CN204646398U - A kind of miniature pesticide spray helicopter engine self power generation constituent - Google Patents

A kind of miniature pesticide spray helicopter engine self power generation constituent Download PDF

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Publication number
CN204646398U
CN204646398U CN201520307449.2U CN201520307449U CN204646398U CN 204646398 U CN204646398 U CN 204646398U CN 201520307449 U CN201520307449 U CN 201520307449U CN 204646398 U CN204646398 U CN 204646398U
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CN
China
Prior art keywords
chassis
output shaft
rotary fan
power generation
axis hole
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
CN201520307449.2U
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Chinese (zh)
Inventor
范冬宇
尹路
徐建锋
高广兴
夏唯一
李彦
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.)
Henan Dacheng General Aviation Technology Co Ltd
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Henan Dacheng General Aviation Technology Co Ltd
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Priority to CN201520307449.2U priority Critical patent/CN204646398U/en
Application granted granted Critical
Publication of CN204646398U publication Critical patent/CN204646398U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

A kind of miniature pesticide spray helicopter engine self power generation constituent, it comprises motor, described motor is provided with output shaft, described output shaft is connected with rotary fan, power facility is provided with in the middle part of described rotary fan, the outer portion of rotary fan is provided with radiation fan, described radiation fan is provided with radiator shutter, the lower surface of rotary fan is provided with chassis, described chassis is annular mechanism, the middle part on chassis is provided with transverse slat, the middle part of described transverse slat is provided with axis hole, the lower end surface of output shaft extend in described axis hole, the upper surface on chassis is provided with protection cylinder, the lower surface on chassis is provided with cooling water tank, the side of described cooling water tank is provided with water intake and water outlet, the utility model has the advantage that mechanism is simple, practical, working efficiency is high.

Description

A kind of miniature pesticide spray helicopter engine self power generation constituent
Technical field
The utility model relates to a kind of motor self power generation constituent, belongs to agricultural spraying apparatus field, is specifically related to a kind of miniature pesticide spray helicopter engine self power generation constituent.
Background technique
In the development of agricultural modernization technology, helicopter spray technique obtains increasing application, but the operating time of agricultural helicopter when spraying insecticide in field is longer, and motor works for a long time and produces a large amount of heat; In addition, motor institute's work in the process run is used for the flight of helicopter except a part and drives atomizing sprayer, also has some useful work to be wasted; How to be both conducive to the heat radiation of the hot water tank to motor, motor institute work all can be utilized again, be the focus received much concern in energy development.
Summary of the invention
The utility model is to overcome the deficiencies in the prior art, and provides the miniature pesticide spray helicopter engine self power generation constituent that a kind of mechanism is simple, practical, working efficiency is high.
The technical solution of the utility model is: a kind of miniature pesticide spray helicopter self power generation constituent, it comprises motor, described motor is provided with output shaft, described output shaft is connected with rotary fan, power facility is provided with in the middle part of described rotary fan, the outer portion of rotary fan is provided with radiation fan, described radiation fan is provided with radiator shutter, the lower surface of rotary fan is provided with chassis, described chassis is annular mechanism, the middle part on chassis is provided with transverse slat, the middle part of described transverse slat is provided with axis hole, the lower end surface of output shaft extend in described axis hole, the upper surface on chassis is provided with protection cylinder, the lower surface on chassis is provided with cooling water tank, the side of described cooling water tank is provided with water intake and water outlet.
The quantity of described radiator shutter is at least 10.
The lower surface of described rotary fan and the distance of chassis upper surface are between 4 millimeters-5 millimeters, and rotary fan freely can rotate around output shaft.
The diameter of described axis hole is a bit larger tham the diameter of output shaft, and axis hole does not run through described transverse slat.
The diameter of described protection cylinder is slightly larger than the diameter of a circle at the outward edge place of radiator shutter.
Beneficial aspects of the present utility model is: the motor that the utility model is arranged provides the power of overall operation for whole helicopter, motor running drives output shaft rotation, output shaft is connected with rotary fan, then rotary fan corresponding rotation along with output shaft does, the middle part of rotary fan is power facility, power facility is continual when output shaft constantly rotates is that electric energy is stored by rotation potential energy converting and energy, the electric energy of storage is used for as other parts of helicopter provide electric energy, the outer portion of rotary fan is radiation fan, radiation fan is provided with radiator shutter, radiator shutter dispels the heat to cooling water tank along with rotary fan rotates, the chassis of the annular mechanism that rotary fan lower surface is arranged, it is the intermediate junction device of cooling water tank and rotary fan, it is again the fixing device of rotating shaft, the middle part on chassis is provided with transverse slat, the middle part of transverse slat is provided with axis hole, the lower end of output shaft extend in axis hole, and contact with the inner wall smooth of axis hole, output shaft freely can be rotated in axis hole, during the protection cylinder that the upper surface on chassis is arranged, radiator shutter is played to the effect of protection, also prevent the rotation of radiator shutter from producing mechanical injuries to other component simultaneously, the utility model has the advantage that mechanism is simple, practical, working efficiency is high.
Accompanying drawing explanation
Fig. 1 is the plan view of a kind of miniature pesticide spray helicopter self power generation constituent of the utility model.
Fig. 2 is the partial top view of a kind of miniature pesticide spray helicopter self power generation constituent of the utility model.
Fig. 3 is blow on one's face figure in the local of a kind of miniature pesticide spray helicopter self power generation constituent of the utility model.
Fig. 4 is the partial top view of a kind of miniature pesticide spray helicopter self power generation constituent of the utility model.
In figure: 1, motor 2, output shaft 3, rotary fan 4, power facility 5, radiation fan 6, radiator shutter 7, chassis 8, transverse slat 9, axis hole 10, protection cylinder 11, cooling water tank 12, water inlet 13, water outlet.
specific embodiment
Below in conjunction with accompanying drawing, the utility model is described further.
Embodiment 1
As Fig. 1, Fig. 2, shown in Fig. 3 and Fig. 4, a kind of miniature pesticide spray helicopter self power generation constituent, it comprises motor 1, described motor 1 is provided with output shaft 2, described output shaft 2 is connected with rotary fan 3, power facility 4 is provided with in the middle part of described rotary fan 3, the outer portion of rotary fan 3 is provided with radiation fan 5, described radiation fan 5 is provided with radiator shutter 6, the lower surface of rotary fan 3 is provided with chassis 7, described chassis 7 is annular mechanism, the middle part on chassis 7 is provided with transverse slat 8, the middle part of described transverse slat 8 is provided with axis hole 9, the lower end surface of output shaft 2 extend in described axis hole 9, the upper surface on chassis 7 is provided with protection cylinder 10, the lower surface on chassis 7 is provided with cooling water tank 11, the side of described cooling water tank 11 is provided with water intake 12 and water outlet 13.
The motor that the utility model is arranged provides the power of overall operation for whole helicopter, motor running drives output shaft rotation, output shaft is connected with rotary fan, then rotary fan corresponding rotation along with output shaft does, the middle part of rotary fan is power facility, power facility is continual when output shaft constantly rotates is that electric energy is stored by rotation potential energy converting and energy, the electric energy of storage is used for as other parts of helicopter provide electric energy, the outer portion of rotary fan is radiation fan, radiation fan is provided with radiator shutter, radiator shutter dispels the heat to cooling water tank along with rotary fan rotates, the chassis of the annular mechanism that rotary fan lower surface is arranged, it is the intermediate junction device of cooling water tank and rotary fan, it is again the fixing device of rotating shaft, the middle part on chassis is provided with transverse slat, the middle part of transverse slat is provided with axis hole, the lower end of output shaft extend in axis hole, and contact with the inner wall smooth of axis hole, output shaft freely can be rotated in axis hole, during the protection cylinder that the upper surface on chassis is arranged, radiator shutter is played to the effect of protection, also prevent the rotation of radiator shutter from producing mechanical injuries to other component simultaneously, the utility model has the advantage that mechanism is simple, practical, working efficiency is high.
Embodiment 2
As Fig. 1, Fig. 2, shown in Fig. 3 and Fig. 4, a kind of miniature pesticide spray helicopter self power generation constituent, it comprises motor 1, described motor 1 is provided with output shaft 2, described output shaft 2 is connected with rotary fan 3, power facility 4 is provided with in the middle part of described rotary fan 3, the outer portion of rotary fan 3 is provided with radiation fan 5, described radiation fan 5 is provided with radiator shutter 6, the lower surface of rotary fan 3 is provided with chassis 7, described chassis 7 is annular mechanism, the middle part on chassis 7 is provided with transverse slat 8, the middle part of described transverse slat 8 is provided with axis hole 9, the lower end surface of output shaft 2 extend in described axis hole 9, the upper surface on chassis 7 is provided with protection cylinder 10, the lower surface on chassis 7 is provided with cooling water tank 11, the side of described cooling water tank 11 is provided with water intake 12 and water outlet 13.
The quantity of described radiator shutter 6 is at least 10.
The lower surface of described rotary fan 3 and the distance of chassis 7 upper surface are between 4 millimeters-5 millimeters, and rotary fan 3 freely can rotate around output shaft 2.
The diameter of described axis hole 9 is a bit larger tham the diameter of output shaft 2, and axis hole 9 does not run through described transverse slat 8.
The diameter of described protection cylinder 10 is slightly larger than the diameter of a circle at the outward edge place of radiator shutter 6.
The motor that the utility model is arranged provides the power of overall operation for whole helicopter, motor running drives output shaft rotation, output shaft is connected with rotary fan, then rotary fan corresponding rotation along with output shaft does, the middle part of rotary fan is power facility, power facility is continual when output shaft constantly rotates is that electric energy is stored by rotation potential energy converting and energy, the electric energy of storage is used for as other parts of helicopter provide electric energy, the outer portion of rotary fan is radiation fan, radiation fan is provided with radiator shutter, radiator shutter dispels the heat to cooling water tank along with rotary fan rotates, the chassis of the annular mechanism that rotary fan lower surface is arranged, it is the intermediate junction device of cooling water tank and rotary fan, it is again the fixing device of rotating shaft, the middle part on chassis is provided with transverse slat, the middle part of transverse slat is provided with axis hole, the lower end of output shaft extend in axis hole, and contact with the inner wall smooth of axis hole, output shaft freely can be rotated in axis hole, during the protection cylinder that the upper surface on chassis is arranged, radiator shutter is played to the effect of protection, also prevent the rotation of radiator shutter from producing mechanical injuries to other component simultaneously, the utility model has the advantage that mechanism is simple, practical, working efficiency is high.

Claims (5)

1. a miniature pesticide spray helicopter engine self power generation constituent, it comprises motor, it is characterized in that: described motor is provided with output shaft, described output shaft is connected with rotary fan, power facility is provided with in the middle part of described rotary fan, the outer portion of rotary fan is provided with radiation fan, described radiation fan is provided with radiator shutter, the lower surface of rotary fan is provided with chassis, described chassis is annular mechanism, the middle part on chassis is provided with transverse slat, the middle part of described transverse slat is provided with axis hole, the lower end surface of output shaft extend in described axis hole, the upper surface on chassis is provided with protection cylinder, the lower surface on chassis is provided with cooling water tank, the side of described cooling water tank is provided with water intake and water outlet.
2. one according to claim 1 miniature pesticide spray helicopter engine self power generation constituent, is characterized in that: the quantity of described radiator shutter is at least 10.
3. one according to claim 1 miniature pesticide spray helicopter engine self power generation constituent, it is characterized in that: the lower surface of described rotary fan and the distance of chassis upper surface are between 4 millimeters-5 millimeters, and rotary fan freely can rotate around output shaft.
4. one according to claim 1 miniature pesticide spray helicopter engine self power generation constituent, is characterized in that: the diameter of described axis hole is a bit larger tham the diameter of output shaft, and axis hole does not run through described transverse slat.
5. one according to claim 1 miniature pesticide spray helicopter engine self power generation constituent, is characterized in that: the diameter of described protection cylinder is slightly larger than the diameter of a circle at the outward edge place of radiator shutter.
CN201520307449.2U 2015-05-14 2015-05-14 A kind of miniature pesticide spray helicopter engine self power generation constituent Expired - Fee Related CN204646398U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201520307449.2U CN204646398U (en) 2015-05-14 2015-05-14 A kind of miniature pesticide spray helicopter engine self power generation constituent

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201520307449.2U CN204646398U (en) 2015-05-14 2015-05-14 A kind of miniature pesticide spray helicopter engine self power generation constituent

Publications (1)

Publication Number Publication Date
CN204646398U true CN204646398U (en) 2015-09-16

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107489513A (en) * 2017-09-22 2017-12-19 湖南省库塔科技有限公司 A kind of air cooling system for helicopter

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107489513A (en) * 2017-09-22 2017-12-19 湖南省库塔科技有限公司 A kind of air cooling system for helicopter
CN107489513B (en) * 2017-09-22 2024-04-16 驼网网络科技南京有限公司 Air cooling system for helicopter

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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: 20150916