CN208470101U - A kind of rechargeable unmanned plane - Google Patents

A kind of rechargeable unmanned plane Download PDF

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Publication number
CN208470101U
CN208470101U CN201821061086.9U CN201821061086U CN208470101U CN 208470101 U CN208470101 U CN 208470101U CN 201821061086 U CN201821061086 U CN 201821061086U CN 208470101 U CN208470101 U CN 208470101U
Authority
CN
China
Prior art keywords
wing
unmanned plane
host box
support frame
outside
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
CN201821061086.9U
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Chinese (zh)
Inventor
彭向明
郭宇红
陶伯欣
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.)
Changchun Zhongxiang Robot Technology Co Ltd
Original Assignee
Changchun Zhongxiang Robot 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 Changchun Zhongxiang Robot Technology Co Ltd filed Critical Changchun Zhongxiang Robot Technology Co Ltd
Priority to CN201821061086.9U priority Critical patent/CN208470101U/en
Application granted granted Critical
Publication of CN208470101U publication Critical patent/CN208470101U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

The utility model discloses a kind of rechargeable unmanned planes, including host box and fixed link, the inside of the host box is equipped with radiating aluminium sheet, and battery is provided on the inside of radiating aluminium sheet, heat release hole is provided with below the battery, and support frame is installed on the outside of heat release hole, charge port is provided on the inside of support frame as described above, the protection cystosepiment is mounted at the outer ledge of host box, and the inside of cystosepiment is protected to run through organic frame, the fixed link is mounted on the rack, and motor is installed in fixed link, wing is connected on the outside of the motor, and Air Filter is installed on the outside of wing, anticollision bumper ring is provided on the outside of the Air Filter, camera is installed below the host box.The rechargeable unmanned plane is mounted with Air Filter and anticollision bumper ring, is conducive to play the role of wing dirt anticollision, effectively obstructs the solid particulate matter of air and dust, convenient for users to safeguarding to wing.

Description

A kind of rechargeable unmanned plane
Technical field
The utility model relates to unmanned plane correlative technology field, specially a kind of rechargeable unmanned plane.
Background technique
The application of further investigation with enterprise to unmanned plane with the development of science and technology, unmanned plane is more and more wider, wide It is general for photographing, agricultural, the fields such as military affairs, some people to go in for photography, if it is desired to when shooting high-altitude scene, no longer step on Height, or found a view using large scale equipment, they can use unmanned plane to shoot, but existing unmanned plane there is also Certain defect does not carry out good safeguard procedures to the wing of unmanned plane, causes wing spoilage big, difficult in maintenance, So that the consumer cost of user is got higher.
In view of the above-mentioned problems, carrying out innovative design on the basis of original rechargeable unmanned plane.
Summary of the invention
The purpose of this utility model is to provide a kind of rechargeable unmanned planes, mentioned above in the background art existing to solve Some unmanned planes do not carry out good safeguard procedures to wing, cause wing spoilage big, difficult in maintenance, so that user The problem of consumer cost is got higher.
To achieve the above object, the utility model provides the following technical solutions: a kind of rechargeable unmanned plane, including host box And fixed link, the inside of the host box is equipped with radiating aluminium sheet, and battery is provided on the inside of radiating aluminium sheet, the electric power storage It is provided with heat release hole below pond, and support frame is installed on the outside of heat release hole, charge port is provided on the inside of support frame as described above, The protection cystosepiment is mounted at the outer ledge of host box, and the inside of cystosepiment is protected to run through organic frame, the fixation Bar is mounted on the rack, and motor is equipped in fixed link, and wing, and the outside installation of wing are connected on the outside of the motor There is Air Filter, anticollision bumper ring is provided on the outside of the Air Filter, camera, the machine are installed below the host box Frame is internally provided with alloy-layer.
Preferably, the heat release hole runs through the bottom of host box, and heat release hole is distributed in the underface of battery in a ring Position.
Preferably, support frame as described above includes wear-resistant coating and damping rubber pad, and wear-resistant coating is uniformly wrapped in support frame Outer surface, and the rounded convex structure of damping rubber pad, while damping rubber pad is isodistantly spaced the bottom for being distributed in support frame.
Preferably, the inside of the rack is double-layer hollow structure, and alloy-layer is embedded in the outer hollow of rack, and And the material of alloy-layer is titanium magnesium alloy material.
Preferably, the Air Filter is provided with 3 groups, and 3 groups of Air Filters are respectively about wing in symmetrical up and down.
Preferably, the anticollision bumper ring is an integral structure with Air Filter, and the diameter length of anticollision bumper ring is greater than The movable diameter of wing.
Compared with prior art, the utility model has the beneficial effects that the rechargeable unmanned plane,
(1) device is mounted with Air Filter and anticollision bumper ring, is conducive to play the role of wing dirt anticollision, the dress It sets in high-altitude flight, is easy for the dust in air to be attached on wing, so that the operating of wing is influenced, and Air Filter can have Effect obstructs the solid particulate matter of air and dust, convenient for users to safeguarding to wing;
(2) it is mounted with protection cystosepiment, protecting the longitudinal section of cystosepiment and Air Filter is shuttle shape structure, reduces flight In air drag, reduce influence of the wind to the device, while protective treatment can be carried out to the device, improve the device Practicability;
(3) wear-resistant coating and damping rubber pad are mounted with, support frame and ground face contact can generate friction, and wear-resistant coating is great The scratch resistance of support frame is improved, the aesthetics for keeping device entirety is facilitated, damping rubber pad reduces the device and connects with ground The impact force generated when touching, plays the role of damping, buffering.
Detailed description of the invention
Fig. 1 is the utility model overlooking structure diagram;
Fig. 2 is the utility model positive structure schematic;
Fig. 3 is the utility model host box bottom substance schematic diagram;
Fig. 4 is the utility model support frame structure diagram;
Fig. 5 is the utility model accumulator structure schematic diagram;
Fig. 6 is the utility model alloy schematic diagram of a layer structure.
In figure: 1, host box;2, radiating aluminium sheet;3, battery;4, heat release hole;5, support frame;501, wear-resistant coating;502, Damping rubber pad;6, charge port;7, cystosepiment is protected;8, rack;9, fixed link;10, motor;11, wing;12, Air Filter;13, Anticollision bumper ring;14, camera;15, alloy-layer.
Specific embodiment
The following will be combined with the drawings in the embodiments of the present invention, carries out the technical scheme in the embodiment of the utility model Clearly and completely describe, it is clear that the described embodiments are only a part of the embodiments of the utility model, rather than whole Embodiment.Based on the embodiments of the present invention, those of ordinary skill in the art are without making creative work Every other embodiment obtained, fall within the protection scope of the utility model.
Fig. 1-6 is please referred to, the utility model provides a kind of technical solution: a kind of rechargeable unmanned plane, including host box 1, Radiating aluminium sheet 2, battery 3, heat release hole 4, support frame 5, wear-resistant coating 501, damping rubber pad 502, charge port 6, protection cystosepiment 7, rack 8, fixed link 9, motor 10, wing 11, Air Filter 12, anticollision bumper ring 13, camera 14 and alloy-layer 15, host box 1 inside is equipped with radiating aluminium sheet 2, and the inside of radiating aluminium sheet 2 is provided with battery 3, and the lower section of battery 3 is provided with heat dissipation Hole 4, and the outside of heat release hole 4 is equipped with support frame 5, the inside of support frame 5 is provided with charge port 6, and protection cystosepiment 7 is mounted on At the outer ledge of host box 1, and the inside of cystosepiment 7 is protected to run through organic frame 8, fixed link 9 is mounted in rack 8, and solid Motor 10 is installed, the outside of motor 10 is connected with wing 11, and the outside of wing 11 is equipped with Air Filter 12, prevents in fixed pole 9 The outside of dirt net 12 is provided with anticollision bumper ring 13, and the lower section of host box 1 is equipped with camera 14, and rack 8 is internally provided with Alloy-layer 15.
Heat release hole 4 runs through the bottom of host box 1, and heat release hole 4 is distributed in the following position directly of battery 3 in a ring, side Just to the circuit power and precision equipment progress radiating and cooling inside host box 1, extend the service life of interior arrangement.
Support frame 5 includes wear-resistant coating 501 and damping rubber pad 502, and wear-resistant coating 501 is uniformly wrapped in support frame 5 Outer surface, and the rounded convex structure of damping rubber pad 502, while damping rubber pad 502 is isodistantly spaced and is distributed in support frame 5 Bottom, enhance the rub proofness of support frame 5, prevent because abrasion and destroy aesthetics, meanwhile, damping rubber pad 502 is to this Device declines when being contacted with ground, can play the role of damping.
The inside of rack 8 is double-layer hollow structure, and alloy-layer 15 is embedded in the outer hollow of rack 8, and alloy The material of layer 15 is titanium magnesium alloy material, facilitates installation circuit facility, and titanium magnesium alloy light weight, hardness is strong, convenient not increase In the case that the device crosses weight, the intensity of lift carriage 8 prevents rack 8 from fractureing.
Air Filter 12 is provided with 3 groups, and 3 groups of Air Filters 12 are respectively about wing 11 in symmetrical up and down, convenience pair Wing 11 carries out proofing dust and protecting, and dust is avoided to enter the junction of motor 10 Yu wing 11, to influence the rotation of wing 11.
Anticollision bumper ring 13 is an integral structure with Air Filter 12, and the diameter length of anticollision bumper ring 13 is greater than wing 11 Movable diameter, play the role of cushion bumper to wing 11, when the device being avoided accidentally to topple over, wing 11 can be destroyed, made At the loss of user.
Working principle: the equipment such as unmanned plane camera, and internal wireless facilities, sensor belong to known technology, no This case novel point is constituted, is not described in detail in the present case, when using the rechargeable unmanned plane, user first checks for this Whether each part of device is intact, in the case where each part does not damage, reuses the device, and according to Fig.5, user will Charger injects in charge port 6, is charged with this to the battery 3 inside host box 1, and battery 3 is having power supply storage In the case of, according to Fig. 1-Fig. 2, to other power-supply devices, 50KTYZ type motor 10 and the camera 14 inside host box 1 into Heat is discharged from heat release hole 4 for row power supply, the radiating aluminium sheet 2 inside host box 1, thereby protects internal power circuit Facility can 50KTYZ type electricity by the remote control control device, in fixed link 9 when user is taken photo by plane using the device Machine 10 starts, so that 11 high speed rotation of wing is driven, so that the device empties height, 12 He of Air Filter required for user Anticollision bumper ring 13 plays the role of dust-proof anticollision to wing 11, and according to Fig.6, the alloy-layer 15 inside rack 8 improves The intensity of rack 8 prevents from fractureing, and protects the streamlined structure of cystosepiment 7 and Air Filter 12, is effectively reduced the resistance of wind, Facilitate the flight of the device, the image photographed by the wireless facilities inside host box 1, is transferred to computer terminal by camera 14 On, when the device falls, according to Fig. 3-Fig. 4, the damping rubber pad 502 of 5 bottom of support frame can be carried out the work of bumper and absorbing shock With the wear-resistant coating 501 outside support frame 5 enhances its scratch resistance, and the content being not described in detail in this specification belongs to this The prior art well known to skilled artisan.
While there has been shown and described that the embodiments of the present invention, for the ordinary skill in the art, It is understood that these embodiments can be carried out with a variety of variations in the case where not departing from the principles of the present invention and spirit, repaired Change, replacement and variant, the scope of the utility model is defined by the appended claims and the equivalents thereof.

Claims (6)

1. a kind of rechargeable unmanned plane, including host box (1) and fixed link (9), it is characterised in that: the host box (1) it is interior Portion is equipped with radiating aluminium sheet (2), and battery (3) are provided on the inside of radiating aluminium sheet (2), is set below the battery (3) It is equipped with heat release hole (4), and support frame (5) is installed on the outside of heat release hole (4), support frame as described above is provided with charging on the inside of (5) Mouth (6), protection cystosepiment (7) are mounted at the outer ledge of host box (1), and protect the inside of cystosepiment (7) through organic Frame (8), the fixed link (9) is mounted on rack (8), and motor (10) are equipped in fixed link (9), the motor (10) Outside is connected with wing (11), and Air Filter (12) are equipped on the outside of wing (11), the outside setting of the Air Filter (12) Have anticollision bumper ring (13), camera (14) is installed below the host box (1), rack (8) are internally provided with Alloy-layer (15).
2. a kind of rechargeable unmanned plane according to claim 1, it is characterised in that: the heat release hole (4) runs through host box (1) bottom, and heat release hole (4) is distributed in the following position directly of battery (3) in a ring.
3. a kind of rechargeable unmanned plane according to claim 1, it is characterised in that: support frame as described above (5) includes wear-resisting painting Layer (501) and damping rubber pad (502), and wear-resistant coating (501) is uniformly wrapped in the outer surface of support frame (5), and damping The rounded convex structure of rubber mat (502), while damping rubber pad (502) is isodistantly spaced the bottom for being distributed in support frame (5).
4. a kind of rechargeable unmanned plane according to claim 1, it is characterised in that: the inside of the rack (8) is bilayer Hollow structure, and alloy-layer (15) are embedded in the outer hollow of rack (8), and the material of alloy-layer (15) is titanium magnesium alloy Material.
5. a kind of rechargeable unmanned plane according to claim 1, it is characterised in that: the Air Filter (12) is provided with 3 groups, And 3 groups of Air Filters (12) are respectively about wing (11) in symmetrical up and down.
6. a kind of rechargeable unmanned plane according to claim 1, it is characterised in that: the anticollision bumper ring (13) with it is dust-proof Net (12) is an integral structure, and the diameter length of anticollision bumper ring (13) is greater than the movable diameter of wing (11).
CN201821061086.9U 2018-07-05 2018-07-05 A kind of rechargeable unmanned plane Expired - Fee Related CN208470101U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201821061086.9U CN208470101U (en) 2018-07-05 2018-07-05 A kind of rechargeable unmanned plane

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201821061086.9U CN208470101U (en) 2018-07-05 2018-07-05 A kind of rechargeable unmanned plane

Publications (1)

Publication Number Publication Date
CN208470101U true CN208470101U (en) 2019-02-05

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Family Applications (1)

Application Number Title Priority Date Filing Date
CN201821061086.9U Expired - Fee Related CN208470101U (en) 2018-07-05 2018-07-05 A kind of rechargeable unmanned plane

Country Status (1)

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CN (1) CN208470101U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113682463A (en) * 2021-09-16 2021-11-23 郑州轻工业大学 Protection system for improving safety of physical layer of unmanned aerial vehicle

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113682463A (en) * 2021-09-16 2021-11-23 郑州轻工业大学 Protection system for improving safety of physical layer of unmanned aerial vehicle
CN113682463B (en) * 2021-09-16 2024-03-12 郑州轻工业大学 Protection system for improving physical layer safety of unmanned aerial vehicle

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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: 20190205

Termination date: 20210705