CN106114843A - A kind of holding frame on rotor wing unmanned aerial vehicle motor cabinet - Google Patents
A kind of holding frame on rotor wing unmanned aerial vehicle motor cabinet Download PDFInfo
- Publication number
- CN106114843A CN106114843A CN201610472075.9A CN201610472075A CN106114843A CN 106114843 A CN106114843 A CN 106114843A CN 201610472075 A CN201610472075 A CN 201610472075A CN 106114843 A CN106114843 A CN 106114843A
- Authority
- CN
- China
- Prior art keywords
- extension
- side wall
- holding frame
- frame body
- unmanned aerial
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/12—Rotor drives
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/10—Propulsion
- B64U50/19—Propulsion using electrically powered motors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Elimination Of Static Electricity (AREA)
Abstract
The present invention relates to the holding frame on a kind of rotor wing unmanned aerial vehicle motor cabinet, including holding frame body；The upper and lower two ends of holding frame body are equipped with the tenon portion facing out projection from this holding frame body end；Holding frame body includes left side wall, right side wall；The upper end of left side wall and right side wall bends towards the direction of its opposing sidewalls respectively and extends, and forms the first extension and the second extension；The bottom of left side wall and right side wall bends towards the direction of its opposing sidewalls respectively and extends, and forms the 3rd extension and the 4th extension；The upper end of the first extension extends towards horizontal direction bending, and is crossed to form roof with the second extension；The bottom of the 3rd extension extends towards horizontal direction bending, and is crossed to form diapire with the 4th extension；Left side wall, right side wall, the first extension, the second extension, the 3rd extension, the 4th extension, roof and diapire enclose formation eight-sided formation.The invention has the beneficial effects as follows: good stability, easy to connect.
Description
Technical field
The present invention relates to unmanned plane field, particularly relate to the holding frame on a kind of rotor wing unmanned aerial vehicle motor cabinet.
Background technology
Unmanned air vehicle technique developed rapidly in recent years, and various types of unmanned planes continue to bring out, and many rotor wing unmanned aerial vehicles system has
Handling can hover by force, anywhere plays degradation advantage, can carry the monitoring devices such as all kinds of optical light sensor and photographing unit,
Tasks such as scouting, take photo by plane can be realized convenient, efficiently, be widely used in public safety, power-line patrolling, traffic monitoring,
Fire-fighting, ocean and the application such as hydrological monitoring, military surveillance.
In existing double-deck rotor wing unmanned aerial vehicle, for connecting the holding frame of two motor mounts, complicated structure, and
And poor stability, also the most inconvenient when carrying out motor mount and connecting.
Summary of the invention
The technical problem to be solved is to provide a kind of good stability, easy to connect, the holding frame of simple in construction.
The technical scheme is that the holding frame on a kind of rotor wing unmanned aerial vehicle motor cabinet,
Including holding frame body, the upper and lower two ends of holding frame body are equipped with the tenon portion facing out projection from this holding frame body end；Clamping
Frame body includes left side wall, right side wall；The upper end of left side wall and right side wall is prolonged towards the bending of the direction of its opposing sidewalls respectively
Stretch, form the first extension and the second extension；The bottom of left side wall and right side wall is respectively towards the direction of its opposing sidewalls
Bending extends, and forms the 3rd extension and the 4th extension；The upper end of the first extension extends towards horizontal direction bending, and
It is crossed to form roof with the second extension；The bottom of the 3rd extension extends towards horizontal direction bending, and extends with the 4th
Portion is crossed to form diapire；Left side wall, right side wall, the first extension, the second extension, the 3rd extension, the 4th extension, roof
And diapire encloses formation eight-sided formation, eight-sided formation is symmetrical.
The invention has the beneficial effects as follows: by being respectively provided with tenon portion at the upper and lower two ends of holding frame body, thus convenient connection pacifies
Dress seat, holding frame body uses eight-sided formation, improves stability, and present configuration is simple in addition.
On the basis of technique scheme, the present invention can also do following improvement.
Further, holding frame body is provided with four the first through holes；Four the first through holes lay respectively at the first extension,
On two extensions, the 3rd extension, the 4th extension.
Use and above-mentioned further provide the benefit that: in the case of ensureing holding frame body bulk strength, alleviate weight.
Further, holding frame body is provided with two the second through holes；Two the second through holes lay respectively at left side wall, right side wall
On.
Use and above-mentioned further provide the benefit that: this is the most internal conveniently to utilize screw that body is fixed on holding frame.
Further, the first extension, left side wall, the 3rd extension constitute X character form structure；Second extension, right side wall,
Four extensions constitute X character form structure.
Use and above-mentioned further provide the benefit that: improve stability.
Accompanying drawing explanation
Fig. 1 is the structural representation of the embodiment of the present invention；
Fig. 2 is the Fig. 1 structural representation when reality is applied；
Fig. 3 is the structural representation after Fig. 1 installs motor；
Fig. 4 is the side view of Fig. 3.
In accompanying drawing, the list of parts representated by each label is as follows:
1, holding frame body, 11, tenon portion, the 12, first through hole, the 13, second through hole, 14, screw hole, 15, screw cross groove,
16, wiring groove, 17, routing hole, 18, radiating groove, 101, left side wall, 102, right side wall, the 103, first extension, 104, second prolongs
Extending portion, the 105, the 3rd extension, the 106, the 4th extension, 107, roof, 108, diapire, 2, mounting seat, 21, slot, 3, electricity
Machine, 4, body, 5, screw.
Detailed description of the invention
Being described principle and the feature of the present invention below in conjunction with accompanying drawing, example is served only for explaining the present invention, and
Non-for limiting the scope of the present invention.
As it is shown in figure 1, the holding frame on a kind of rotor wing unmanned aerial vehicle motor cabinet, including holding frame body 1；Holding frame body 1
Two ends are equipped with and project outwardly of tenon portion 11 from this holding frame body 1 end face up and down；Holding frame body 1 includes left side wall 101, the right side
Sidewall 102；The upper end of left side wall 101 and right side wall 102 bends towards the direction of its opposing sidewalls respectively and extends, and forms first
Extension 103 and the second extension 104；The bottom of left side wall 101 and right side wall 102 is respectively towards the direction of its opposing sidewalls
Bending extends, and forms the 3rd extension 105 and the 4th extension 106；The upper end of the first extension 103 is curved towards horizontal direction
Folding extends, and is crossed to form roof 107 with the second extension 104；The bottom of the 3rd extension 105 bends towards horizontal direction
Extend, and be crossed to form diapire 108 with the 4th extension 106；Left side wall 101, right side wall the 102, first extension 103, second
Extension the 104, the 3rd extension the 105, the 4th extension 106, roof 107 and diapire 108 enclose formation eight-sided formation, and eight
Limit shape structure is symmetrical；The appearance profile of body 4 cross section is suitable with described eight-sided formation.In order to ensure total
Bearing up-down force is balance, so first extension the 103, second extension the 104, the 3rd extension the 105, the 4th extension 106
Structure identical.
As it is shown in figure 1, holding frame body 1 can also improve as follows: holding frame body 1 is provided with four the first through holes
12；Four the first through holes 12 lay respectively at first extension the 103, second extension the 104, the 3rd extension the 105, the 4th extension
On 106.In order to reduce by first its contour shape of through hole 12 of holding frame body 1 overall weight can be oval, circular or by
The enclosed construction that curve connects into.Can ensure that required for holding frame body 1 under intensity, it is not excluded that eight the first through holes are set
12 or ten two the first through holes 12.
As it is shown in figure 1, holding frame body 1 can also improve as follows: holding frame body 1 is provided with two the second through holes
13；Two the second through holes 13 lay respectively on left side wall 101, right side wall 102.In order to can ensure that body 4 is well fixed on folder
Hold in frame body 1, two second 13, three the second through holes 13 of through hole etc. can be set on left side wall 101, right side wall 102.
As it is shown in figure 1, have the motor cabinet of this holding frame, including 1, two mounting seats 2 of holding frame body；Two mounting seats
2 two ends up and down being arranged on holding frame body 1；It is connected together between mounting seat 2 and holding frame body 1；In mounting seat 2 corresponding
Be provided with the slot 21 matched with tenon portion 11, tenon portion 11 snap in correspondence slot 21 in.The cross section of tenon portion 11 and card
The cross section closing groove 21 is the most dovetail-shape or T-shaped.
As shown in Figure 2, Figure 3, Figure 4, it is equipped with, in holding frame body 1, the pipe being easy to be connected with horn by whole motor cabinet
Body 4；In two mounting seats 2, equal correspondence is provided with motor 3.The outer contour shape of the body 4 worn is octagon, so when
After body 4 is inserted in holding frame body 1, does not haves relative slip between body 4 with holding frame body 1, improve nothing
Safety during man-machine flight.
As it is shown on figure 3, mounting seat 2 is connected by four screws 5 are fixing with motor 3；Mounting seat 2 is at corresponding each screw 5
Place is equipped with a screw hole 14.If four screws 5 are when fixing connection, motor 3 occurs rolling relatively for mounting seat 2
Dynamic, screw hole 14 can be set to six, eight etc..
As it is shown in figure 1, mounting seat 2 can also be improved as follows: mounting seat 2 is equipped with one at corresponding each screw hole 14
Groove 15 crossed by individual screw.
As it is shown in figure 1, the installed surface that mounting seat 2 connects motor 3 is provided with a routing hole 17.In mounting seat 2 with electricity
The end face that machine 3 installed surface is relative is provided with wiring groove 16；Routing hole 17 is connected with wiring groove 16；Wiring groove 16 two ends are all in opening
Formula.
Additionally mounting seat 2 can be improved as follows: some louvres 18 are set in mounting seat 2, convenient to motor 3
Dispel the heat.
When mounted:
The other end of body 4 is arranged in the horn of unmanned plane.
Being arranged on holding frame body 1 of two mounting seat 2 correspondences, is arranged on motor 3 in mounting seat 2 simultaneously, and profit
Fix with screw 5.
In describing the invention, it is to be understood that term " " center ", " longitudinally ", " laterally ", " length ", " width ",
" thickness ", " on ", D score, "front", "rear", "left", "right", " vertically ", " level ", " top ", " end " " interior ", " outward ", " up time
Pin ", " counterclockwise ", " axially ", " radially ", the orientation of the instruction such as " circumferential " or position relationship be based on orientation shown in the drawings or
Position relationship, is for only for ease of the description present invention and simplifies description rather than instruction or imply that the device of indication or element must
Must have specific orientation, with specific azimuth configuration and operation, be therefore not considered as limiting the invention.
Additionally, term " first ", " second " are only used for describing purpose, and it is not intended that instruction or hint relative importance
Or the implicit quantity indicating indicated technical characteristic.Thus, define " first ", the feature of " second " can express or
Implicitly include at least one this feature.In describing the invention, " multiple " are meant that at least two, such as two, three
Individual etc., unless otherwise expressly limited specifically.
In the present invention, unless otherwise clearly defined and limited, term " install ", " being connected ", " connection ", " fixing " etc.
Term should be interpreted broadly, and connects for example, it may be fixing, it is also possible to be to removably connect, or integral；Can be that machinery connects
Connect, it is also possible to be electrical connection；Can be to be joined directly together, it is also possible to be indirectly connected to by intermediary, in can being two elements
The connection in portion or the interaction relationship of two elements, unless otherwise clear and definite restriction.For those of ordinary skill in the art
For, above-mentioned term concrete meaning in the present invention can be understood as the case may be.
In the present invention, unless otherwise clearly defined and limited, fisrt feature second feature " on " or D score permissible
It is that the first and second features directly contact, or the first and second features are by intermediary mediate contact.And, fisrt feature exists
Second feature " on ", " top " and " above " but fisrt feature directly over second feature or oblique upper, or be merely representative of
Fisrt feature level height is higher than second feature.Fisrt feature second feature " under ", " lower section " and " below " can be
One feature is immediately below second feature or obliquely downward, or is merely representative of fisrt feature level height less than second feature.
In the description of this specification, reference term " embodiment ", " some embodiments ", " example ", " specifically show
Example " or the description of " some examples " etc. means to combine this embodiment or example describes specific features, structure, material or spy
Point is contained at least one embodiment or the example of the present invention.In this manual, to the schematic representation of above-mentioned term not
Identical embodiment or example must be directed to.And, the specific features of description, structure, material or feature can be in office
One or more embodiments or example combine in an appropriate manner.Additionally, in the case of the most conflicting, the skill of this area
The feature of the different embodiments described in this specification or example and different embodiment or example can be tied by art personnel
Close and combination.
Although above it has been shown and described that embodiments of the invention, it is to be understood that above-described embodiment is example
Property, it is impossible to being interpreted as limitation of the present invention, those of ordinary skill in the art within the scope of the invention can be to above-mentioned
Embodiment is changed, revises, replaces and modification.
Claims (4)
1. the holding frame on rotor wing unmanned aerial vehicle motor cabinet, including holding frame body (1), it is characterised in that described holding frame
Body (1) two ends up and down are equipped with and project outwardly of tenon portion (11) from this holding frame body (1) end face；Described holding frame body
(1) left side wall (101), right side wall (102) are included；The upper end of described left side wall (101) and right side wall (102) is respectively towards it
The direction bending of opposing sidewalls extends, and forms the first extension (103) and the second extension (104)；Described left side wall (101) and
The bottom of right side wall (102) bends towards the direction of its opposing sidewalls respectively and extends, and forms the 3rd extension (105) and the 4th
Extension (106)；The upper end of described first extension (103) towards horizontal direction bending extend, and with the second extension
(104) roof (107) it is crossed to form；The bottom of described 3rd extension (105) extends towards horizontal direction bending, and with the
Four extensions (106) are crossed to form diapire (108)；Described left side wall (101), right side wall (102), the first extension (103),
Two extensions (104), the 3rd extension (105), the 4th extension (106), roof (107) and diapire (108) enclose formation
Eight-sided formation, described eight-sided formation is symmetrical.
Holding frame on a kind of rotor wing unmanned aerial vehicle motor cabinet the most according to claim 1, it is characterised in that described holding frame
Body (1) is provided with four the first through holes (12)；Described four the first through holes (12) lay respectively at described first extension
(103), on the second extension (104), the 3rd extension (105), the 4th extension (106).
Holding frame on a kind of rotor wing unmanned aerial vehicle motor cabinet the most according to claim 2, it is characterised in that described holding frame
Body (1) is provided with two the second through holes (13)；Said two the second through hole (13) lays respectively at described left side wall (101), the right side
On sidewall (102).
Holding frame on a kind of rotor wing unmanned aerial vehicle motor cabinet the most according to claim 1, it is characterised in that described first prolongs
Extending portion (103), left side wall (101), the 3rd extension (105) constitute X character form structure；Described second extension (104), right side wall
(102), the 4th extension (106) constitutes X character form structure.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610472075.9A CN106114843A (en) | 2016-06-23 | 2016-06-23 | A kind of holding frame on rotor wing unmanned aerial vehicle motor cabinet |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610472075.9A CN106114843A (en) | 2016-06-23 | 2016-06-23 | A kind of holding frame on rotor wing unmanned aerial vehicle motor cabinet |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106114843A true CN106114843A (en) | 2016-11-16 |
Family
ID=57269368
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610472075.9A Pending CN106114843A (en) | 2016-06-23 | 2016-06-23 | A kind of holding frame on rotor wing unmanned aerial vehicle motor cabinet |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106114843A (en) |
-
2016
- 2016-06-23 CN CN201610472075.9A patent/CN106114843A/en active Pending
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20161116 |
|
| WD01 | Invention patent application deemed withdrawn after publication |