CN106275459A - A kind of easy assembling type motor of many rotors - Google Patents
A kind of easy assembling type motor of many rotors Download PDFInfo
- Publication number
- CN106275459A CN106275459A CN201610779830.8A CN201610779830A CN106275459A CN 106275459 A CN106275459 A CN 106275459A CN 201610779830 A CN201610779830 A CN 201610779830A CN 106275459 A CN106275459 A CN 106275459A
- Authority
- CN
- China
- Prior art keywords
- transverse arm
- motor
- hole
- assembling type
- easy assembling
- 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
- 230000002787 reinforcement Effects 0.000 claims abstract description 12
- 239000000741 silica gel Substances 0.000 claims description 7
- 229910002027 silica gel Inorganic materials 0.000 claims description 7
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 claims description 6
- 210000003205 muscle Anatomy 0.000 claims description 2
- 230000005855 radiation Effects 0.000 claims 1
- 239000007787 solid Substances 0.000 claims 1
- 230000008901 benefit Effects 0.000 abstract description 5
- 239000006185 dispersion Substances 0.000 abstract description 3
- 208000031481 Pathologic Constriction Diseases 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 230000001141 propulsive effect Effects 0.000 description 1
- 210000001215 vagina Anatomy 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/24—Aircraft characterised by the type or position of power plants using steam or spring force
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/40—Arrangements for mounting power plants in aircraft
-
- 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
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02K—DYNAMO-ELECTRIC MACHINES
- H02K5/00—Casings; Enclosures; Supports
- H02K5/04—Casings or enclosures characterised by the shape, form or construction thereof
- H02K5/20—Casings or enclosures characterised by the shape, form or construction thereof with channels or ducts for flow of cooling medium
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Power Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
The invention discloses the easy assembling type motor of a kind of many rotors, described bolt hole totally two, transverse arm is tightly fastened with motor, described bridge cavity is provided with reinforcement, the direction of described reinforcement is consistent with the direction of bolt hole, improve the mechanical strength of transverse arm, transverse arm is avoided to rupture, hole, described location is provided with abrasion-proof rubber cushion, make transverse arm and motor closely coupled, described motor body is provided with louvre, improve its heat dispersion, extend its service life, the easy assembling type motor of these many rotors has assembling, it is convenient to change, reduce loss, cost-effective advantage, there is wide market prospect.
Description
Technical field
The present invention relates to mechanical field, particularly to the easy assembling type motor of a kind of many rotors.
Background technology
Many rotor wing unmanned aerial vehicles, are a kind of special pilotless helicopters with three and above rotor shaft.It passes through
Motor rotation on each axle, drives rotor, thus produces a liter thrust.Rotor always away from fixing, and unlike helicopter
The most variable.By changing the relative rotation speed between different rotor, thus it is possible to vary the size of single shaft propulsive force, thus control flight
The running orbit of device, need to be clipped in two transverse arm two sides, by the spiral shell of locating piece with locating piece during the assembling of existing many rotors motor
Stricture of vagina screwed lock motor base, motor lines need to pass in the middle of two transverse arms, and lock motor can cause transverse arm to break when exerting oneself excessive
Split, deform.During replacing, inconvenience, need to remove one whole transverse arm.
Summary of the invention
The technical problem to be solved is to provide the easy assembling type motor of a kind of many rotors to solve in prior art
The above-mentioned multinomial defect caused.
For achieving the above object, the present invention provides following technical scheme: the easy assembling type motor of a kind of many rotors includes electricity
Owner's body, transverse arm and silica gel line, the side of affiliated motor body is provided with hole, location, and described motor body is provided with bolt hole, institute
Stating transverse arm and be provided with the bolt hole of correspondence, described transverse arm is cylindric, and hole, described location is in the same size with the cross section of transverse arm, institute
State transverse arm to be positioned in hole, location, and be screwed, in described transverse arm, be provided with bridge cavity, described silica gel line and motor body phase
Connect, and through bridge cavity.
Preferably, described bolt hole totally two.
Preferably, described bridge cavity is provided with reinforcement.
Preferably, the direction of described reinforcement and the direction of bolt hole are consistent.
Preferably, hole, described location is provided with abrasion-proof rubber cushion.
Preferably, described motor body is provided with louvre.
Above technical scheme is used to provide the benefit that: to the invention discloses the easy assembling type motor of a kind of many rotors, described
Bolt hole totally two, is tightly fastened transverse arm with motor, is provided with reinforcement, the direction of described reinforcement and spiral shell in described bridge cavity
The direction of keyhole is consistent, improves the mechanical strength of transverse arm, it is to avoid transverse arm ruptures, and hole, described location is provided with abrasion-proof rubber cushion, makes
Transverse arm and motor are closely coupled, and described motor body is provided with louvre, improve its heat dispersion, extend its service life, should
The easy assembling type motor of many rotors has assembling, and it is convenient to change, and reduces loss, and cost-effective advantage, before having wide market
Scape.
Accompanying drawing explanation
Fig. 1 is the structural representation of the present invention；
Fig. 2 is the structural representation of transverse arm；
Fig. 3 is the structural representation in transverse arm cross section；
Fig. 4 is the structural representation in motor body cross section.
Wherein, 1-motor body, 2-transverse arm, 3-silica gel line, 4-position hole, 5-bolt hole, 6-screw, 7-bridge cavity, 8-
Louvre, 9-reinforcement, 10-abrasion-proof rubber cushion.
Detailed description of the invention
Describe the preferred embodiment of the present invention below in conjunction with the accompanying drawings in detail.
Fig. 1 shows the detailed description of the invention of the present invention: the easy assembling type motor of a kind of many rotors includes motor body 1, transverse arm 2
With silica gel line 3, the side of affiliated motor body 1 is provided with hole 4, location, and described motor body 1 is provided with bolt hole 5, described transverse arm 2
Being provided with the bolt hole 5 of correspondence, described transverse arm 2 is cylindric, and hole, described location 4 is in the same size with the cross section of transverse arm 2, described
Transverse arm 2 is positioned in hole 4, location, and is fixed by screw 6, is provided with bridge cavity 7, described silica gel line 3 and motor master in described transverse arm 2
Body is connected, and through bridge cavity 7, described motor body 1 is provided with louvre 8.
In addition Fig. 2, shown in 3 and 4, described bolt hole 5 totally two, described bridge cavity 7 is provided with reinforcement 9, described reinforcement
The direction of muscle 9 is consistent with the direction of bolt hole 5, and hole, described location 4 is provided with abrasion-proof rubber cushion 10.
Above technical scheme is used to provide the benefit that: to the invention discloses the easy assembling type motor of a kind of many rotors, described
Bolt hole totally two, is tightly fastened transverse arm with motor, is provided with reinforcement, the direction of described reinforcement and spiral shell in described bridge cavity
The direction of keyhole is consistent, improves the mechanical strength of transverse arm, it is to avoid transverse arm ruptures, and hole, described location is provided with abrasion-proof rubber cushion, makes
Transverse arm and motor are closely coupled, and described motor body is provided with louvre, improve its heat dispersion, extend its service life, should
The easy assembling type motor of many rotors has assembling, and it is convenient to change, and reduces loss, and cost-effective advantage, before having wide market
Scape.
Above-described is only the preferred embodiment of the present invention, it is noted that for those of ordinary skill in the art
For, without departing from the concept of the premise of the invention, it is also possible to make some deformation and improvement, these broadly fall into the present invention
Protection domain.
Claims (6)
1. the easy assembling type motor of rotor more than a kind, it is characterised in that include motor body, transverse arm and silica gel line, affiliated motor master
The side of body is provided with hole, location, and described motor body is provided with bolt hole, and described transverse arm is provided with the bolt hole of correspondence, described horizontal stroke
Arm is cylindric, and hole, described location is in the same size with the cross section of transverse arm, and described transverse arm is positioned in hole, location, and solid by screw
Fixed, it is provided with bridge cavity in described transverse arm, described silica gel line is connected with motor body, and through bridge cavity.
The easy assembling type motor of many rotors the most according to claim 1, it is characterised in that described bolt hole totally two.
The easy assembling type motor of many rotors the most according to claim 1, it is characterised in that be provided with reinforcement in described bridge cavity
Muscle.
The easy assembling type motor of many rotors the most according to claim 3, it is characterised in that the direction of described reinforcement and bolt
The direction in hole is consistent.
The easy assembling type motor of many rotors the most according to claim 1, it is characterised in that hole, described location is provided with wear-resisting rubber
Rubber cushion.
The easy assembling type motor of many rotors the most according to claim 1, it is characterised in that described motor body is provided with heat radiation
Hole.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610779830.8A CN106275459A (en) | 2016-08-31 | 2016-08-31 | A kind of easy assembling type motor of many rotors |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610779830.8A CN106275459A (en) | 2016-08-31 | 2016-08-31 | A kind of easy assembling type motor of many rotors |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106275459A true CN106275459A (en) | 2017-01-04 |
Family
ID=57672527
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610779830.8A Pending CN106275459A (en) | 2016-08-31 | 2016-08-31 | A kind of easy assembling type motor of many rotors |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106275459A (en) |
Citations (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2193484Y (en) * | 1994-05-31 | 1995-03-29 | 杭州铝材厂 | Aluminium alloy pipe with inside reinforcing rib |
| CN2697392Y (en) * | 2004-04-30 | 2005-05-04 | 付建立 | Hydraulic clean water valve of water isolation pump |
| CN101776007A (en) * | 2010-01-26 | 2010-07-14 | 镇江东方康驰电机制造有限公司 | Heat dissipation structure of box-type diesel generator set |
| CN202040255U (en) * | 2010-09-21 | 2011-11-16 | 李中立 | Novel automobile shock absorber |
| CN102635900A (en) * | 2012-05-18 | 2012-08-15 | 珠海格力电器股份有限公司 | Indoor unit of air conditioner |
| CN102684354A (en) * | 2012-04-26 | 2012-09-19 | 锦州汉拿电机有限公司 | Vehicle generator brush end cover and manufacture method thereof |
| CN203127141U (en) * | 2012-12-13 | 2013-08-14 | 深圳市大疆创新科技有限公司 | Multi-rotor wing unmanned aerial vehicle |
| CN204871614U (en) * | 2015-07-09 | 2015-12-16 | 深圳市尚腾影科技有限公司 | Battery embeds multiaxis aircraft |
| CN105173068A (en) * | 2015-07-31 | 2015-12-23 | 广州极飞电子科技有限公司 | Unmanned plane |
| CN204937518U (en) * | 2015-05-14 | 2016-01-06 | 苏州绿农航空植保科技有限公司 | A kind of multi-rotor aerocraft motor base |
| US20160101850A1 (en) * | 2014-10-13 | 2016-04-14 | Che Min LIN | Multi-rotor frame structure |
| CN105857588A (en) * | 2016-04-13 | 2016-08-17 | 辽宁壮龙无人机科技有限公司 | Four-rotor plant protection unmanned aerial vehicle adopting helicopter armor plate structure |
| CN206374990U (en) * | 2016-10-31 | 2017-08-04 | 浙江天马行空创新科技有限公司 | A kind of new unmanned plane motor cabinet |
-
2016
- 2016-08-31 CN CN201610779830.8A patent/CN106275459A/en active Pending
Patent Citations (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2193484Y (en) * | 1994-05-31 | 1995-03-29 | 杭州铝材厂 | Aluminium alloy pipe with inside reinforcing rib |
| CN2697392Y (en) * | 2004-04-30 | 2005-05-04 | 付建立 | Hydraulic clean water valve of water isolation pump |
| CN101776007A (en) * | 2010-01-26 | 2010-07-14 | 镇江东方康驰电机制造有限公司 | Heat dissipation structure of box-type diesel generator set |
| CN202040255U (en) * | 2010-09-21 | 2011-11-16 | 李中立 | Novel automobile shock absorber |
| CN102684354A (en) * | 2012-04-26 | 2012-09-19 | 锦州汉拿电机有限公司 | Vehicle generator brush end cover and manufacture method thereof |
| CN102635900A (en) * | 2012-05-18 | 2012-08-15 | 珠海格力电器股份有限公司 | Indoor unit of air conditioner |
| CN203127141U (en) * | 2012-12-13 | 2013-08-14 | 深圳市大疆创新科技有限公司 | Multi-rotor wing unmanned aerial vehicle |
| US20160101850A1 (en) * | 2014-10-13 | 2016-04-14 | Che Min LIN | Multi-rotor frame structure |
| CN204937518U (en) * | 2015-05-14 | 2016-01-06 | 苏州绿农航空植保科技有限公司 | A kind of multi-rotor aerocraft motor base |
| CN204871614U (en) * | 2015-07-09 | 2015-12-16 | 深圳市尚腾影科技有限公司 | Battery embeds multiaxis aircraft |
| CN105173068A (en) * | 2015-07-31 | 2015-12-23 | 广州极飞电子科技有限公司 | Unmanned plane |
| CN105857588A (en) * | 2016-04-13 | 2016-08-17 | 辽宁壮龙无人机科技有限公司 | Four-rotor plant protection unmanned aerial vehicle adopting helicopter armor plate structure |
| CN206374990U (en) * | 2016-10-31 | 2017-08-04 | 浙江天马行空创新科技有限公司 | A kind of new unmanned plane motor cabinet |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20170104 |
|
| RJ01 | Rejection of invention patent application after publication |