CN208216989U - A kind of multi-rotor unmanned aerial vehicle with searchlighting function - Google Patents

A kind of multi-rotor unmanned aerial vehicle with searchlighting function Download PDF

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Publication number
CN208216989U
CN208216989U CN201820865378.1U CN201820865378U CN208216989U CN 208216989 U CN208216989 U CN 208216989U CN 201820865378 U CN201820865378 U CN 201820865378U CN 208216989 U CN208216989 U CN 208216989U
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CN
China
Prior art keywords
probe
micro
mainframe
unmanned aerial
rotation
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Expired - Fee Related
Application number
CN201820865378.1U
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Chinese (zh)
Inventor
郑文
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Binzhou University
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Binzhou University
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Application filed by Binzhou University filed Critical Binzhou University
Priority to CN201820865378.1U priority Critical patent/CN208216989U/en
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Publication of CN208216989U publication Critical patent/CN208216989U/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 multi-rotor unmanned aerial vehicles with searchlighting function, its structure includes pedestal, support rod, frame side block, power rail, high-speed motor, rotor head, blade, upper cover plate, mainframe, revolve position probe, a kind of multi-rotor unmanned aerial vehicle with searchlighting function of the utility model, first the master control system in mainframe is started, instruction is issued to be transmitted on high-speed motor by power rail, high-speed motor starting drives rotor head and blade rotation to take up unmanned plane, synchronous signal starts illumination probe by the lower electrical storage device that mainframe is oriented in the probe of rotation position, make to revolve position probe progress transverse shifting by adjusting micro-step motor, the steering for adjusting micro-machine simultaneously is modified linkage gear with the steering with moving gear, to drive illumination probe to be vertically moved, illumination is set to pop one's head in by micro-machine and micro-step motor Practice multi-directional rotation carries out searchlighting using path of the rotation position probe to night in this way, reduces failure occurrence probability.

Description

A kind of multi-rotor unmanned aerial vehicle with searchlighting function
Technical field
The utility model is a kind of multi-rotor unmanned aerial vehicle with searchlighting function, belongs to multi-rotor unmanned aerial vehicle field.
Background technique
Unmanned plane be it is current start a kind of gradually practical aircraft, with maneuverability, rapid reaction, nobody flies Row, operation require low advantage, especially multi-rotor unmanned aerial vehicle, more and more appear in daily life, work In amusement.
Prior art discloses application No. is a kind of 201720879840.9 multi-rotor unmanned aerial vehicle, including body, fly control Equipment, multiple rotor systems, the multi-rotor unmanned aerial vehicle further include for the oil-fired power generating equipment to power itself, but this is existing There is technology when detecting to path at night, when illumination is easy to appear dead angle, causes the visual field fuzzy, is easy to happen failure.
Utility model content
In view of the deficienciess of the prior art, the utility model aim be to provide a kind of more rotors with searchlighting function without Man-machine, to solve existing technology when detecting to path at night, when illumination, is easy to appear dead angle, causes the visual field fuzzy, It is easy to happen failure problems.
To achieve the goals above, the utility model is achieved through the following technical solutions: a kind of have searchlighting function Can multi-rotor unmanned aerial vehicle, structure include pedestal, support rod, frame side block, power rail, high-speed motor, rotor head, blade, on Cover board, mainframe, rotation position are popped one's head in, and are integrated on the left of the right side of the rotor head and blade, under the upper cover plate Side be connected above frame side block, be integrated above the lower section of the upper cover plate and mainframe, rotation position spy The top insertion of head is installed on the lower section of mainframe, and the rotation position probe includes terminal plate, micro-step motor, linkage board, cross Lever, illumination probe, lower electrical storage device, lower protective case, linkage gear, band moving gear, micro-machine, outer protecting shell, the terminal plate It is integrated on the left of right side and micro-step motor, the lower section insertion of the micro-step motor is installed on linkage board Top is connected on the inside of the outside of the linkage board and outer protecting shell, and the left side insertion of the traverse bar is installed on illumination probe Right side, the top of the lower electrical storage device is connected with the lower section that illumination is popped one's head in, under the top and outer protecting shell of the lower protective case Side is mutually welded, and with being connected below moving gear, the right side of the linkage gear is embedded in installation for the top of the linkage gear In the left side of illumination probe, the lower section of the micro-machine with being connected above moving gear, the left side of the micro-machine It mutually welds with the right side of outer protecting shell, is nested below the top of the lower protective case and mainframe.
Further, it is integrated below the top of the pedestal and support rod, the top of the support rod is embedding Enter to be installed on the lower section of frame side block.
Further, it is connected on the left of the right side of the frame side block and mainframe, the right side of the power rail is embedded in peace Left side loaded on upper cover plate.
Further, it is integrated on the right side of the left side of the power rail and high-speed motor, under the rotor head Side's insertion is installed on the top of high-speed motor.
Further, the rotor head is semicircular structure.
Further, the pedestal is made of aluminium alloy.
Further, the blade is made of plastics.
Beneficial effect
A kind of multi-rotor unmanned aerial vehicle with searchlighting function of the utility model first starts the master control system in mainframe, It issues instruction to be transmitted on high-speed motor by power rail, high-speed motor starting drives rotor head and blade rotation to take up nobody Machine, synchronous signal starts illumination by the lower electrical storage device that mainframe is oriented in the probe of rotation position and pops one's head in, by adjusting miniature stepping electricity Machine makes to revolve position probe progress transverse shifting, while the steering for adjusting micro-machine carries out linkage gear with the steering with moving gear Change keeps illumination probe practice more so that illumination probe be driven to be vertically moved by micro-machine and micro-step motor Orientation rotation carries out searchlighting using path of the rotation position probe to night in this way, reduces failure occurrence probability.
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 the multi-rotor unmanned aerial vehicle with searchlighting function of the utility model;
Fig. 2 is a kind of the schematic diagram of the section structure of rotation position probe of the utility model.
In figure: pedestal -1, support rod -2, frame side block -3, power rail -4, high-speed motor -5, rotor head -6, blade -7, on Cover board -8, mainframe -9, rotation position probe -10, terminal plate -1001, micro-step motor -1002, linkage board -1003, traverse bar - 1004, illumination probe -1005, lower electrical storage device -1006, lower protective case -1007, linkage gear -1008, band moving gear -1009, small-sized Motor -1010, outer protecting shell -1011.
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.
Fig. 1, Fig. 2 are please referred to, the utility model provides a kind of multi-rotor unmanned aerial vehicle technical solution with searchlighting function: its Structure includes pedestal 1, support rod 2, frame side block 3, power rail 4, high-speed motor 5, rotor head 6, blade 7, upper cover plate 8, mainframe 9, rotation position probe 10, the right side of the rotor head 6 and the left side of blade 7 are integrated, the lower section and side of the upper cover plate 8 The top of frame block 3 is connected, and the lower section of the upper cover plate 8 and the top of mainframe 9 are integrated, the rotation position probe 10 Top insertion be installed on the lower section of mainframe 9, the rotation position probe 10 including terminal plate 1001, micro-step motor 1002, Linkage board 1003, illumination probe 1005, lower electrical storage device 1006, lower protective case 1007, linkage gear 1008, drives traverse bar 1004 Gear 1009, micro-machine 1010, outer protecting shell 1011, the right side of the terminal plate 1001 and the left side of micro-step motor 1002 It is integrated, the lower section insertion of the micro-step motor 1002 is installed on the top of linkage board 1003, the linkage board 1003 outside is connected with the inside of outer protecting shell 1011, and the left side insertion of the traverse bar 1004 is installed on illumination probe 1005 Right side, the top of the lower electrical storage device 1006 is connected with the lower section of illumination probe 1005, the top of the lower protective case 1007 It is mutually welded with the lower section of outer protecting shell 1011, the top of the linkage gear 1008 is connected with the lower section with moving gear 1009, institute The right side insertion for stating linkage gear 1008 is installed on the left side of illumination probe 1005, the lower section of the micro-machine 1010 and drive The top of gear 1009 is connected, and the left side of the micro-machine 1010 is mutually welded with the right side of outer protecting shell 1011, the lower shield The top of shell 1007 and the lower section of mainframe 9 are nested, and the top of the pedestal 1 and the lower section of support rod 2 are integrated, The top insertion of the support rod 2 is installed on the lower section of frame side block 3, and the right side of the frame side block 3 is connected with the left side of mainframe 9 It connects, the right side insertion of the power rail 4 is installed on the left side of upper cover plate 8, the left side of the power rail 4 and the right side of high-speed motor 5 Side is integrated, and the lower section insertion of the rotor head 6 is installed on the top of high-speed motor 5, and the rotor head 6 is semicircle Structure, the pedestal 1 are made of aluminium alloy, and the blade 7 is made of plastics.
One component of 1 hydraulic support of pedestal described in this patent, it directly and contacts baseplate passes the support force of bracket Be delivered to bottom plate, the high-speed motor 5 is indicated with letter M in circuit, its main function be generate driving torque, as with The power source of electric appliance or various machinery, generator indicate that its main function is converted using mechanical energy with letter G in circuit For electric energy.
Carry out using when first by mainframe 9 master control system start, issue instruction by power rail 4 is transmitted to high speed On motor 5, the starting of high-speed motor 5 drives rotor head 6 and the rotation of blade 7 to take up unmanned plane, and synchronous signal is oriented to by mainframe 9 It revolves the lower electrical storage device 1006 in position probe 10 and starts illumination probe 1005, make to revolve position probe by adjusting micro-step motor 1002 10 carry out transverse shiftings, at the same steerings for adjusting micro-machine 1010 make linkage gear 1008 and the steering with moving gear 1009 into Row change is made so that illumination probe 1005 be driven to be vertically moved by micro-machine 1010 and micro-step motor 1002 The 1005 practice multi-directional rotation of illumination probe.
The utility model solves the prior art when detecting to path at night, and when illumination is easy to appear dead angle, makes The problem of obscuring at the visual field, being easy to happen failure, the utility model are combined with each other by above-mentioned component, and the utility model is a kind of Multi-rotor unmanned aerial vehicle with searchlighting function first starts the master control system in mainframe, issues instruction and is conducted by power rail Onto high-speed motor, high-speed motor starting drives rotor head and blade rotation to take up unmanned plane, and synchronous signal is led by mainframe Lower electrical storage device starting illumination probe in Xiang Xuanwei probe makes rotation position probe carry out lateral shifting by adjusting micro-step motor It is dynamic, while the steering for adjusting micro-machine is modified linkage gear with the steering with moving gear, so that illumination be driven to pop one's head in It is vertically moved, illumination probe practice multi-directional rotation is made by micro-machine and micro-step motor, utilizes rotation position in this way It pops one's head in and searchlighting is carried out to the path at night, reduce failure occurrence probability.
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 (5)

1. a kind of multi-rotor unmanned aerial vehicle with searchlighting function, it is characterised in that: its structure include pedestal (1), support rod (2), Frame side block (3), power rail (4), high-speed motor (5), rotor head (6), blade (7), upper cover plate (8), mainframe (9), rotation position are visited Head (10) is integrated on the left of the right side and blade (7) of the rotor head (6), the lower section and side of the upper cover plate (8) Frame block is connected above (3), is integrated above the lower section and mainframe (9) of the upper cover plate (8), the rotation position The top insertion of probe (10) is installed on the lower sections of mainframe (9), the rotation position pop one's head in (10) include terminal plate (1001), it is miniature Stepper motor (1002), linkage board (1003), traverse bar (1004), illumination probe (1005), lower electrical storage device (1006), lower protective case (1007), linkage gear (1008), band moving gear (1009), micro-machine (1010), outer protecting shell (1011), the terminal plate (1001) it is integrated on the left of right side and micro-step motor (1002), under the micro-step motor (1002) Side's insertion is installed on the top of linkage board (1003), and the outside of the linkage board (1003) is connected with the inside of outer protecting shell (1011) It connects, the left side insertion of the traverse bar (1004) is installed on the right side of illumination probe (1005), the lower electrical storage device (1006) It is connected below top and illumination probe (1005), the top of the lower protective case (1007) and the lower section phase of outer protecting shell (1011) Welding, the top of the linkage gear (1008) with being connected below moving gear (1009), the linkage gear (1008) Right side insertion be installed on illumination probe (1005) left side, the lower section of the micro-machine (1010) with moving gear (1009) Top be connected, the left side of the micro-machine (1010) and the right side of outer protecting shell (1011) are mutually welded, the lower protective case (1007) it is nested below top and mainframe (9).
2. a kind of multi-rotor unmanned aerial vehicle with searchlighting function according to claim 1, it is characterised in that: the pedestal (1) it is integrated below top and support rod (2), the top insertion of the support rod (2) is installed on frame side block (3) Lower section.
3. a kind of multi-rotor unmanned aerial vehicle with searchlighting function according to claim 1, it is characterised in that: the frame side block (3) it is connected on the left of right side and mainframe (9), the right side insertion of the power rail (4) is installed on a left side for upper cover plate (8) Side.
4. a kind of multi-rotor unmanned aerial vehicle with searchlighting function according to claim 1, it is characterised in that: the power rail (4) it is integrated on the right side of left side and high-speed motor (5), the lower section insertion of the rotor head (6) is installed on high speed electricity The top of machine (5).
5. a kind of multi-rotor unmanned aerial vehicle with searchlighting function according to claim 1, it is characterised in that: the rotor head It (6) is semicircular structure.
CN201820865378.1U 2018-05-30 2018-05-30 A kind of multi-rotor unmanned aerial vehicle with searchlighting function Expired - Fee Related CN208216989U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201820865378.1U CN208216989U (en) 2018-05-30 2018-05-30 A kind of multi-rotor unmanned aerial vehicle with searchlighting function

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201820865378.1U CN208216989U (en) 2018-05-30 2018-05-30 A kind of multi-rotor unmanned aerial vehicle with searchlighting function

Publications (1)

Publication Number Publication Date
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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108820234A (en) * 2018-05-30 2018-11-16 滨州学院 A kind of multi-rotor unmanned aerial vehicle with searchlighting function

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108820234A (en) * 2018-05-30 2018-11-16 滨州学院 A kind of multi-rotor unmanned aerial vehicle with searchlighting function

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CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20181211

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