of bar, 211-, 212- support sections, radome fairing, 302- wings connection frame, 303- connect on 301- coupling parts
After socket part point under radome fairing, 304- coupling parts radome fairing, 401- electricity adjust installing plate, 402- upper stratas heat conductive silica gel, 403- electricity to adjust,
404- lower floors heat conductive silica gel, 405- electricity adjust lid.
Specific embodiment
Make specific introduction to the utility model below in conjunction with the drawings and specific embodiments.
Reference picture 1, the modular removable formula nacelle of unmanned plane of the present utility model, using modularized design, bag
Include four most of：Power section 10, support section 20, wing connection point 30 and electricity adjust part 40.Wherein, the He of power section 10
Wing connection point 30 is separately mounted to the front-end and back-end of support section 20, and electricity adjusts part 40 to be arranged on the interior of support section 20
Portion.
The structure that power section 10, support section 20, wing connection point 30 and electricity adjust part 40 is introduced separately below.
First, power section
Reference picture 2, power section 10 includes：Motor 101 and motor cabinet 102.
Motor 101 is screwed and is installed in motor cabinet 102, and the He of jump ring 103 is provided with the outer wall of motor cabinet 102
Rotating shaft 104.Wherein, jump ring 103 can be stuck in rotating shaft 104, and rotating shaft 104 is inserted into the support section 20 that will be introduced below
Bearing 203 in, power section 10 and support section 20 realize connection by rotating shaft 104 and the cooperation of bearing 203.
2nd, support section
Reference picture 2, support section 20 includes：Radome fairing 201, right floor 202, bearing 203, limited block on support section
204th, the first wire casing 205, the second wire casing 206, steering wheel 207, steering wheel frame 208, rocking arm 209, connecting rod 210, left floor 211 and support
The lower radome fairing 212 in part.
Limited block 204 is fixedly connected by screw with left floor 211 and right floor 202；Bearing 203 is respectively pressed into left floor
211 and right floor 202 groove in, bearing 203 be used for and the clamping of power section 10；Connecting rod 210 is arranged on rocking arm 209, rocking arm
209 are arranged on the output shaft of steering wheel 207, and steering wheel 207 is screwed on steering wheel frame 208；First wire casing 205 connects
It is connected on the second wire casing 206, the second wire casing 206 is connected on steering wheel frame 208；Steering wheel frame 208 and left floor 211 and right floor
202 are screwed connection；Radome fairing 212 is screwed connection under radome fairing 201 and support section on support section
On left floor 211 and right floor 202.
3rd, wing connection point
Reference picture 2, wing connection point 30 includes：Radome fairing 301, wing connection frame 302, coupling part on coupling part
Radome fairing 304 under radome fairing 303 and coupling part afterwards.
Radome fairing 301 is screwed above wing connection frame 302 on coupling part, whole under coupling part
Stream cover 304 is screwed below wing connection frame 302, and radome fairing 303 is screwed behind coupling part
The rear end of frame 302 is connected installed in wing.
Support section 20 and wing connection point 30 are screwed and are installed together.
4th, electricity adjusts part
Reference picture 2, electricity tune part 40 includes：Electricity adjusts installing plate 401, upper strata heat conductive silica gel 402, electricity to adjust 403, lower floor's heat conduction
Silica gel 404 and electricity adjust lid 405.
Upper strata heat conductive silica gel 402 and lower floor's heat conductive silica gel 404 are attached to the both sides up and down that electricity adjusts 403 respectively；Electricity adjusts installing plate
401 adjust lid 405 to be screwed with electricity is installed together, and electricity adjusts installing plate 401 to adjust lid 405 under upper, electric, posts heat conduction
The electricity of silica gel adjusts 403 to be positioned in the cavity for adjusting installing plate 401 and electricity to adjust lid 405 to be formed by electricity.
Electricity adjusts part 40 to be screwed on the left floor 211 and right floor 202 of support section 20.
Installation method：
1st step：Motor 101 is screwed and is installed in motor cabinet 102；
2nd step：Connecting rod 210 is arranged on rocking arm 209, rocking arm 209 is arranged on the output shaft of steering wheel 207, by rudder
Machine 207 is screwed on steering wheel frame 208；
3rd step：First wire casing 205 is connected on the second wire casing 206, the second wire casing 206 is connected to steering wheel frame 208
On, steering wheel frame 208 is screwed and be connected with left floor 211 and right floor 202；
4th step：Bearing 203 is respectively pressed into the groove of left floor 211 and right floor 202, limited block 204 is passed through into screw
It is fixedly connected with left floor 211 and right floor 202, radome fairing 212 under radome fairing on support section 201 and support section is passed through
Screw is fixedly connected on left floor 211 and right floor 202；
5th step：303 points of radome fairing behind radome fairing 304 and coupling part under radome fairing 301, coupling part on coupling part
Be not screwed installed in wing connection frame 302 above, below and rear end；
6th step：Upper strata heat conductive silica gel 402 and lower floor's heat conductive silica gel 404 are attached to the both sides up and down that electricity adjusts 403 respectively, will
The electricity for posting heat conductive silica gel adjusts 403 to be positioned in the cavity for adjusting installing plate 401 and electricity to adjust lid 405 to be formed by electricity, electricity is adjusted and is pacified
Dress plate 401 and electricity are adjusted lid 405 to be screwed and are installed together；
7th step：During the rotating shaft 104 of power section 10 inserted into the bearing 203 of support section 20, jump ring 103 is stuck in rotating shaft
On 104；
8th step：Wing connection point 30 is screwed installed in the rear end of support section 20；
9th step：Part 40 is adjusted to be screwed left floor 211 and right floor 202 installed in support section 20 electricity
On.
Nacelle after assembling is finished is as shown in Figure 3.
Reference picture 4, nacelle of the present utility model is integrally connected with the outer section of wing, the inner segment wing by latch respectively, from
And form a complete unmanned plane structure.
Because nacelle has been designed to modularization, Demountable by the utility model, so not only can be very square
Carrying out just is repaired and is changed, and modular design is more beneficial for debugging.
It should be noted that above-described embodiment does not limit the utility model in any form, all use equivalents or wait
The technical scheme that the mode of conversion is obtained is imitated, is all fallen within protection domain of the present utility model.
Claims (5)
1. the modular removable formula nacelle of a kind of unmanned plane, it is characterised in that use modularized design, it is overall respectively with
Outer section of wing, the inner segment wing are connected by latch, and the nacelle is by power section (10), support section (20), wing connection point
(30) constituted with electricity tune part (40), power section (10) and wing connection point (30) are separately mounted to support section (20)
Front-end and back-end, electricity adjusts part (40) installed in the inside of support section (20), wherein, the support section (20) includes：Branch
Support part point upper radome fairing (201), right floor (202), bearing (203), limited block (204), the first wire casing (205), the second wire casing
(206), steering wheel (207), steering wheel frame (208), rocking arm (209), connecting rod (210), left floor (211) and radome fairing under support section
(212), wherein,
The limited block (204) is fixedly connected by screw with left floor (211) and right floor (202), the bearing (203) point
Be not pressed into the groove of left floor (211) and right floor (202), for power section (10) clamping, the connecting rod (210) installs
On rocking arm (209), the rocking arm (209) is on the output shaft of steering wheel (207), and the steering wheel (207) is solid by screw
On steering wheel frame (208), first wire casing (205) is connected on the second wire casing (206), second wire casing for Dingan County
(206) it is connected on steering wheel frame (208), the steering wheel frame (208) is solid by screw with left floor (211) and right floor (202)
Fixed connection, radome fairing (212) is screwed and is connected to left rib under radome fairing (201) and support section on the support section
On plate (211) and right floor (202)；
The wing connection point (30) includes：After radome fairing (301), wing connect frame (302), coupling part on coupling part
Radome fairing (304) under radome fairing (303) and coupling part, wherein,
Radome fairing (303) leads to respectively behind radome fairing (304) and coupling part under radome fairing (301), coupling part on coupling part
Cross screw and be fixedly mounted on wing and connect above frame (302), below and rear end.
2. the modular removable formula nacelle of a kind of unmanned plane according to claim 1, it is characterised in that described dynamic
Power part (10) includes：Motor (101) and motor cabinet (102), wherein,
The motor (101) is screwed and is installed in motor cabinet (102), is set on the outer wall of the motor cabinet (102)
There are jump ring (103) and rotating shaft (104), in the bearing (203) of the rotating shaft (104) insertion support section (20), the jump ring
(103) it is stuck in rotating shaft (104).
3. a kind of modular removable formula nacelle of unmanned plane according to claim 1, it is characterised in that the branch
Support part point (20) and wing connection point (30) are screwed and are installed together.
4. a kind of modular removable formula nacelle of unmanned plane according to claim 1, it is characterised in that the electricity
Adjusting part (40) includes：Electricity adjusts installing plate (401), upper strata heat conductive silica gel (402), electricity to adjust (403), lower floor's heat conductive silica gel (404)
Lid (405) is adjusted with electricity, wherein,
The upper strata heat conductive silica gel (402) and lower floor's heat conductive silica gel (404) are attached to the both sides up and down that electricity adjusts (403) respectively, described
Electricity is adjusted installing plate (401) and electricity to adjust lid (405) to be screwed and is installed together, and electricity adjusts installing plate (401) to adjust lid upper, electric
(405) under, post the electric of heat conductive silica gel and adjust (403) to be positioned over what is formed by electricity tune installing plate (401) and electricity tune lid (405)
In cavity.
5. a kind of modular removable formula nacelle of unmanned plane according to claim 4, it is characterised in that the electricity
Part (40) is adjusted to be screwed on the left floor (211) and right floor (202) of support section (20).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621292919.3U CN206202704U (en) | 2016-11-29 | 2016-11-29 | The modular removable formula nacelle of unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621292919.3U CN206202704U (en) | 2016-11-29 | 2016-11-29 | The modular removable formula nacelle of unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206202704U true CN206202704U (en) | 2017-05-31 |
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ID=58750809
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621292919.3U Active CN206202704U (en) | 2016-11-29 | 2016-11-29 | The modular removable formula nacelle of unmanned plane |
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| Country | Link |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106379544A (en) * | 2016-11-29 | 2017-02-08 | 北京奇正数元科技股份有限公司 | Modularized and detachable type power nacelle of unmanned aerial vehicle |
| WO2020000206A1 (en) * | 2018-06-26 | 2020-01-02 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle |
-
2016
- 2016-11-29 CN CN201621292919.3U patent/CN206202704U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106379544A (en) * | 2016-11-29 | 2017-02-08 | 北京奇正数元科技股份有限公司 | Modularized and detachable type power nacelle of unmanned aerial vehicle |
| WO2020000206A1 (en) * | 2018-06-26 | 2020-01-02 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle |
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