CN106379544B - The modular removable formula nacelle of unmanned plane - Google Patents
The modular removable formula nacelle of unmanned plane Download PDFInfo
- Publication number
- CN106379544B CN106379544B CN201611073960.6A CN201611073960A CN106379544B CN 106379544 B CN106379544 B CN 106379544B CN 201611073960 A CN201611073960 A CN 201611073960A CN 106379544 B CN106379544 B CN 106379544B
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- Prior art keywords
- electricity
- support section
- radome fairing
- floor
- steering engine
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D29/00—Power-plant nacelles, fairings, or cowlings
- B64D29/02—Power-plant nacelles, fairings, or cowlings associated with wings
Abstract
The invention discloses a kind of modular removable formula nacelles of unmanned plane, it uses modularized design, it is whole to be connected respectively with the outer section of wing, the inner segment wing by bolt, the nacelle adjusts part to form 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.The invention has the beneficial effects that：Nacelle has been designed to modularization, Demountable by the present invention, not only very easily can be carried out maintenance and be replaced, but also modular design is more advantageous to debugging.
Description
Technical field
The present invention relates to a kind of nacelles, and in particular to a kind of modular removable formula nacelle of unmanned plane belongs to
In 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 in unmanned aerial vehicle design manufacture
A part.
Due to the dynamical system of existing unmanned plane be connected firmly with body together with, so can actually make to unmanned plane
With bringing many inconvenience, such as：
(1) unmanned plane is when performing different task, it may be necessary to replace different dynamical systems, such as：In plateau flight,
Need replacing the dynamical system of more high thrust, connected firmly with body due to the dynamical system of unmanned plane together with, so needing whole
It is operated on a body, replacement can not be rapidly completed.
(2) want in design development on existing unmanned plane, such as：Remodeling becomes power vertical take-off and landing drone of verting,
Together with being connected firmly with body due to the dynamical system of unmanned plane, so successfully remodeling is not easy to accomplish.
The content of the invention
To solve the deficiencies in the prior art, the modular removable formula it is an object of the invention to provide a kind of unmanned plane is moved
Power nacelle.
In order to realize above-mentioned target, the present invention adopts the following technical scheme that：
A kind of modular removable formula nacelle of unmanned plane, which is characterized in that using modularized design, whole difference
It is connected with the outer section of wing, the inner segment wing by bolt, 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 divide (30) to be separately mounted to support section (20)
Front-end and back-end, electricity adjust part (40) be mounted on support section (20) inside, wherein,
Foregoing support section (20) includes：Radome fairing (201), right floor (202), bearing (203), /V on support section
Block (204), the first wire casing (205), the second wire casing (206), steering engine (207), steering engine 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) it is respectively pressed into the slot of left floor (211) and right floor (202), for being clamped with power section (10), foregoing connecting rod
(210) it is mounted on rocking arm (209), foregoing rocking arm (209) is mounted on the output shaft of steering engine (207), and foregoing steering engine (207) is logical
Screw to be crossed to be fixedly mounted on steering engine frame (208), foregoing first wire casing (205) is connected on the second wire casing (206), and foregoing second
Wire casing (206) is connected on steering engine frame (208), and foregoing steering engine frame (208) passes through spiral shell with left floor (211) and right floor (202)
Silk is fixedly connected, and radome fairing (212) is fixed by screws 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 connection 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 mounted on wing connection frame (302) the upper surface of, below and rear end.
The modular removable formula nacelle of foregoing a kind of unmanned plane, which is characterized in that previous power part (10)
Including：Motor (101) and motor cabinet (102), wherein,
Aforementioned motor (101), which is screwed, to be installed in motor cabinet (102), on the outer wall of aforementioned motor seat (102)
Clamp spring (103) and shaft (104) are provided with, aforementioned rotation axis (104) is inserted into the bearing (203) of support section (20), foregoing card
Spring (103) is stuck in shaft (104).
A kind of modular removable formula nacelle of foregoing unmanned plane, which is characterized in that foregoing support section (20)
It is screwed and is installed together with wing connection point (30).
The modular removable formula nacelle of foregoing a kind of unmanned plane, which is characterized in that foregoing electricity adjusts part (40)
Including：Electricity adjusts installing plate (401), upper strata heat conductive silica gel (402), electricity that (403), lower floor's heat conductive silica gel (404) and electricity is adjusted 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 adjusts installing plate (401) and electricity tune lid (405) to be screwed and be installed together, and electricity adjusts installing plate (401) upper, electric
Tune lid (405) posts the electric of heat conductive silica gel and (403) is adjusted 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, which is characterized in that foregoing electricity adjusts part (40)
It is screwed on the left floor (211) and right floor (202) of support section (20).
The invention has the beneficial effects that：Nacelle has been designed to modularization, Demountable by the present invention, not only
Very easily it can carry out maintenance and replace, and modular design is more advantageous to debugging.
Description of the drawings
Fig. 1 is the composition schematic diagram of the modular removable formula nacelle of the present invention；
Fig. 2 is the explosive view of the modular removable formula nacelle of the present invention；
Fig. 3 is the structure diagram after the modular removable formula nacelle assembling of the present invention；
Fig. 4 is the final assembly figure of the modular removable formula nacelle of the present invention.
The meaning of reference numeral in figure：10- power sections, 20- support sections, 30- wing connections point, 40- electricity tune portion
Divide, radome fairing, the right floors of 202-, 203- on 101- motors, 102- motor cabinets, 103- clamp springs, 104- shafts, 201- support sections
Bearing, 204- limited blocks, the first wire casings of 205-, the second wire casings of 206-, 207- steering engines, 208- steering engines 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 installing plate, 402- upper stratas heat conductive silica gel, 403- electricity is adjusted to adjust,
404- lower floors heat conductive silica gel, 405- electricity adjust lid.
Specific embodiment
Make specific introduce to the present invention below in conjunction with the drawings and specific embodiments.
With reference to Fig. 1, the modular removable formula nacelle of unmanned plane of the invention, using modularized design, including four
It is most of：Power section 10, support section 20, wing connection point 30 and electricity adjust part 40.Wherein, power section 10 and wing
Coupling part 30 is separately mounted to the front-end and back-end of support section 20, and electricity adjusts part 40 mounted on the inside of support section 20.
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
With reference to Fig. 2, power section 10 includes：Motor 101 and motor cabinet 102.
Motor 101, which is screwed, to be installed in motor cabinet 102, and 103 He of clamp spring is provided on the outer wall of motor cabinet 102
Shaft 104.Wherein, clamp spring 103 can be stuck in shaft 104, and shaft 104 is inserted into the support section that will be introduced below 20
Bearing 203 in, connection is realized in the cooperation that power section 10 and support section 20 pass through shaft 104 and bearing 203.
2nd, support section
With reference to Fig. 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 engine 207, steering engine 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 slot in, bearing 203 with power section 10 for being clamped；Connecting rod 210 is mounted on rocking arm 209, rocking arm
209 are mounted on the output shaft of steering engine 207, and steering engine 207 is screwed on steering engine 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 engine frame 208；Steering engine frame 208 and left floor 211 and right floor
202 are fixed by screws；Radome fairing 212 is fixed by screws under radome fairing 201 and support section on support section
On left floor 211 and right floor 202.
3rd, wing connection point
With reference to Fig. 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 mounted on wing connection frame 302 the upper surface of 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
Mounted on the rear end of wing connection frame 302.
Support section 20 and wing connection point 30 are screwed and are installed together.
4th, electricity adjusts part
With reference to Fig. 2, electricity adjusts part 40 to include：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 upper, electric lid 405 to be adjusted to post heat conduction under
The electricity of silica gel adjusts 403 to be positioned in the cavity for adjusting installing plate 401 and electricity that lid 405 is adjusted 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 mounted on rocking arm 209, rocking arm 209 is mounted on the output shaft of steering engine 207, by rudder
Machine 207 is screwed on steering engine 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 engine frame 208
On, steering engine frame 208 and left floor 211 and right floor 202 are fixed by screws；
4th step：Bearing 203 is respectively pressed into the slot 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：Radome fairing 303 divides behind radome fairing 304 and coupling part under radome fairing 301, coupling part on coupling part
Be not screwed mounted on wing connection frame 302 the upper surface of, 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 of electricity tune 403 respectively, it will
The electricity for posting heat conductive silica gel adjusts 403 to be positioned in the cavity for adjusting installing plate 401 and electricity that lid 405 is adjusted to be formed by electricity, and electricity is adjusted and is pacified
Loading board 401 and electricity are adjusted lid 405 to be screwed and are installed together；
7th step：The shaft 104 of power section 10 is inserted into the bearing 203 of support section 20, clamp spring 103 is stuck in shaft
On 104；
8th step：Wing connection point 30 is screwed mounted on the rear end of support section 20；
9th step：Part 40 is adjusted to be screwed mounted on the left floor 211 of support section 20 and right floor 202 electricity
On.
Nacelle after assembling is as shown in Figure 3.
With reference to Fig. 4, the nacelle of the present invention is integrally connected with the outer section of wing, the inner segment wing by bolt respectively, so as to shape
Into a complete unmanned plane structure.
Since nacelle has been designed to modularization, Demountable by the present invention, so not only can be very easily
It carries out maintenance and replaces, and modular design is more advantageous to debugging.
It should be noted that the invention is not limited in any way for above-described embodiment, it is all to use equivalent substitution or equivalent change
The technical solution that the mode changed is obtained, all falls in protection scope of the present invention.
Claims (3)
1. a kind of modular removable formula nacelle of unmanned plane, which is characterized in that using modularized design, it is whole respectively with
The outer section of wing, the inner segment wing are connected by bolt, and the nacelle is by power section (10), support section (20), wing connection point
(30) and electricity adjusts part (40) composition, and power section (10) and wing connection point (30) are separately mounted to support section (20)
Front-end and back-end, support section (20) and wing connection point (30), which are screwed, to be installed together, and electricity adjusts part (40)
Mounted on the inside of support section (20), wherein,
The power section (10) includes：Motor (101) and motor cabinet (102), wherein,
The motor (101), which is screwed, to be installed in motor cabinet (102), is set on the outer wall of the motor cabinet (102)
There are clamp spring (103) and shaft (104), the shaft (104) is inserted into the bearing (203) of support section (20), the clamp spring
(103) it is stuck in shaft (104)；
The support section (20) includes：Radome fairing (201), right floor (202), bearing (203), limited block on support section
(204), the first wire casing (205), the second wire casing (206), steering engine (207), steering engine frame (208), rocking arm (209), connecting rod (210),
Radome fairing (212) under left floor (211) and support section, wherein,
The limited block (204) is fixedly connected by screw with left floor (211) and right floor (202), the bearing (203) point
It is not pressed into the slot of left floor (211) and right floor (202), for being clamped with power section (10), connecting rod (210) installation
On rocking arm (209), the rocking arm (209) is mounted on the output shaft of steering engine (207), and the steering engine (207) is consolidated by screw
Dingan County is on steering engine frame (208), and first wire casing (205) is connected on the second wire casing (206), second wire casing
(206) it is connected on steering engine frame (208), the steering engine frame (208) is consolidated with left floor (211) and right floor (202) by screw
Fixed connection, radome fairing (212) is fixed by screws in 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：On coupling part behind radome fairing (301), wing connection frame (302), 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
It crosses screw and is fixedly mounted on wing connection frame (302) the upper surface of, following and rear end.
A kind of 2. modular removable formula nacelle of unmanned plane according to claim 1, which is characterized in that the electricity
Part (40) is adjusted to include：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 adjusts installing plate (401) and electricity tune lid (405) to be screwed and be installed together, and electricity adjusts installing plate (401) to be covered in upper, electric adjust
(405) under, post the electric of heat conductive silica gel and (403) is adjusted to be positioned over what is formed by electricity tune installing plate (401) and electricity tune lid (405)
In cavity.
A kind of 3. modular removable formula nacelle of unmanned plane according to claim 2, which is characterized 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 |
|---|---|---|---|
| CN201611073960.6A CN106379544B (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 |
|---|---|---|---|
| CN201611073960.6A CN106379544B (en) | 2016-11-29 | 2016-11-29 | The modular removable formula nacelle of unmanned plane |
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| Publication Number | Publication Date |
|---|---|
| CN106379544A CN106379544A (en) | 2017-02-08 |
| CN106379544B true CN106379544B (en) | 2018-05-25 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201611073960.6A Active CN106379544B (en) | 2016-11-29 | 2016-11-29 | The modular removable formula nacelle of unmanned plane |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| CN109515706A (en) * | 2018-12-03 | 2019-03-26 | 成都纵横大鹏无人机科技有限公司 | A kind of Modularized unmanned machine |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| US5645250A (en) * | 1993-08-26 | 1997-07-08 | Gevers; David E. | Multi-purpose aircraft |
| CN102765477B (en) * | 2012-08-10 | 2014-09-10 | 南昌航空大学 | Airplane capable of performing fixed wing flight and vertical take-off and landing based on three-axle flight control panel |
| CN106143901A (en) * | 2016-08-05 | 2016-11-23 | 北京奇正数元科技股份有限公司 | The unmanned plane wing that a kind of active force can be verted |
| CN106143898B (en) * | 2016-08-08 | 2018-07-10 | 北京奇正数元科技股份有限公司 | A kind of VTOL tilting rotor fixed wing aircraft |
| CN206202704U (en) * | 2016-11-29 | 2017-05-31 | 北京奇正数元科技股份有限公司 | The modular removable formula nacelle of unmanned plane |
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