CN206332289U - Many rotor quick connector mounting assemblies - Google Patents
Many rotor quick connector mounting assemblies Download PDFInfo
- Publication number
- CN206332289U CN206332289U CN201621297455.5U CN201621297455U CN206332289U CN 206332289 U CN206332289 U CN 206332289U CN 201621297455 U CN201621297455 U CN 201621297455U CN 206332289 U CN206332289 U CN 206332289U
- Authority
- CN
- China
- Prior art keywords
- female
- quick connector
- fixed block
- hole
- fuselage
- 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
- 230000000712 assembly Effects 0.000 title claims abstract description 13
- 238000000429 assembly Methods 0.000 title claims abstract description 13
- 239000003292 glue Substances 0.000 claims description 19
- 230000000694 effects Effects 0.000 description 2
- 238000003780 insertion Methods 0.000 description 2
- 230000037431 insertion Effects 0.000 description 2
- 238000009434 installation Methods 0.000 description 2
- 229920000297 Rayon Polymers 0.000 description 1
- 238000004026 adhesive bonding Methods 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000004880 explosion Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000003801 milling Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
Classifications
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E60/00—Enabling technologies; Technologies with a potential or indirect contribution to GHG emissions mitigation
- Y02E60/10—Energy storage using batteries
Landscapes
- Connection Of Batteries Or Terminals (AREA)
Abstract
A kind of many rotor quick connector mounting assemblies, include the male and female of supporting grafting, male connection power line, female connection electrical equipment with electric wire and be fixed on by the fixed block of rectangle on fuselage roof.This mounting means can effectively prevent that the situation that the wiring of power supply quick connector position loosens caused by fuselage is rocked from occurring, and greatly reinforce the stability of power supply signal.
Description
Technical field
The utility model is related to multi-rotor unmanned aerial vehicle construction applications, more particularly to many rotor quick connector mounting assemblies.
Background technology
Multi-rotor unmanned aerial vehicle belongs to a kind of small-sized unmanned vehicle, and its flying power is typically provided by battery, so
Battery can all be fixedly mounted on the fuselage of multi-rotor unmanned aerial vehicle, but be due to that battery dismounts frequently characteristic in itself, in battery
Power supply quick connector can be all provided between electrical equipment, to adapt to the frequent dismounting of battery.Power supply is inserted soon in the prior art
Joint is all freely to be arranged at fuselage interior, during unmanned plane during flying, it is easy to cause the fast grafting of power supply because fuselage is rocked
The connection of head position loosens, and from making and the power supply of unmanned plane is unstable, can so influence the normal flight of unmanned plane, even sometimes
It is likely to result in the serious consequence that unmanned plane falls in flight course.
Utility model content
The purpose of this utility model is to provide a kind of many rotor quick connector mounting assemblies, with can fix many rotors
The effect of attaching plug on unmanned plane.
Above-mentioned purpose of the present utility model technical scheme is that：
Many rotor quick connector mounting assemblies, multi-rotor unmanned aerial vehicle includes battery, connects the quick connector and machine of battery
Body top board, the quick connector includes the male and, installation group supporting and be connected the female of electrical equipment with male of connection battery
Part includes fixed block, and the fuselage roof is provided with the class square opening that can pass through female, and the fixed block, which is provided with, to be used for
Embedded female and the through hole being adapted to female size, the fuselage roof positioned at the vicinity of the class square opening are provided with fixing hole,
The fixed block is provided with the screw fixed with fixing hole, when the female is embedded in fixed block and is fixed on fuselage roof, institute
The portion bottom surface and the fuselage roof for stating female are contradicted.
By using above-mentioned technical proposal, the setting of class square opening is convenient to pass from below through female, due to electrical equipment
Fuselage interior is provided in, and the fixed block of present specification is provided in fuselage roof, so in order to ensure to use
Electric equipment is connected with female by wire while also need to be fixed on fuselage roof, is come so being merely able to put on from below, Gu
Determine to be provided with through hole on block to prevent female, the size of the fixed block is more than class square opening, when mounted in order to ensure female not
It can be fallen down below fixed seat, so be accomplished by being configured the position of fixing hole and screw, reach female insertion
Fixed block and when being fixed on fuselage roof, the portion bottom surface of female is contradicted with the fuselage roof, passes through through hole and fuselage roof
To limit the position of female.
Improve, the lateral projections formation card article of female, be provided with and card article phase in the through hole as of the present utility model
The edge of cooperation.
By using above-mentioned technical proposal, the setting of card article and edge prevents that female from deviating from from the top of through hole.
Improved as of the present utility model, distance and the edge to fixed block bottom surface of the card article to female bottom surface
Apart from equal.
By using above-mentioned technical proposal, the energy rotary fixing base when preventing having put female can be enable, make screw and solid
Determine hole alignment.
Improved as of the present utility model, excessive glue groove is provided with the through hole.
By using above-mentioned technical proposal, the setting of excessive glue groove enables to hold when fixing by viscose glue after having laid female
Certain glue of receiving is acted on, while making bonding more firm.
Improved as of the present utility model, the excessive glue groove is annular excessive glue groove.
By using above-mentioned technical proposal, excessive glue groove is set to annular excessive glue groove and facilitates groove milling and annular also with energy
Enough accommodate the effect of more glue.
Improved as of the present utility model, the fuselage roof is provided with least one mounting assembly.
By using above-mentioned technical proposal, generally require the several stand-by power supplies of setting and make provision against emergencies, so need set more
Several groups of mounting assemblies are to dock more reserve batteries.
In summary, the utility model has the advantages that：The setting of class square opening is convenient from below to wear female
Cross, because electrical equipment is provided in fuselage interior, and the fixed block of present specification is provided in fuselage roof, so
In order to ensure that electrical equipment is connected with female by wire while also need to be fixed on fuselage roof, thus be merely able to from
Lower section, which is put on, to be come, and through hole is provided with fixed block to prevent female, the size of the fixed block is more than class square opening, when mounted for
Guarantee female will not fall down below fixed seat, be so accomplished by being configured the position of fixing hole and screw, make it
When reaching female insertion fixed block and being fixed on fuselage roof, the portion bottom surface of female is contradicted with the fuselage roof, by logical
Hole and fuselage roof limit the position of female.
Brief description of the drawings
Fig. 1 is the axonometric drawing of power outlet；
Fig. 2 is the A portions enlarged drawing in Fig. 1；
Fig. 3 is the explosion figure of power outlet；
Fig. 4 is the axonometric drawing of female；
Fig. 5 is the axonometric drawing of fixed block；
Fig. 6 is the axonometric drawing of fuselage roof；
Fig. 7 is the B portions enlarged drawing in Fig. 6.
In figure, 1, fuselage roof；11st, class square opening；12nd, fixing hole；2nd, male；3rd, female；31st, female inserted terminal；32、
Female terminals；321st, female binding post；33rd, card article；4th, fixed block；41 screws；42nd, through hole；43rd, excessive glue groove；44th, block
Side.
Embodiment
The utility model is described in further detail below in conjunction with accompanying drawing.Wherein identical parts identical accompanying drawing
Mark is represented.It should be noted that the word "front", "rear" used below in description, "left", "right", "up" and "down" refer to
It is the direction in accompanying drawing 1, word " bottom surface " and " top surface ", " interior " and " outer " are referred respectively to towards or away from particular elements geometry
The direction at center.
According to shown in accompanying drawing 1-2, a kind of many rotor quick connector mounting assemblies include the male 2 and female 3 of supporting grafting
And the fixed block 4 for being fixed on female 3 on fuselage roof 1, male 2 connects the power line of external fuselage, and female 3 connects
Fuselage interior electrical equipment uses electric wire.
According to shown in accompanying drawing 2-7, the two ends of fixed block 4 be provided with two screws 41, fixed block 4 be additionally provided with it is female
The through hole 42 of first 3 matching, the center line of the hole face of through hole 42 and the line of the hole face of two screws 41 are located on the same line.
Some annular excessive glue grooves 43 are provided with the inwall of through hole 42.An edge 44 is each provided with two inwalls of through hole 42（This
Two inwalls at place are preferably two inwalls parallel to each other）, be provided with the shell of female 3 two it is corresponding with edge 44
The distance between terminals 32 of the card article 33 of protrusion, card article 33 and female 3 are identical with the depth of through hole 42.
Two circular fixation holes 12 for corresponding to screw 41 are provided with fuselage roof 1 and one matches with female 3
Class square opening 11, the circle center line connecting L and class square opening of two fixing holes 12 center line is not arranged on the same straight line, this implementation
It is preferably that the center line N of circle center line connecting L and the class square opening of two fixing holes 12 be arranged in parallel and distance away in example.
During installation, the female 3 for first finishing wiring through the class square opening 11 on fuselage roof 1, will overflow from bottom to top
Female 3, is then inserted upwardly into through hole 42 by gluing in glue groove 43 from the lower end of fixed block 4, when card article 33 is stuck in the position of edge 44
When, the glue that female terminals 32 are in same plane, and excessive glue groove 43 with the bottom of fixed block 4 can fix adhesion female 3
With fixed block 4., then fixed block 4 is fixed by being arranged in the screw of screw 41 and fixing hole 12 corresponding with screw 41
In the upper of fuselage roof 1, finally the male 1 for connecting power line is plugged in together with female 2.Now female binding post 321
Through class square opening 11 with being connected in fuselage with electric wire, and the shell of female terminals 32 can be stuck in the edge of class square opening
So as to prevent that female 3 from falling into fuselage interior from class square opening, while female and fixed block are fixed adhesion by the glue in excessive glue groove 43
Further prevent female 3 and fix situation about loosening.
After quick connector mounting assembly is installed, the quick connector between the power supply and electrical equipment of many rotors will
Be fixed on fuselage roof, thus prevent rocked because of fuselage caused by power supply quick connector position connection loosen situation hair
It is raw.
This specific embodiment is only to explain of the present utility model, and it is not to limitation of the present utility model, ability
Field technique personnel can make the modification without creative contribution to the present embodiment as needed after this specification is read, but
As long as all being protected in right of the present utility model by Patent Law.
Claims (6)
1. more than rotor quick connector mounting assembly, multi-rotor unmanned aerial vehicle include battery, connect battery quick connector and fuselage
Top board (1), the quick connector includes the male (2) of connection battery and supporting and be connected the female of electrical equipment with male (2)
(3), it is characterised in that：Mounting assembly includes fixed block (4), and the fuselage roof (1), which is provided with, can make what female (3) was passed through
Class square opening (11), the fixed block (4) is provided with for being embedded in female (3) and the through hole being adapted to female (3) size, is located at
The fuselage roof (1) of the vicinity of the class square opening (11) is provided with fixing hole (12), and the fixed block (4) is provided with fixing
The screw of hole (12) fixation, when the female (3) is embedded in fixed block (4) and is fixed on fuselage roof (1), the female (3)
Portion bottom surface and the fuselage roof (1) contradict.
2. many rotor quick connector mounting assemblies according to claim 1, it is characterised in that：The lateral projections of female (3)
Formed in card article (33), the through hole and be provided with the edge being engaged with card article (33)（44）.
3. many rotor quick connector mounting assemblies according to claim 2, it is characterised in that：The card article (33) arrives female
(3) distance of bottom surface and the edge（44）Distance to fixed block (4) bottom surface is equal.
4. many rotor quick connector mounting assemblies according to claim 1, it is characterised in that：It is provided with the through hole excessive
Glue groove（43）.
5. many rotor quick connector mounting assemblies according to claim 4, it is characterised in that：The excessive glue groove overflows for annular
Glue groove（43）.
6. many rotor quick connector mounting assemblies according to claim 1, it is characterised in that：The fuselage roof (1) sets
It is equipped with least one mounting assembly.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621297455.5U CN206332289U (en) | 2016-11-29 | 2016-11-29 | Many rotor quick connector mounting assemblies |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621297455.5U CN206332289U (en) | 2016-11-29 | 2016-11-29 | Many rotor quick connector mounting assemblies |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206332289U true CN206332289U (en) | 2017-07-14 |
Family
ID=59288911
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621297455.5U Expired - Fee Related CN206332289U (en) | 2016-11-29 | 2016-11-29 | Many rotor quick connector mounting assemblies |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206332289U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108172710A (en) * | 2017-12-20 | 2018-06-15 | 海鹰航空通用装备有限责任公司 | A kind of locking device for unmanned machine battery |
| CN110915074A (en) * | 2018-09-26 | 2020-03-24 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle and plug connector thereof |
| US11541996B2 (en) * | 2017-07-28 | 2023-01-03 | Samsung Electronics Co., Ltd. | Unmanned aerial vehicle |
-
2016
- 2016-11-29 CN CN201621297455.5U patent/CN206332289U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US11541996B2 (en) * | 2017-07-28 | 2023-01-03 | Samsung Electronics Co., Ltd. | Unmanned aerial vehicle |
| CN108172710A (en) * | 2017-12-20 | 2018-06-15 | 海鹰航空通用装备有限责任公司 | A kind of locking device for unmanned machine battery |
| CN110915074A (en) * | 2018-09-26 | 2020-03-24 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle and plug connector thereof |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20170714 Termination date: 20201129 |