CN105480405A - Connecting structure of remote control aircraft - Google Patents
Connecting structure of remote control aircraft Download PDFInfo
- Publication number
- CN105480405A CN105480405A CN201510863096.9A CN201510863096A CN105480405A CN 105480405 A CN105480405 A CN 105480405A CN 201510863096 A CN201510863096 A CN 201510863096A CN 105480405 A CN105480405 A CN 105480405A
- Authority
- CN
- China
- Prior art keywords
- chassis
- under
- remote control
- buckle
- motor
- 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
Links
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 239000006185 dispersion Substances 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000002688 persistence Effects 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C7/00—Structures or fairings not otherwise provided for
-
- A—HUMAN NECESSITIES
- A63—SPORTS; GAMES; AMUSEMENTS
- A63H—TOYS, e.g. TOPS, DOLLS, HOOPS OR BUILDING BLOCKS
- A63H27/00—Toy aircraft; Other flying toys
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Toys (AREA)
Abstract
The invention discloses a connecting structure of a remote control aircraft, which comprises an undercarriage, an undercarriage bolt, first buckles, a reserved hole, two fixed blocks, heat emission holes, motor covers, lower casings, positioning columns, motors, positioning sleeves, second buckles, screw hole columns and screws, wherein the undercarriage bolt is positioned in the middle of the rear part of the undercarriage; the two fixed blocks are symmetrically distributed at the front part of the undercarriage; screw holes are formed in the fixed blocks; the motor covers are arranged at the upper ends of the lower casings; the motors are installed in the motor covers; the positioning columns are fixedly connected with the lower casings; the positioning sleeves are arranged at the lower ends of the motor covers; and the screw hole columns are arranged on the lower casings. The structure is simple in assembly, convenient to disassemble and assemble, saved in cost and better in heat emission performance; by matching of the sleeve structure and the screw structure, a specific appearance requirement (long and narrow appearance) can be met, wherein the screws are longitudinally arranged and the sleeves are transversely arranged; a vertical tightening structure cannot cause shaking, thereby improving the stability; and thus, the requirements of users liking remote control aircrafts can be met.
Description
Technical field
The present invention relates to a kind of connection mode, particularly relate to a kind of remote control class aircraft connection structure.
Background technology
The aircraft controlling flight by onboard flight control system by the command and control station on ground or machine tool is remotely-piloted vehicle, along with the development of society, existing remotely-piloted vehicle is little of toy for children, large to aerocraft, along with the development of remotely-piloted vehicle, grow, the all parts of remotely-piloted vehicle is also in improvement development, present remotely-piloted vehicle under-chassis on the market, the mode of motor sleeve and motor sleeve fixing motor is varied, tradition fixing motor mode is for increasing motor sleeve over cap, cost increases, assembling also more bothers, connection mode stability and persistence not ideal enough, be difficult to the demand of satisfied present remotely-piloted vehicle user.
Summary of the invention
Object of the present invention is just to provide a kind of remote control class aircraft connection structure to solve the problem.
The present invention is achieved through the following technical solutions above-mentioned purpose: a kind of remote control class aircraft connection structure, comprise under-chassis, under-chassis latch, first buckle, preformed hole, fixed block, louvre, motor sleeve, lower casing, registration mast, 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, be symmetrically distributed on the rib of under-chassis rear portion, preformed hole for installing cushion rubber is also set 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 registration mast is fixedly connected with lower casing, 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, are respectively under-chassis inside face and under-chassis rib inside face.
Further, abutment sleeve of telling is provided with four.
Further, each described lower casing is provided with two screw hole posts, and two described screws pin under-chassis from top to bottom, lower casing, motor sleeve and upper casing.
Further, described motor sleeve upper end is provided with the second buckle, and described second buckle has certain elasticity.
The invention has the beneficial effects as follows: this Standard is simple, easy accessibility, cost-saving, heat dispersion is better, 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 can not cause rocking, improve stability, meet the demand liking now remote control class aircraft user.
Accompanying drawing explanation
Fig. 1 is under-chassis structural representation of the present invention;
Fig. 2 position motor sleeve of the present invention is arranged on the structural representation on lower casing;
Fig. 3 is motor sleeve structural representation of the present invention;
Fig. 4 is lower casing structural representation of the present invention;
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, registration mast, 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 the embodiment of the present invention, be clearly and completely described the technical scheme in the embodiment of the present invention, obviously, described embodiment is only the present invention's part embodiment, instead of whole embodiments.Based on the embodiment in the present invention, those of ordinary skill in the art, not making the every other embodiment obtained under creative work prerequisite, belong to the scope of protection of the invention.
Refer to Fig. 1 ~ 4, the invention provides a kind of technical scheme: a kind of remote control class aircraft connection structure, comprise under-chassis 1, under-chassis latch 2, first buckle 3, preformed hole 4, fixed block 5, louvre 6, motor sleeve 7, lower casing 8, registration mast 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, be symmetrically distributed on the rib of under-chassis 1 rear portion, preformed hole 4 for installing cushion rubber is also set 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 registration mast 9 is fixedly connected with lower casing 8, 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 dispelling the heat to equipment in under-chassis 1, described under-chassis latch 2, first buckle 3 and fixed block 5 all have two joint faces with under-chassis 1, be respectively under-chassis 1 inside face and under-chassis 1 rib inside face, the fixed form of under-chassis 1 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 the effect be connected and fixed, play positioning action again, make this device precisely fixing, the connection of two screws 14 can make this device balance, be conducive to the resistance to overturning of this device, abutment sleeve of telling 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.
To those skilled in the art, obviously the invention is not restricted to the details of above-mentioned one exemplary embodiment, and when not deviating from spirit of the present invention or essential characteristic, the present invention can be realized in other specific forms.Therefore, no matter from which point, all should embodiment be regarded as exemplary, and be nonrestrictive, scope of the present invention is limited by claims instead of above-mentioned explanation, and all changes be therefore intended in the implication of the equivalency by dropping on claim and scope are included in the present invention.Any Reference numeral in claim should be considered as the claim involved by limiting.
In addition, be to be understood that, although this specification sheets is described according to embodiment, but not each embodiment only comprises an independently technical scheme, this narrating mode of specification sheets is only for clarity sake, those skilled in the art should by specification sheets integrally, and the technical scheme in each embodiment also through appropriately combined, can form other embodiments that it will be appreciated by those skilled in the art that.
Claims (6)
1. a remote control class aircraft connection structure, comprises under-chassis (1), under-chassis latch (2), first buckle (3), preformed hole (4), fixed block (5), louvre (6), motor sleeve (7), lower casing (8), registration mast (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, be symmetrically distributed on the rib of under-chassis (1) rear portion, preformed hole (4) for installing cushion rubber is also set 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 registration mast (9) is fixedly connected with lower casing (8), 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 connection structure according to claim 1, is characterized in that: described under-chassis (1) is provided with louvre (6).
3. a kind of remote control class aircraft connection 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), be respectively under-chassis (1) inside face and under-chassis (1) rib inside face.
4. a kind of remote control class aircraft connection structure according to claim 1, is characterized in that: institute's abutment sleeve of telling (11) is provided with four.
5. a kind of remote control class aircraft connection 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) from top to bottom, lower casing (8), motor sleeve (7) and upper casing.
6. a kind of remote control class aircraft connection structure according to claim 1, it is characterized 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 |
|---|---|---|---|
| CN201510863096.9A CN105480405A (en) | 2015-12-01 | 2015-12-01 | Connecting structure of remote control aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510863096.9A CN105480405A (en) | 2015-12-01 | 2015-12-01 | Connecting structure of remote control aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN105480405A true CN105480405A (en) | 2016-04-13 |
Family
ID=55667761
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510863096.9A Pending CN105480405A (en) | 2015-12-01 | 2015-12-01 | Connecting structure of remote control aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN105480405A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112498672A (en) * | 2020-11-03 | 2021-03-16 | 中国直升机设计研究所 | Unmanned aerial vehicle |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| TWM247264U (en) * | 2003-11-05 | 2004-10-21 | Guo-Rung Huang | Heat-dissipation structure for propeller motor of mobile model |
| CN203135624U (en) * | 2013-03-29 | 2013-08-14 | 深圳市大疆创新科技有限公司 | Motor |
| CN204597676U (en) * | 2015-03-18 | 2015-08-26 | 深圳一电科技有限公司 | For the motor of unmanned plane, Power Component and unmanned plane |
| WO2015144036A1 (en) * | 2014-03-24 | 2015-10-01 | 杨建军 | Motor mounting structure in pan-tilt device |
| CN204776058U (en) * | 2015-07-21 | 2015-11-18 | 江西顶翔智控科技有限公司 | Remote control flight ware |
| CN205327395U (en) * | 2015-12-01 | 2016-06-22 | 深圳市哈博森智能股份有限公司 | Remote control class aircraft connection structure |
-
2015
- 2015-12-01 CN CN201510863096.9A patent/CN105480405A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| TWM247264U (en) * | 2003-11-05 | 2004-10-21 | Guo-Rung Huang | Heat-dissipation structure for propeller motor of mobile model |
| CN203135624U (en) * | 2013-03-29 | 2013-08-14 | 深圳市大疆创新科技有限公司 | Motor |
| WO2015144036A1 (en) * | 2014-03-24 | 2015-10-01 | 杨建军 | Motor mounting structure in pan-tilt device |
| CN204597676U (en) * | 2015-03-18 | 2015-08-26 | 深圳一电科技有限公司 | For the motor of unmanned plane, Power Component and unmanned plane |
| CN204776058U (en) * | 2015-07-21 | 2015-11-18 | 江西顶翔智控科技有限公司 | Remote control flight ware |
| CN205327395U (en) * | 2015-12-01 | 2016-06-22 | 深圳市哈博森智能股份有限公司 | Remote control class aircraft connection structure |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112498672A (en) * | 2020-11-03 | 2021-03-16 | 中国直升机设计研究所 | Unmanned aerial vehicle |
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| C06 | Publication | ||
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| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| TA01 | Transfer of patent application right | ||
| TA01 | Transfer of patent application right |
Effective date of registration: 20210820 Address after: 2801, building F, Xinghe world, No.1, Yabao Road, Nankeng community, Bantian street, Longgang District, Shenzhen, Guangdong 518000 Applicant after: SHENZHEN HUBSAN TECHNOLOGY Co.,Ltd. Address before: Room 201, Building A, 1 Qianwan Road, Qianhai Shenzhen-Hong Kong Cooperation Zone, Shenzhen, Guangdong Province Applicant before: SHENZHEN HUBSAN INTELLIGENT Co.,Ltd. |
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| WD01 | Invention patent application deemed withdrawn after publication | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20160413 |