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CN208285150U - A kind of propeller motor rapid heat radiation device - Google Patents

A kind of propeller motor rapid heat radiation device Download PDF

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Publication number
CN208285150U
CN208285150U CN201820940011.1U CN201820940011U CN208285150U CN 208285150 U CN208285150 U CN 208285150U CN 201820940011 U CN201820940011 U CN 201820940011U CN 208285150 U CN208285150 U CN 208285150U
Authority
CN
China
Prior art keywords
shell
handle box
box
diversion pipe
cooling fin
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
Application number
CN201820940011.1U
Other languages
Chinese (zh)
Inventor
马相鸣
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Tianjin Jingtian Aviation Technology Co Ltd
Original Assignee
Tianjin Jingtian Aviation Technology Co Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Tianjin Jingtian Aviation Technology Co Ltd filed Critical Tianjin Jingtian Aviation Technology Co Ltd
Priority to CN201820940011.1U priority Critical patent/CN208285150U/en
Application granted granted Critical
Publication of CN208285150U publication Critical patent/CN208285150U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

The utility model provides a kind of propeller motor rapid heat radiation device, including radiator fan, relay box, diversion pipe one, handle box one, cooling fin one, cooling fin two, handle box two and diversion pipe two, radiator fan is embedded in the mounting hole in the middle part of shell left side, relay box installs left side medium position inside the shell, diversion pipe one and the setting symmetrical above and below of diversion pipe two are in relay box annular side, one right end of diversion pipe is connected with handle box one, handle box one is fixed on shell annular side surface upper part, cooling fin one is fixed on one lower end surface of spring, cooling fin two is fixed on two upper end of spring, handle box two is fixed on shell annular side lower, two right end of diversion pipe is connected with handle box two, the design achieves the rapid convectives of air in shell, improve radiating efficiency, the utility model cross-ventilation effect is good, Good heat dissipation effect, use scope is wide, high reliablity.

Description

A kind of propeller motor rapid heat radiation device
Technical field
The utility model is a kind of propeller motor rapid heat radiation device, belongs to motor radiating apparatus field.
Background technique
Propeller motor radiator in the prior art can not be applicable in the use with different size motor, use limitation Property it is big, and heat dissipation effect is bad, and convection effects are poor, so being badly in need of that a kind of propeller motor is wanted to be solved with rapid heat radiation device State the problem.
Utility model content
It is filled in view of the deficienciess of the prior art, the utility model aim is to provide a kind of propeller motor with rapid cooling It sets, to solve the problems mentioned in the above background technology, the utility model cross-ventilation effect is good, and good heat dissipation effect uses model Enclose wide, high reliablity.
To achieve the goals above, the utility model is achieved through the following technical solutions: a kind of propeller motor With rapid heat radiation device, including shell and cooling mechanism, the cooling mechanism is arranged in annular side inside the shell, described to dissipate Heat engine structure include radiator fan, relay box, diversion pipe one, handle box one, spring one, cooling fin one, cooling fin two, spring two, Handle box two and diversion pipe two, the radiator fan are embedded in the mounting hole in the middle part of shell left side, the relay box peace Cased left side medium position, the diversion pipe one is with the setting symmetrical above and below of diversion pipe two in relay box annular side On, one right end of diversion pipe is connected with handle box one, and the handle box one is fixed on shell annular side surface upper part, described Spring one is mounted on one downside of handle box, and the cooling fin one is fixed on one lower end surface of spring, and the cooling fin two is solid It is scheduled on two upper end of spring, the spring two is mounted on two upper side of handle box, and the handle box two is fixed on shell annular Side lower, two right end of diversion pipe are connected with handle box two.
Further, it is connected on the left of the relay box with mounting hole, left side is equipped with strainer in the mounting hole.
Further, control switch is installed, the control switch is distinguished by connecting line in the shell annular side It is connected with cooling fan and external power supply.
Further, air inlet, the air inlet are offered on one lower end surface of handle box and two upper surface of handle box Grid is mounted in mouthful.
Further, three groups of convex blocks are installed on the relay box right side, convex block described in three groups is equidistantly arranged in transfer On box right side, and three groups of convex block specifications are identical.
Further, one cross section of cooling fin and two cross section of cooling fin are arc-shaped.
The utility model has the beneficial effects that a kind of propeller motor rapid heat radiation device of the utility model, because of this reality Radiator fan, relay box, diversion pipe one, handle box one, spring one, cooling fin one, cooling fin two, spring are added to novel Two, handle box two and diversion pipe two, the design achieves the rapid convectives of air in shell, improve radiating efficiency, simultaneously Suitable for the use of different size motor, solving original propeller motor radiator can not be applicable in and different size motor Use, it is big using limitation, and heat dissipation effect is bad, the problem of convection effects difference.
Because the utility model is added to strainer, which avoids the case where external sundries blocks mounting hole generation, Yin Ben Utility model is added to control switch, which runs radiator fan convenient for operating personnel, because the utility model is added to air inlet Mouthful, which is convenient for the quick flowing of air-flow, and the utility model cross-ventilation effect is good, and good heat dissipation effect, use scope is wide, can By property height.
Detailed description of the invention
Upon reading the detailed description of non-limiting embodiments with reference to the following drawings, other spies of the utility model Sign, objects and advantages will become more apparent upon:
Fig. 1 is a kind of structural schematic diagram of propeller motor rapid heat radiation device of the utility model;
Fig. 2 is the structural schematic diagram of cooling mechanism in a kind of propeller motor rapid heat radiation device of the utility model;
In figure: 1- cooling mechanism, 2- shell, 101- radiator fan, 102- relay box, 103- diversion pipe one, 104- processing Box one, 105- spring one, 106- cooling fin one, 107- cooling fin two, 108- spring two, 109- handle box two, 110- diversion pipe Two.
Specific embodiment
To be easy to understand the technical means, creative features, achievement of purpose, and effectiveness of the utility model, below In conjunction with specific embodiment, the utility model is further described.
Please refer to Fig. 1 and Fig. 2, the utility model provides a kind of technical solution: a kind of propeller motor is filled with rapid cooling It sets, including shell 2 and cooling mechanism 1, cooling mechanism 1 is arranged on 2 annular side of shell, and cooling mechanism 1 includes heat dissipation Fan 101, relay box 102, diversion pipe 1, handle box 1, spring 1, cooling fin 1, cooling fin 2 107, Spring 2 108, handle box 2 109 and diversion pipe 2 110, radiator fan 101 are embedded in the mounting hole in the middle part of 2 left side of shell Interior, relay box 102 is mounted on left side medium position in shell 2, diversion pipe 1 and the setting symmetrical above and below of diversion pipe 2 110 In 102 annular side of relay box, one 103 right end of diversion pipe is connected with handle box 1, and handle box 1 is fixed on outer 2 annular side surface upper part of shell, spring 1 are mounted on one 104 downside of handle box, and cooling fin 1 is fixed on spring one On 105 lower end surfaces, cooling fin 2 107 is fixed on 2 108 upper end of spring, and spring 2 108 is mounted on 2 109 upper side of handle box On, handle box 2 109 is fixed on 2 annular side lower of shell, and 2 110 right end of diversion pipe is connected with handle box 2 109, should Design realizes the rapid convective of air in shell 2, improves radiating efficiency, while being suitable for the use of different size motor.
The left side of relay box 102 is connected with mounting hole, in mounting hole on the left of strainer is installed, can cross barrier external impurities into Enter in mounting hole, ensure that the duration of convection current, control switch is installed in 2 annular side of shell, control switch passes through connection Line is connected with cooling fan and external power supply respectively, radiator fan 101 is run convenient for operating personnel, under handle box 1 Air inlet is offered on end face and 2 109 upper surface of handle box, is mounted on grid in air inlet, convenient for gas in shell 2 Stream rapidly enters in handle box 1 and handle box 2 109, and three groups of convex blocks are equipped on 102 right side of relay box, and three groups convex Block is equidistantly arranged on 102 right side of relay box, and three groups of convex block specifications are identical, can make to stay between motor and relay box 102 There is gap, avoid the case where motor left side heat is concentrated, one 106 cross section of cooling fin and cooling fin 2 107 are transversal Face be it is arc-shaped, improve the contact area of cooling fin 1 and cooling fin 2 107 and motor, improve heat dissipation effect.
Specific embodiment: it in progress in use, operating personnel checks the utility model first, checks whether and deposits In defect, it can not just carry out using if there is defect, need that maintenance personal is notified to repair at this time, if do not deposited It is can be carried out if problem using shell 2 is sleeved in outer surface of motor by operating personnel, and then motor squeezes dissipate simultaneously Backing 1 and cooling fin 2 107, cooling fin 1 squeeze spring 1, and cooling fin 2 107 squeezes spring 2 108, and Under 2 108 rebound effect of spring 1 and spring, paste cooling fin 1 and cooling fin 2 107 closely with motor It closes, and then shell 2 is fixed on outer surface of motor, motor when in use, generates heat, cooling fin 1 and cooling fin two 107 quickly absorb motor heat, and operating personnel runs radiator fan 101 by control switch, and radiator fan 101 generates negative pressure, And then the hot-air in shell 2, on cooling fin 1 and cooling fin 2 107 is delivered to handle box by air inlet respectively One 104 in handle box 2 109, and the hot-air in handle box 1 enters relay box 102, handle box by diversion pipe 1 Hot-air in 2 109 enters relay box 102 by diversion pipe 2 110, and radiator fan 101 is by the hot-air in relay box 102 Shell 2 is discharged by mounting hole to improve radiating efficiency to realize the rapid convective of air in shell 2, be suitable for simultaneously The use of different size motor.
The basic principles and main features of the present invention and the advantages of the present invention have been shown and described above, for For those skilled in the art, it is clear that the present invention is not limited to the details of the above exemplary embodiments, and without departing substantially from this In the case where the spirit or essential attributes of utility model, the utility model can be realized in other specific forms.Therefore, no matter From the point of view of which point, the present embodiments are to be considered as illustrative and not restrictive, and the scope of the utility model is by institute Attached claim rather than above description limit, it is intended that will fall within the meaning and scope of the equivalent elements of the claims All changes are embraced therein.It should not treat any reference in the claims as limiting related right It is required that.
In addition, it should be understood that although this specification is described in terms of embodiments, but not each embodiment is only wrapped Containing an independent technical solution, this description of the specification is merely for the sake of clarity, and those skilled in the art should It considers the specification as a whole, the technical solutions in the various embodiments may also be suitably combined, forms those skilled in the art The other embodiments being understood that.

Claims (6)

1. a kind of propeller motor rapid heat radiation device, including shell (2) and cooling mechanism (1), it is characterised in that: described Cooling mechanism (1) is arranged on shell (2) annular side, and the cooling mechanism (1) includes radiator fan (101), relay box (102), diversion pipe one (103), handle box one (104), spring one (105), cooling fin one (106), cooling fin two (107), bullet Spring two (108), handle box two (109) and diversion pipe two (110), the radiator fan (101) are embedded in shell (2) left side In the mounting hole at middle part, the relay box (102) is mounted on the interior left side medium position of shell (2), the diversion pipe one (103) With diversion pipe two (110) setting symmetrical above and below in relay box (102) annular side, diversion pipe one (103) right end and place Reason box one (104) is connected, and the handle box one (104) is fixed on shell (2) annular side surface upper part, the spring one (105) it being mounted on handle box one (104) downside, the cooling fin one (106) is fixed on spring one (105) lower end surface, The cooling fin two (107) is fixed on spring two (108) upper end, and the spring two (108) is mounted on the upside of handle box two (109) On face, the handle box two (109) is fixed on shell (2) annular side lower, diversion pipe two (110) right end and processing Box two (109) is connected.
2. a kind of propeller motor rapid heat radiation device according to claim 1, it is characterised in that: the relay box (102) left side is connected with mounting hole, and left side is equipped with strainer in the mounting hole.
3. a kind of propeller motor rapid heat radiation device according to claim 1, it is characterised in that: the shell (2) Control switch is installed, the control switch is connected with cooling fan and external power supply respectively by connecting line in annular side It connects.
4. a kind of propeller motor rapid heat radiation device according to claim 1, it is characterised in that: the handle box one (104) air inlet is offered on lower end surface and handle box two (109) upper surface, is mounted on grid in the air inlet.
5. a kind of propeller motor rapid heat radiation device according to claim 1, it is characterised in that: the relay box (102) three groups of convex blocks are installed, convex block described in three groups is equidistantly arranged on relay box (102) right side, and three groups on right side Convex block specification is identical.
6. a kind of propeller motor rapid heat radiation device according to claim 1, it is characterised in that: the cooling fin one (106) cross section and cooling fin two (107) cross section are arc-shaped.
CN201820940011.1U 2018-06-19 2018-06-19 A kind of propeller motor rapid heat radiation device Expired - Fee Related CN208285150U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201820940011.1U CN208285150U (en) 2018-06-19 2018-06-19 A kind of propeller motor rapid heat radiation device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201820940011.1U CN208285150U (en) 2018-06-19 2018-06-19 A kind of propeller motor rapid heat radiation device

Publications (1)

Publication Number Publication Date
CN208285150U true CN208285150U (en) 2018-12-25

Family

ID=64704662

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201820940011.1U Expired - Fee Related CN208285150U (en) 2018-06-19 2018-06-19 A kind of propeller motor rapid heat radiation device

Country Status (1)

Country Link
CN (1) CN208285150U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112217341A (en) * 2020-09-28 2021-01-12 张晓卫 Motor cooling assembly with temperature detection device

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112217341A (en) * 2020-09-28 2021-01-12 张晓卫 Motor cooling assembly with temperature detection device
CN112217341B (en) * 2020-09-28 2021-10-12 肇东市华州石油机械设备有限公司 Motor cooling assembly with temperature detection device

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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: 20181225