CN205675251U - A kind of double-deck rotor wing unmanned aerial vehicle motor cabinet - Google Patents
A kind of double-deck rotor wing unmanned aerial vehicle motor cabinet Download PDFInfo
- Publication number
- CN205675251U CN205675251U CN201620639431.7U CN201620639431U CN205675251U CN 205675251 U CN205675251 U CN 205675251U CN 201620639431 U CN201620639431 U CN 201620639431U CN 205675251 U CN205675251 U CN 205675251U
- Authority
- CN
- China
- Prior art keywords
- extension
- holding frame
- side wall
- double
- 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.)
- Expired - Fee Related
Links
Landscapes
- Toys (AREA)
Abstract
The utility model relates to a kind of double-deck rotor wing unmanned aerial vehicle motor cabinet, including holding frame, two mounting seats of two mounting seats are arranged on the two ends up and down of holding frame；It is connected together between mounting seat and holding frame；The upper and lower two ends of holding frame are equipped with and project outwardly of tenon portion from this holding frame end face；Corresponding in mounting seat being provided with the slot matching with tenon portion, tenon portion snaps in corresponding slot；The left and right sides of holding frame is all in X character form structure.The beneficial effects of the utility model are: by being arranged at two mounting seats on holding frame, two motors are cancelled out each other under the effect of holding frame by reaction force produced by rotor when operating at the same time, and then effectively reduce the vibrations when flight for the unmanned plane, improve security during unmanned plane during flying, and the utility model simple in construction, easy accessibility.
Description
Technical field
The utility model relates to unmanned plane field, particularly relates to a kind of double-deck 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 camera,
Can convenient, realize efficiently scouting, the task such as take photo by plane, be widely used in public safety, power-line patrolling, traffic monitoring,
Fire-fighting, ocean and the application such as hydrological monitoring, military surveillance.
Existing its rotor of many rotor wing unmanned aerial vehicles is divided into two kinds when arranging: one is that individual layer is arranged, another kind is double-deck
Arranging, individual layer rotor flying speed is relatively slow, and double-deck rotor flying speed is relatively fast.But existing double-deck rotor is unmanned
The motor cabinet that machine is used can not allow positive and negative rotation rotor produced by reaction force cancel out each other, produced reaction
Power makes unmanned plane bigger vibrations occur when flight, causes security during unmanned plane during flying to reduce.
Utility model content
Technical problem to be solved in the utility model is to provide a kind of can reduce the vibrations when flight for the unmanned plane, carry
Security during high flight, the motor cabinet of easy accessibility.
The technical scheme that the utility model solves above-mentioned technical problem is as follows: a kind of double-deck rotor wing unmanned aerial vehicle motor cabinet, bag
Include holding frame, two mounting seats；Two mounting seats are arranged on the two ends up and down of holding frame；Engage between mounting seat with holding frame even
Connect；The upper and lower two ends of holding frame are equipped with and project outwardly of tenon portion from this holding frame end face；Corresponding being provided with and tenon in mounting seat
The slot that portion matches, tenon portion snaps in corresponding slot；The left and right sides of holding frame is all in X character form structure.
The beneficial effects of the utility model are: by being arranged at two mounting seats on holding frame, and two motors are together
Cancelled out each other under the effect of holding frame by reaction force produced by rotor during Shi Yunzhuan, and then effectively reduced unmanned
The vibrations when flight for the machine, improve security during unmanned plane during flying, and the utility model simple in construction, easy accessibility.
On the basis of technique scheme, the utility model can also do following improvement.
Further, the cross section of tenon portion and the cross section of slot are all dovetail-shape or T-shaped.
Use and above-mentioned further provide the benefit that: convenient be arranged on mounting seat on holding frame, and good stability.
Further, holding frame includes left side wall, right side wall；The upper end of left side wall and right side wall is respectively towards its opposite side
The direction bending of wall extends, and forms the first extension and the second extension；The bottom of left side wall and right side wall is respectively towards it
The direction bending of opposing sidewalls extends, and forms the 3rd extension and the 4th extension；The upper end of the first extension is towards level
Direction bending extends, and is crossed to form roof with the second extension；The bottom of the 3rd extension is prolonged towards horizontal direction bending
Stretch, and be crossed to form diapire with the 4th extension；Left side wall, right side wall, the first extension, the second extension, the 3rd extension,
4th extension, roof and diapire enclose formation eight-sided formation, and eight-sided formation is symmetrical；First extension, left side
Wall, the 3rd extension constitute X character form structure；Second extension, right side wall, the 4th extension constitute X character form structure.
Further, holding frame is provided with four the first through holes；Four the first through holes lay respectively at the first extension, second prolong
On extending portion, the 3rd extension, the 4th extension.
Use and above-mentioned further provide the benefit that: in the case of ensureing holding frame bulk strength, mitigate weight.
Further, holding frame is provided with two the second through holes；Two the second through holes lay respectively at left side wall, on right side wall.
Use and above-mentioned further provide the benefit that: conveniently utilize screw to be fixed on body in holding frame.
Further, mounting seat is provided with the screw hole that at least four connects motor.
Use and above-mentioned further provide the benefit that: screw is fixing more firm, improves security performance.
Further, described mounting seat is equipped with a screw at each described screw hole corresponding and crosses groove.
Use and above-mentioned further provide the benefit that: the convenient nut portion accommodating screw.
Further, the installed surface of the described motor of described mounting seat connection is provided with a routing hole.
Use and above-mentioned further provide the benefit that: be easy to lay the circuit of motor.
Further, described mounting seat is provided with wiring groove at the end face relative with motor installed surface；Described routing hole and institute
State wiring groove to be connected；Described wiring groove two ends are all in open.
Use and above-mentioned further provide the benefit that: play the effect of lead-in wire, it is simple to circuit and the horn of motor will be connected
Interior circuit is connected.
Brief description
Fig. 1 is the structural representation of the utility model embodiment；
Fig. 2 is the structural representation when reality is applied for the Fig. 1；
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:
1st, holding frame, the 11st, tenon portion, the 12nd, the first through hole, the 13rd, the second through hole, the 14th, screw hole, the 15th, groove crossed by screw, the 16th, cloth
Wire casing, the 17th, routing hole, the 18th, radiating groove, the 101st, left side wall, the 102nd, right side wall, the 103rd, the first extension, the 104th, the second extension,
105th, the 3rd extension, the 106th, the 4th extension, the 107th, roof, the 108th, diapire, the 2nd, mounting seat, the 21st, slot, the 3rd, motor, the 4th,
Body, the 5th, screw.
Detailed description of the invention
Being described principle of the present utility model and feature below in conjunction with accompanying drawing, example is served only for explaining this practicality
Novel, it is not intended to limit scope of the present utility model.
As it is shown in figure 1, a kind of double-deck rotor wing unmanned aerial vehicle motor cabinet, including holding frame the 1st, two mounting seats 2；Two mounting seats
2 two ends up and down being arranged on holding frame 1；It is connected together between mounting seat 2 and holding frame 1；Holding frame is equipped with certainly at two ends about 1
This holding frame 1 end face projects outwardly of tenon portion 11；It corresponding in mounting seat 2 is provided with the slot 21 matching with tenon portion 11,
Tenon portion 11 snaps in corresponding slot 21.The cross section of the cross section of tenon portion 11 and slot 21 is all dovetail-shape or T-shaped.
As it is shown in figure 1, holding frame 1 includes left side wall the 101st, right side wall 102；Left side wall 101 and the upper end of right side wall 102
Direction bending towards its opposing sidewalls respectively extends, and forms the first extension 103 and the second extension 104；Left side wall 101 He
The bottom of right side wall 102 extends towards the direction bending of its opposing sidewalls respectively, forms the 3rd extension 105 and the 4th and extends
Portion 106；The upper end of the first extension 103 extends towards horizontal direction bending, and is crossed to form roof with the second extension 104
107；The bottom of the 3rd extension 105 extends towards horizontal direction bending, and is crossed to form diapire with the 4th extension 106
108；Left side wall the 101st, right side wall the 102nd, the first extension the 103rd, the second extension the 104th, the 3rd extension the 105th, the 4th extension
106th, roof 107 and diapire 108 enclose formation eight-sided formation, and eight-sided formation is symmetrical；The profile of body 4 cross section
Profile is suitable with described eight-sided formation.In order to ensure that total bearing up-down force is balance, so the first extension
103rd, the structure of the second extension the 104th, the 3rd extension the 105th, the 4th extension 106 is identical.
As it is shown in figure 1, holding frame 1 can also improve as follows: holding frame 1 is provided with four the first through holes 12；Four
One through hole 12 lays respectively on the first extension the 103rd, the second extension the 104th, the 3rd extension the 105th, the 4th extension 106.For
First its contour shape of through hole 12 reducing holding frame 1 overall weight can be oval, circular or connected into by curve
Enclosed construction.Under can ensure that intensity required for holding frame 1, it is not excluded that eight the first through holes 12 or the ten two the first through holes are set
12。
As it is shown in figure 1, holding frame 1 can also improve as follows: holding frame 1 is provided with two the second through holes 13；Two
Two through holes 13 lay respectively on left side wall the 101st, right side wall 102.In order to can ensure that body 4 is well fixed in holding frame 1, can
To arrange two the second through holes the 13rd, three the second through holes 13 etc. on left side wall the 101st, right side wall 102.
As shown in Figure 2, Figure 3, Figure 4, it is equipped with the body 4 that being easy to, whole motor cabinet is connected with horn in holding frame 1；
It all corresponding in two mounting seats 2 is provided with motor 3.The outer contour shape of the body 4 wearing is octagon, so works as body
After 4 are inserted in holding frame 1, between body 4 with holding frame 1, do not have relative slip, when improve unmanned plane during flying
Security.
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 each screw 5 corresponding
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 each screw hole 14 corresponding
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 relative end face of machine 3 installed surface 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.
Two mounting seats 2 are corresponding to be arranged on holding frame 1, is arranged on motor 3 in mounting seat 2 simultaneously, and utilizes spiral shell
Nail 5 is fixed.
Double-deck rotor wing unmanned aerial vehicle motor cabinet described in the utility model, by being arranged at holding frame 1 by two mounting seats 2
On, two motors 3 are cancelled out each other under the effect of holding frame 1 by reaction force produced by rotor when operating at the same time, enter
And effectively reduce the vibrations when flight for the unmanned plane, improve security during unmanned plane during flying, and the utility model
Simple in construction, easy accessibility.
In of the present utility model description, it is to be understood that term " " center ", " longitudinally ", " laterally ", " length ", " width
Degree ", " thickness ", " on ", D score, "front", "rear", "left", "right", " vertically ", " level ", " top ", " end " " interior ", " outward ", " suitable
The orientation of the instruction such as hour hands ", " counterclockwise ", " axially ", " radially ", " circumferential " or position relationship are for based on orientation shown in the drawings
Or position relationship, be for only for ease of description the utility model and simplify describe, rather than instruction or hint indication device or
Element must have specific orientation, with specific azimuth configuration and operation, therefore it is not intended that to limit of the present utility model
System.
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 of the present utility model description, " multiple " are meant that at least two, such as two
Individual, three etc., unless otherwise expressly limited specifically.
In the utility model, unless otherwise clearly defined and limited, term " install ", " being connected ", " connection ", " Gu
Fixed " etc. term should be interpreted broadly, connect for example, it may be fixing, it is also possible to be to removably connect, or integral；Can be
It is mechanically connected, 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, can be two
The connection of element internal or the interaction relationship of two elements, limit unless otherwise clear and definite.Common skill for this area
For art personnel, concrete meaning in the utility model for the above-mentioned term can be understood as the case may be.
In the utility model, unless otherwise clearly defined and limited, fisrt feature second feature " on " or D score
Can be that the first and second features directly contact, or the first and second features pass through intermediary mediate contact.And, first is special
Levy second feature " on ", " top " and " above " but fisrt feature directly over second feature or oblique upper, or only
Represent that fisrt feature level height is higher than second feature.Fisrt feature second feature " under ", " lower section " and " below " permissible
Be fisrt feature immediately below second feature or obliquely downward, or be merely representative of fisrt feature level height and be less than second feature.
In the description of this specification, reference term " embodiment ", " some embodiments ", " example ", " specifically show
Specific features, structure, material or the spy that the description of example " or " some examples " etc. means to combine this embodiment or example describes
Point is contained at least one embodiment of the present utility model or example.In this manual, the schematic table to above-mentioned term
State and be necessarily directed to identical embodiment or example.And, the specific features of description, structure, material or feature are permissible
One or more embodiment in office or example combine in an appropriate manner.Additionally, in the case of not conflicting, this area
Technical staff the feature of the different embodiment described in this specification or example and different embodiment or example can be entered
Row combines and combination.
Although above it has been shown and described that embodiment of the present utility model, it is to be understood that above-described embodiment is
Exemplary, it is impossible to it is interpreted as that those of ordinary skill in the art is in scope of the present utility model to restriction of the present utility model
In above-described embodiment can be changed, change, replace and modification.
Claims (9)
1. a double-deck rotor wing unmanned aerial vehicle motor cabinet, it is characterised in that include holding frame (1), two mounting seats (2)；Described two
Individual mounting seat (2) is arranged on the two ends up and down of described holding frame (1)；Engage between described mounting seat (2) with described holding frame (1)
Connect；The upper and lower two ends of described holding frame (1) are equipped with and project outwardly of tenon portion (11) from this holding frame (1) end face；Described installation
Seat (2) is upper corresponding is provided with the slot (21) matching with described tenon portion (11), and described tenon portion (11) snaps in corresponding institute
State in slot (21)；The left and right sides of described holding frame (1) is all in X character form structure.
2. a kind of double-deck rotor wing unmanned aerial vehicle motor cabinet according to claim 1, it is characterised in that the horizontal stroke of described tenon portion (11)
The cross section of cross section and described slot (21) is all dovetail-shape or T-shaped.
3. a kind of double-deck rotor wing unmanned aerial vehicle motor cabinet according to claim 1, it is characterised in that described holding frame (1) wraps
Include left side wall (101), right side wall (102)；Described left side wall (101) is relative towards it respectively with the upper end of right side wall (102)
The direction bending of sidewall extends, and forms the first extension (103) and the second extension (104)；Described left side wall (101) and right side
The bottom of wall (102) extends towards the direction bending of its opposing sidewalls respectively, forms the 3rd extension (105) and the 4th and extends
Portion (106)；The upper end of described first extension (103) towards horizontal direction bending extend, and with the second extension (104) phase
Hand over and form roof (107)；The bottom of described 3rd extension (105) extends towards horizontal direction bending, and extends with the 4th
Portion (106) is crossed to form diapire (108)；Described left side wall (101), right side wall (102), the first extension (103), the second extension
Portion (104), the 3rd extension (105), the 4th extension (106), roof (107) and diapire (108) enclose formation octagon
Structure, described eight-sided formation is symmetrical；Described first extension (103), left side wall (101), the 3rd extension (105) structure
Become X character form structure；Described second extension (104), right side wall (102), the 4th extension (106) constitute X character form structure.
4. a kind of double-deck rotor wing unmanned aerial vehicle motor cabinet according to claim 3, it is characterised in that on described holding frame (1)
It is provided with four the first through holes (12)；Described four the first through holes (12) lay respectively at described first extension (103), the second extension
Portion (104), the 3rd extension (105), on the 4th extension (106).
5. a kind of double-deck rotor wing unmanned aerial vehicle motor cabinet according to claim 3, it is characterised in that on described holding frame (1)
It is provided with two the second through holes (13)；Said two the second through hole (13) lays respectively at described left side wall (101), right side wall (102)
On.
6. a kind of double-deck rotor wing unmanned aerial vehicle motor cabinet according to claim 1, it is characterised in that in described mounting seat (2)
It is provided with at least four and connect the screw hole (14) of motor (3).
7. a kind of double-deck rotor wing unmanned aerial vehicle motor cabinet according to claim 6, it is characterised in that described mounting seat (2) exists
Each described screw hole (14) place corresponding is equipped with a screw and crosses groove (15).
8. a kind of double-deck rotor wing unmanned aerial vehicle motor cabinet according to any one of claim 1 to 6, it is characterised in that described peace
The installed surface that dress seat (2) connects motor (3) is provided with a routing hole (17).
9. a kind of double-deck rotor wing unmanned aerial vehicle motor cabinet according to claim 8, it is characterised in that in described mounting seat (2)
It is provided with wiring groove (16) at the end face relative with motor (3) installed surface；Described routing hole (17) is connected with described wiring groove (16)
Logical；Described wiring groove (16) two ends are all in open.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620639431.7U CN205675251U (en) | 2016-06-23 | 2016-06-23 | A kind of double-deck rotor wing unmanned aerial vehicle motor cabinet |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620639431.7U CN205675251U (en) | 2016-06-23 | 2016-06-23 | A kind of double-deck rotor wing unmanned aerial vehicle motor cabinet |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205675251U true CN205675251U (en) | 2016-11-09 |
Family
ID=57429218
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620639431.7U Expired - Fee Related CN205675251U (en) | 2016-06-23 | 2016-06-23 | A kind of double-deck rotor wing unmanned aerial vehicle motor cabinet |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205675251U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107933920A (en) * | 2017-10-19 | 2018-04-20 | 深圳市莲花百川科技有限公司 | A kind of agricultural plant protection unmanned plane |
-
2016
- 2016-06-23 CN CN201620639431.7U patent/CN205675251U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107933920A (en) * | 2017-10-19 | 2018-04-20 | 深圳市莲花百川科技有限公司 | A kind of agricultural plant protection unmanned plane |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN205554623U (en) | Optical zoom nacelle | |
| CN206411593U (en) | A kind of high-availability computer heat abstractor | |
| EP3654404B1 (en) | Battery pack | |
| CN105977424A (en) | Battery pack fixing frame for electric automobile | |
| CN205675251U (en) | A kind of double-deck rotor wing unmanned aerial vehicle motor cabinet | |
| CN105882953A (en) | Aircraft | |
| CN205574258U (en) | Unmanned aerial vehicle | |
| CN106043713A (en) | Double-layer rotor unmanned aerial vehicle motor seat | |
| CN106218884A (en) | The portable multi-rotor aerocraft of Spliced type | |
| CN206125442U (en) | Unmanned aerial vehicle motor mount pad and unmanned aerial vehicle | |
| CN208963325U (en) | A kind of unmanned plane | |
| CN208181415U (en) | Multi-rotor unmanned aerial vehicle fuselage box | |
| CN207274991U (en) | A kind of unmanned aerial vehicle onboard lighting device and unmanned plane | |
| CN205675215U (en) | A kind of fast-spliced aircraft | |
| CN104843191A (en) | Non-contact type intelligent rainproof device for unmanned aerial vehicle | |
| CN205675252U (en) | For connecting the connecting tube of motor cabinet on a kind of unmanned plane | |
| CN205376602U (en) | Unmanned aerial vehicle's external battery securing device | |
| CN206265281U (en) | A kind of integral type unmanned plane frame | |
| CN209719917U (en) | Aircraft duct and culvert type aircraft | |
| CN207381459U (en) | A kind of battery modules side plate | |
| CN106114843A (en) | A kind of holding frame on rotor wing unmanned aerial vehicle motor cabinet | |
| CN205838262U (en) | A kind of sightseeing elevator | |
| CN215498535U (en) | Motor structure and rotor unmanned aerial vehicle | |
| CN207006490U (en) | Weigh style grid and ceiling machine | |
| CN206466170U (en) | Multi-stage cascade formula self-balancing is tethered at UAS |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20161109 Termination date: 20190623 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |