CN205327395U - Remote control class aircraft connection structure - Google Patents
Remote control class aircraft connection structure Download PDFInfo
- Publication number
- CN205327395U CN205327395U CN201520978549.8U CN201520978549U CN205327395U CN 205327395 U CN205327395 U CN 205327395U CN 201520978549 U CN201520978549 U CN 201520978549U CN 205327395 U CN205327395 U CN 205327395U
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- China
- Prior art keywords
- chassis
- under
- motor
- buckle
- remote control
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- 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.)
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- 239000006185 dispersion Substances 0.000 abstract description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000002372 labelling Methods 0.000 description 1
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Abstract
The utility model discloses a remote control class aircraft connection structure, including undercarriage, undercarriage bolt, first buckle, preformed hole, fixed block, louvre, motor cover, inferior valve, reference column, motor, abutment sleeve, second buckle, screw hole post and screw, the undercarriage bolt is located undercarriage rear portion middle part, two fixed blocks are located the anterior symmetric distribution of undercarriage, be equipped with the screw hole on the fixed block, the motor cover sets up the upper end at the inferior valve, the motor is installed in the motor cover, reference column and inferior valve fixed connection, abutment sleeve sets up at motor cover lower extreme, the screw hole post sets up on the inferior valve, and the assembly of this structure is simple, and easy dismounting practices thrift the cost, and heat dispersion is better, and tube -in -tube structure and screw structure's cooperation can be satisfied the distinctive appearance and require (long and narrow appearance), and vertical -> screw, horizontal -> sleeve step up the structure from top to bottom and can not lead to rocking, have improved stable ability, satisfy the demand of liking remote control class aircraft user now.
Description
Technical field
This utility model relates to a kind of connected mode, particularly relates to a kind of remote control class aircraft attachment structure。
Background technology
The aircraft being controlled system control flight by onboard flight by the remote control station on ground or machine tool is remotely-piloted vehicle, development along with society, existing remotely-piloted vehicle is little of toy for children, big to airborne vehicle, development along with remotely-piloted vehicle, grow, the all parts of remotely-piloted vehicle is also improving development, remotely-piloted vehicle under-chassis on the market now, the mode of motor sleeve and motor sleeve fixing motor is varied, tradition fixing motor mode is for increasing motor sleeve protection lid, cost increases, assembling also more bothers, connected mode stability and persistency are not ideal enough, it is difficult to meet the demand of present remotely-piloted vehicle user。
Utility model content
The purpose of this utility model is that provides a kind of remote control class aircraft attachment structure to solve the problems referred to above。
This utility model is achieved through the following technical solutions above-mentioned purpose: a kind of remote control class aircraft attachment structure, including under-chassis, under-chassis latch, first buckle, preformed hole, fixed block, louvre, motor sleeve, lower casing, locating dowel, motor, abutment sleeve, second buckle, screw hole post and screw, described under-chassis latch is positioned at middle part, under-chassis rear portion, described first buckle is provided with two, it is symmetrically distributed on the rib of under-chassis rear portion, the preformed hole for installing cushion pad is also set up at under-chassis rear portion, it is symmetrical that described two fixed blocks are positioned at under-chassis front portion, described fixed block is provided with screw hole, described motor sleeve is arranged on the upper end of lower casing, and motor sleeve is provided with four, described motor is arranged in motor sleeve, described locating dowel is fixing with lower casing to be connected, described abutment sleeve is arranged on motor sleeve lower end, described screw hole post is arranged on lower casing。
Further, described under-chassis is provided with louvre。
Further, described under-chassis latch, the first buckle and fixed block all have two joint faces with under-chassis, respectively under-chassis inner surface and under-chassis rib inner surface。
Further, told abutment sleeve is provided with four。
Further, each described lower casing is provided with two screw hole posts, and two described screws pin under-chassis, lower casing, motor sleeve and upper casing from top to bottom。
Further, described motor sleeve upper end is provided with the second buckle, and described second buckle has certain elasticity。
The beneficial effects of the utility model are: this Standard is simple, easy accessibility, save cost, heat dispersion is more preferably, the cooperation of tube-in-tube structure and screw structural can meet distinctive appearance and require (long and narrow profile), and longitudinal direction → screw, transverse direction → sleeve add locking structure up and down and be not result in rocking, improve stability, meet the demand liking now remote control class aircraft user。
Accompanying drawing explanation
Fig. 1 is this utility model under-chassis structural representation；
Fig. 2 position this utility model motor sleeve is arranged on the structural representation on lower casing；
Fig. 3 is this utility model motor sleeve structural representation；
Fig. 4 is this utility model lower casing structural representation；
In figure: 1, under-chassis, 2, under-chassis latch, the 3, first buckle, 4, preformed hole, 5, fixed block, 6, louvre, 7, motor sleeve, 8, lower casing, 9, locating dowel, 10, motor, 11, abutment sleeve, the 12, second buckle, 13, screw hole post, 14, screw。
Detailed description of the invention
Below in conjunction with the accompanying drawing in this utility model embodiment, the technical scheme in this utility model embodiment is clearly and completely described, it is clear that described embodiment is only a part of embodiment of this utility model, rather than whole embodiments。Based on the embodiment in this utility model, the every other embodiment that those of ordinary skill in the art obtain under not making creative work premise, broadly fall into the scope of this utility model protection。
Refer to Fig. 1 ~ 4, this utility model provides a kind of technical scheme: a kind of remote control class aircraft attachment structure, including under-chassis 1, under-chassis latch 2, first buckle 3, preformed hole 4, fixed block 5, louvre 6, motor sleeve 7, lower casing 8, locating dowel 9, motor 10, abutment sleeve 11, second buckle 12, screw hole post 13 and screw 14, described under-chassis latch 2 is positioned at middle part, under-chassis 1 rear portion, described first buckle 3 is provided with two, it is symmetrically distributed on the rib of under-chassis 1 rear portion, the preformed hole 4 for installing cushion pad is also set up at under-chassis 1 rear portion, it is anterior symmetrical that described two fixed blocks 5 are positioned at under-chassis 1, described fixed block 5 is provided with screw hole 51, described motor sleeve 7 is arranged on the upper end of lower casing 8, and motor sleeve 7 is provided with four, described motor 10 is arranged in motor sleeve 7, described locating dowel 9 is fixing with lower casing 8 to be connected, described abutment sleeve 11 is arranged on motor sleeve 7 lower end, described screw hole post 13 is arranged on lower casing 8, described under-chassis 1 is provided with louvre 6, for equipment in under-chassis 1 is dispelled the heat, described under-chassis latch 2, first buckle 3 and fixed block 5 all have two joint faces with under-chassis 1, respectively under-chassis 1 inner surface and under-chassis 1 rib inner surface, the under-chassis 1 fixed form on lower casing 8 is fastened on lower casing 8 by the first buckle 3, under-chassis latch 2 is assemblied in abutment sleeve 11, additional two screws 14 are fixed, three kinds of fixed forms share, both safety was firm, Applied economy again, first buckle 3 makes connection efficient and convenient, under-chassis latch 2 had both played and had connected fixing effect, play again positioning action, make this device fixing precisely, the connection of two screws 14 can make this device balance, be conducive to the stability in the large of this device, told abutment sleeve 11 is provided with four, each described lower casing 8 is provided with two screw hole posts 13, and two described screws 14 pin under-chassis 1 from top to bottom, lower casing 8, motor sleeve 7 and upper casing, improve stability, described motor sleeve 7 upper end is provided with the second buckle 12, and described second buckle 12 has certain elasticity, motor 10 is assembled to motor sleeve 7 and assembles position, when being seated, second buckle 12 automatic rebounding, motor 10 is limited in assembling position, improve the steadiness of motor 10。
It is obvious to a person skilled in the art that this utility model is not limited to the details of above-mentioned one exemplary embodiment, and when without departing substantially from spirit of the present utility model or basic feature, it is possible to realize this utility model in other specific forms。Therefore, no matter from which point, embodiment all should be regarded as exemplary, and be nonrestrictive, scope of the present utility model is limited by claims rather than described above, it is intended that all changes in the implication of the equivalency dropping on claim and scope included in this utility model。Any accompanying drawing labelling in claim should be considered as the claim that restriction is involved。
In addition, it is to be understood that, although this specification is been described by according to embodiment, but not each embodiment only comprises an independent technical scheme, this narrating mode of description is only for clarity sake, description should be made as a whole by those skilled in the art, and the technical scheme in each embodiment through appropriately combined, can also form other embodiments that it will be appreciated by those skilled in the art that。
Claims (6)
1. a remote control class aircraft attachment structure, including under-chassis (1), under-chassis latch (2), first buckle (3), preformed hole (4), fixed block (5), louvre (6), motor sleeve (7), lower casing (8), locating dowel (9), motor (10), abutment sleeve (11), second buckle (12), screw hole post (13) and screw (14), it is characterized in that: described under-chassis latch (2) is positioned at under-chassis (1) middle part, rear portion, described first buckle (3) is provided with two, it is symmetrically distributed on the rib of under-chassis (1) rear portion, the preformed hole (4) for installing cushion pad is also set up at under-chassis (1) rear portion, it is anterior symmetrical that described two fixed blocks (5) are positioned at under-chassis (1), described fixed block (5) is provided with screw hole (51), described motor sleeve (7) is arranged on the upper end of lower casing (8), and motor sleeve (7) is provided with four, described motor (10) is arranged in motor sleeve (7), described locating dowel (9) is fixing with lower casing (8) to be connected, described abutment sleeve (11) is arranged on motor sleeve (7) lower end, and described screw hole post (13) is arranged on lower casing (8)。
2. a kind of remote control class aircraft attachment structure according to claim 1, it is characterised in that: described under-chassis (1) is provided with louvre (6)。
3. a kind of remote control class aircraft attachment structure according to claim 1, it is characterized in that: described under-chassis latch (2), the first buckle (3) and fixed block (5) all have two joint faces with under-chassis (1), respectively under-chassis (1) inner surface and under-chassis (1) rib inner surface。
4. a kind of remote control class aircraft attachment structure according to claim 1, it is characterised in that: told abutment sleeve (11) is provided with four。
5. a kind of remote control class aircraft attachment structure according to claim 1, it is characterized in that: each described lower casing (8) is provided with two screw hole posts (13), and two described screws (14) pin under-chassis (1), lower casing (8), motor sleeve (7) and upper casing from top to bottom。
6. a kind of remote control class aircraft attachment structure according to claim 1, it is characterised in that: described motor sleeve (7) upper end is provided with the second buckle (12), and described second buckle (12) has certain elasticity。
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520978549.8U CN205327395U (en) | 2015-12-01 | 2015-12-01 | Remote control class aircraft connection structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520978549.8U CN205327395U (en) | 2015-12-01 | 2015-12-01 | Remote control class aircraft connection structure |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205327395U true CN205327395U (en) | 2016-06-22 |
Family
ID=56214788
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520978549.8U Expired - Fee Related CN205327395U (en) | 2015-12-01 | 2015-12-01 | Remote control class aircraft connection structure |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205327395U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105480405A (en) * | 2015-12-01 | 2016-04-13 | 深圳市哈博森智能股份有限公司 | Connecting structure of remote control aircraft |
-
2015
- 2015-12-01 CN CN201520978549.8U patent/CN205327395U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105480405A (en) * | 2015-12-01 | 2016-04-13 | 深圳市哈博森智能股份有限公司 | Connecting structure of remote control aircraft |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20180328 Address after: 523900 Guangdong city in Dongguan Province town of Tangxia City No. A22 Yi Lu Keyuan deer Patentee after: DONGGUAN TENGSHENG INDUSTRIAL Co.,Ltd. Address before: 518054 Guangdong city of Shenzhen province Qianhai Shenzhen Hong Kong cooperation zone before Bay Road No. 1 building 201 room A (located in Shenzhen Qianhai business secretary Co. Ltd.) Patentee before: SHENZHEN HUBSAN INTELLIGENT CO.,LTD. |
|
| TR01 | Transfer of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20160622 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |