CN106081087A - A kind of Portable unmanned machine - Google Patents

A kind of Portable unmanned machine Download PDF

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Publication number
CN106081087A
CN106081087A CN201610625688.1A CN201610625688A CN106081087A CN 106081087 A CN106081087 A CN 106081087A CN 201610625688 A CN201610625688 A CN 201610625688A CN 106081087 A CN106081087 A CN 106081087A
Authority
CN
China
Prior art keywords
rotary shaft
main body
unmanned plane
connecting rod
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.)
Pending
Application number
CN201610625688.1A
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Chinese (zh)
Inventor
刘友波
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.)
Chengdu Hengsheng Technology Co Ltd
Original Assignee
Chengdu Hengsheng 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 Chengdu Hengsheng Technology Co Ltd filed Critical Chengdu Hengsheng Technology Co Ltd
Priority to CN201610625688.1A priority Critical patent/CN106081087A/en
Publication of CN106081087A publication Critical patent/CN106081087A/en
Pending legal-status Critical Current

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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/04Helicopters
    • B64C27/08Helicopters with two or more rotors
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C1/00Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/061Frames
    • B64C1/063Folding or collapsing to reduce overall dimensions, e.g. foldable tail booms
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C1/00Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/30Parts of fuselage relatively movable to reduce overall dimensions of aircraft
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U10/00Type of UAV
    • B64U10/10Rotorcrafts

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Remote Sensing (AREA)
  • Toys (AREA)

Abstract

The invention discloses a kind of Portable unmanned machine, including unmanned plane main body, the inner chamber of described unmanned plane main body is provided with center and is installed with I shape fixed block, the left and right sides of described I shape fixed block is all installed with expansion link, the outside of described expansion link is installed with contiguous block, the outside of described contiguous block is installed with connecting rod, and the outer wall of described connecting rod is provided with main rotary shaft, and the outer wall of described main rotary shaft is provided with main screw.This Portable unmanned machine, when not in use, by promoting contiguous block that expansion link can be made to regain in the I shape fixed block in unmanned plane body lumen, thus contiguous block blocks the both sides of unmanned plane main body, and connecting rod drives main rotary shaft and main screw to be retracted to the both sides of unmanned plane main body, by loosening fixing bolt, rotary shaft can be made to rotate in lower rotary shaft, thus revolute pair connecting rod, it is easier to storage, more convenient carry.

Description

A kind of Portable unmanned machine
Technical field
The present invention relates to unmanned air vehicle technique field, be specially a kind of Portable unmanned machine.
Background technology
Along with developing rapidly of unmanned plane industry, unmanned plane will enter the daily life of ordinary consumer as camera In living, working, entertain, and conventional four rotor wing unmanned aerial vehicles are all fixed horns, and small product size is relatively big, takes up space, particularly Thin and sharp blade allows most people fear especially when high speed operation, and product does not has affinity, therefore, in order to make unmanned plane More affinity, its product, it is also contemplated that fashion takes design factor and the speciality of level product, is allowed to a kind of more affinity Image is presented in face of everybody, and in addition to profile fashion is attractive in appearance, powerful and compact unmanned plane more can meet people The needs of daily life, the such as patent of Patent No. 201620029845.8, put down including four bracing frames, Multi-functional suspension Platform and foot rest, rotor system, rotor system includes driver, propeller and connecting rod, and one end of connecting rod is provided with drives Dynamic device, the other end of connecting rod is hinged with bracing frame, although connecting rod can be folded and pack up, but profile is single, unsightly, The attention of consumer can not be caused.
Summary of the invention
It is an object of the invention to provide a kind of Portable unmanned machine, with the problem solving to propose in above-mentioned background technology.
For achieving the above object, the present invention provides following technical scheme: a kind of Portable unmanned machine, including unmanned owner Body, the inner chamber of described unmanned plane main body is provided with center and is installed with I shape fixed block, described I shape fixed block The left and right sides is all installed with expansion link, and the outside of described expansion link is installed with contiguous block, the outside of described contiguous block Being installed with connecting rod, the outer wall of described connecting rod is provided with main rotary shaft, and the outer wall of described main rotary shaft is provided with main spiral shell Rotation oar, the corner of described unmanned plane main body is all installed with secondary propeller main body, and described secondary propeller main body includes secondary fixing Plate, the outside of described secondary fixed plate is provided with lower rotary shaft, and the top of described lower rotary shaft is provided with rotary shaft, described upper rotary shaft Being connected with lower rotary shaft by fixing bolt, the outside of described upper rotary shaft is provided with secondary connecting rod, the outside of described secondary connecting rod Being provided with secondary rotary shaft, the outer wall of described secondary rotary shaft is provided with secondary rotation oar.
Preferably, the corner, bottom of described unmanned plane main body is equipped with base, and described base includes urceolus, described urceolus Inner side is provided with inner core, and the circumference of described inner core is provided with groove, and the inner side of described groove is provided with roating sphere.
Preferably, the bottom of described urceolus is provided with sucker.
Preferably, described I shape fixed block is provided with reinforcing plate with the junction of expansion link.
Preferably, the left and right sides of described unmanned plane main body is equipped with protecting film.
Preferably, the bottom of described unmanned plane main body is provided with handle, and the outer wall of described handle is provided with rubber sleeve.
Compared with prior art, the invention has the beneficial effects as follows: this Portable unmanned machine, when not in use, by promoting Contiguous block can make expansion link regain in the I shape fixed block in unmanned plane body lumen, thus contiguous block blocks unmanned owner The both sides of body, and connecting rod drives main rotary shaft and main screw to be retracted to the both sides of unmanned plane main body, by loosening fixing spiral shell Bolt, can make rotary shaft rotate in lower rotary shaft, thus revolute pair connecting rod, make secondary connecting rod drive secondary rotary shaft and The secondary oar that rotates turns to the corner of unmanned plane main body, carries handle and can take dynamic very easily, it is easier to storage, more convenient takes Band, can play a very good protection to main rotary shaft and main screw simultaneously.
Accompanying drawing explanation
Fig. 1 is present configuration schematic diagram;
Fig. 2 is the unmanned plane body interior structural representation of the present invention;
Fig. 3 is the understructure schematic diagram of the present invention.
In figure: 1, unmanned plane main body, 2, secondary propeller main body, 201, secondary connecting rod, 202, fixing bolt, 203, secondary fixing Plate, 204, secondary rotary shaft, 205, the secondary oar that rotates, 206, lower rotary shaft, 207, upper rotary shaft, 3, base, 301, urceolus, 302, interior Cylinder, 303, groove, 304, roating sphere, 305, sucker, 4, expansion link, 5, main screw, 6, main rotary shaft, 7, protecting film, 8, even Connect block, 9, connecting rod, 10, I shape fixed block, 11, reinforcing plate, 12, rubber sleeve, 13, handle.
Detailed description of the invention
Below in conjunction with the accompanying drawing in the embodiment of the present invention, the technical scheme in the embodiment of the present invention is carried out clear, complete Describe, it is clear that described embodiment is only a part of embodiment of the present invention rather than whole embodiments wholely.Based on Embodiment in the present invention, it is every other that those of ordinary skill in the art are obtained under not making creative work premise Embodiment, broadly falls into the scope of protection of the invention.
Referring to Fig. 1-3, the present invention provides a kind of technical scheme: a kind of Portable unmanned machine, including unmanned plane main body 1, The corner, bottom of described unmanned plane main body 1 is equipped with base 3, and described base 3 includes that urceolus 301, the bottom of described urceolus 301 set Having sucker 305, the inner side of described urceolus 301 to be provided with inner core 302, the circumference of described inner core 302 is provided with groove 303, described recessed The inner side of groove 303 is provided with roating sphere 304, inner core 302 can be made to rotate in urceolus 301 by rotary shaft 304, such that it is able to band Dynamic unmanned plane main body 1 rotates, and the left and right sides of described unmanned plane main body 1 is equipped with protecting film 7, is possible to prevent by protecting film 7 Unmanned plane main body 1 is worn and torn, and the bottom of described unmanned plane main body 1 is provided with handle 13, and the outer wall of described handle 13 is provided with rubber sleeve 12, can more easily carry unmanned plane main body 1 by handle 13, it is solid that the inner chamber of described unmanned plane main body 1 is provided with center Dingan County is all installed with expansion link 4, described work equipped with I shape fixed block 10, the left and right sides of described I shape fixed block 10 Font fixed block 10 is provided with reinforcing plate 11 with the junction of expansion link 4, by reinforcing plate 11 can make I shape fixed block 10 with The connection of expansion link 4 is more firm, and the outside of described expansion link 4 is installed with contiguous block 8, and the outside of described contiguous block 8 is fixed Being provided with connecting rod 9, the outer wall of described connecting rod 9 is provided with main rotary shaft 6, and the outer wall of described main rotary shaft 6 is provided with main spiral shell Rotation oar 5, by promoting contiguous block 8 that expansion link 4 can be made to regain in the I shape fixed block 10 in unmanned plane main body 1 inner chamber, from And contiguous block 8 blocks the both sides of unmanned plane main body 1, and connecting rod 9 drives main rotary shaft 6 and main screw 5 to be retracted to unmanned plane The both sides of main body 1, the corner of described unmanned plane main body 1 is all installed with secondary propeller main body 2, described secondary propeller main body 2 Including secondary fixed plate 203, the outside of described secondary fixed plate 203 is provided with lower rotary shaft 206, and the top of described lower rotary shaft 206 sets Upper rotary shaft 207, described upper rotary shaft 207 is had to be connected with lower rotary shaft 206 by fixing bolt 202, described upper rotary shaft 207 Outside be provided with secondary connecting rod 201, the outside of described secondary connecting rod 201 is provided with secondary rotary shaft 204, described secondary rotary shaft 204 Outer wall is provided with secondary rotation oar 205, by loosening fixing bolt 202, rotary shaft 207 can be made to turn in lower rotary shaft 206 Dynamic, thus revolute pair connecting rod 201, make secondary connecting rod 201 drive secondary rotary shaft 204 and the secondary oar 205 that rotates to turn to unmanned The corner of owner's body 1.
When not in use, by promoting contiguous block 8 that expansion link 4 can be made to regain the I shape in unmanned plane main body 1 inner chamber In fixed block 10, thus contiguous block 8 blocks the both sides of unmanned plane main body 1, and connecting rod 9 drives main rotary shaft 6 and main screw 5 It is retracted to the both sides of unmanned plane main body 1, by loosening fixing bolt 202, can make rotary shaft 207 in lower rotary shaft 206 Rotate, thus revolute pair connecting rod 201, make secondary connecting rod 201 drive secondary rotary shaft 204 and the secondary oar 205 that rotates to turn to nothing The corner of man-machine main body 1, carries handle 13 and can take dynamic very easily, it is easier to storage, more convenient carries, simultaneously can be to master Rotary shaft 6 and main screw 5 play a very good protection.
Although an embodiment of the present invention has been shown and described, for the ordinary skill in the art, permissible Understand and these embodiments can be carried out multiple change without departing from the principles and spirit of the present invention, revise, replace And modification, the scope of the present invention be defined by the appended.

Claims (6)

1. a Portable unmanned machine, including unmanned plane main body, it is characterised in that: the inner chamber of described unmanned plane main body is provided with center Position is installed with I shape fixed block, and the left and right sides of described I shape fixed block is all installed with expansion link, described The outside of expansion link is installed with contiguous block, and the outside of described contiguous block is installed with connecting rod, outside described connecting rod Wall is provided with main rotary shaft, and the outer wall of described main rotary shaft is provided with main screw, and the corner of described unmanned plane main body is the most fixing Being provided with secondary propeller main body, described secondary propeller main body includes that secondary fixed plate, the outside of described secondary fixed plate are provided with lower rotation Axle, the top of described lower rotary shaft is provided with rotary shaft, and described upper rotary shaft is connected with lower rotary shaft by fixing bolt, described The outside of upper rotary shaft is provided with secondary connecting rod, and the outside of described secondary connecting rod is provided with secondary rotary shaft, the outer wall of described secondary rotary shaft It is provided with secondary rotation oar.
A kind of Portable unmanned machine the most according to claim 1, it is characterised in that: the corner, bottom of described unmanned plane main body Being equipped with base, described base includes that urceolus, the inner side of described urceolus are provided with inner core, and the circumference of described inner core is provided with groove, The inner side of described groove is provided with roating sphere.
A kind of Portable unmanned machine the most according to claim 2, it is characterised in that: the bottom of described urceolus is provided with sucker.
A kind of Portable unmanned machine the most according to claim 1, it is characterised in that: described I shape fixed block and expansion link Junction be provided with reinforcing plate.
A kind of Portable unmanned machine the most according to claim 1, it is characterised in that: the left and right sides of described unmanned plane main body It is equipped with protecting film.
A kind of Portable unmanned machine the most according to claim 1, it is characterised in that: the bottom of described unmanned plane main body is provided with Handle, the outer wall of described handle is provided with rubber sleeve.
CN201610625688.1A 2016-08-01 2016-08-01 A kind of Portable unmanned machine Pending CN106081087A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201610625688.1A CN106081087A (en) 2016-08-01 2016-08-01 A kind of Portable unmanned machine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201610625688.1A CN106081087A (en) 2016-08-01 2016-08-01 A kind of Portable unmanned machine

Publications (1)

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108557053A (en) * 2018-02-05 2018-09-21 叶哲企 A kind of telescopic device of unmanned plane horn
CN108802280A (en) * 2018-05-29 2018-11-13 山西天时利和智能科技有限公司 A kind of unmanned plane atmospheric monitoring charging appliance

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN205022916U (en) * 2015-08-14 2016-02-10 湖北易瓦特科技股份有限公司 Portable flight equipment
CN205044967U (en) * 2015-09-21 2016-02-24 温州乐享科技信息有限公司 Unmanned aerial vehicle with reserve screw
CN205203378U (en) * 2015-08-24 2016-05-04 深圳市诺亚星辰科技开发有限公司 Improved multi -rotor unmanned aerial vehicle
CN205931241U (en) * 2016-08-01 2017-02-08 深圳市盛祥科技开发有限公司 Portable unmanned aerial vehicle

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN205022916U (en) * 2015-08-14 2016-02-10 湖北易瓦特科技股份有限公司 Portable flight equipment
CN205203378U (en) * 2015-08-24 2016-05-04 深圳市诺亚星辰科技开发有限公司 Improved multi -rotor unmanned aerial vehicle
CN205044967U (en) * 2015-09-21 2016-02-24 温州乐享科技信息有限公司 Unmanned aerial vehicle with reserve screw
CN205931241U (en) * 2016-08-01 2017-02-08 深圳市盛祥科技开发有限公司 Portable unmanned aerial vehicle

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108557053A (en) * 2018-02-05 2018-09-21 叶哲企 A kind of telescopic device of unmanned plane horn
CN108802280A (en) * 2018-05-29 2018-11-13 山西天时利和智能科技有限公司 A kind of unmanned plane atmospheric monitoring charging appliance

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Application publication date: 20161109