CN208377054U - A kind of remote sensing unmanned plane being readily disassembled maintenance - Google Patents

A kind of remote sensing unmanned plane being readily disassembled maintenance Download PDF

Info

Publication number
CN208377054U
CN208377054U CN201820494986.6U CN201820494986U CN208377054U CN 208377054 U CN208377054 U CN 208377054U CN 201820494986 U CN201820494986 U CN 201820494986U CN 208377054 U CN208377054 U CN 208377054U
Authority
CN
China
Prior art keywords
buckle
bottom case
shell
housing
bracket
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
CN201820494986.6U
Other languages
Chinese (zh)
Inventor
欧伟洪
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.)
Qingyuan Jujin Technology Co Ltd
Original Assignee
Qingyuan Jujin 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 Qingyuan Jujin Technology Co Ltd filed Critical Qingyuan Jujin Technology Co Ltd
Priority to CN201820494986.6U priority Critical patent/CN208377054U/en
Application granted granted Critical
Publication of CN208377054U publication Critical patent/CN208377054U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Landscapes

  • Toys (AREA)

Abstract

The utility model discloses a kind of remote sensing unmanned planes for being readily disassembled maintenance, component is torn open including casing assembly, flight component and peace, it includes bottom case buckle, shell card slot, the first shell buckle and second housing buckle that the peace, which tears component open, the bottom case buckle is located at front on the left of the bottom case upper surface, and it is fixedly connected with the bottom case, the second housing inside front surface left bottom is equipped with the shell card slot, and the first shell buckle is located at front on the left of first upper surface of outer cover;Shell card slot is buckled and opened up by setting bottom case, it is convenient to be fixed bottom case and second housing by bottom case buckle and shell card slot, make the simpler convenience of installing and dismounting between bottom case and second housing, it is buckled by the first shell of setting and second housing buckles, it is convenient to pass through the first shell buckle and second housing buckle, fixed second housing and bottom case are buckled, keeps installing and dismounting between the first shell, second housing and bottom case more convenient.

Description

A kind of remote sensing unmanned plane being readily disassembled maintenance
Technical field
The utility model belongs to air vehicle technique field, and in particular to a kind of remote sensing unmanned plane for being readily disassembled maintenance.
Background technique
Unmanned plane is the not manned vehicle manipulated by radio robot or airborne computer stored program controlled. Unmanned plane structure is simple, use cost is low, can not only complete the task of manned aircraft execution, be more suitable for someone's aircraft not Preferably executing for task, such as the Geological Hazards Investigation of danger zone, air rescue commander and remote sensing of environment, unmanned plane is aerial The miniature remote sensing technology of remote sensing platform.
Traditional remote sensing unmanned plane is chiefly used in high-altitude shooting, environmental monitoring etc., is widely used in current social development, passes System remote sensing unmanned plane inconvenience detachable maintaining, the complicated large-scale remote sensing unmanned plane disassembly of certain structures is even more time-consuming and laborious, both The maintenance efficiency of maintenance man is influenced, and influences the development and popularization of remote sensing unmanned plane, and traditional remote sensing unmanned plane propeller and spiral shell Linear sundries is easily wound between rotation paddle fixed link, so that the normal flight of remote sensing unmanned plane is affected, also easily causes when serious distant Feel the damage of unmanned plane.
Utility model content
The purpose of this utility model is to provide a kind of remote sensing unmanned planes for being readily disassembled maintenance, to solve above-mentioned background skill The traditional remote sensing unmanned plane inconvenience detachable maintaining proposed in art, the complicated large-scale remote sensing unmanned plane disassembly of certain structures are even more It is time-consuming and laborious, the maintenance efficiency of maintenance man was not only influenced, but also influence the development and popularization of remote sensing unmanned plane, and traditional remote sensing unmanned plane Linear sundries is easily wound between propeller and propeller fixed link, so that the normal flight of remote sensing unmanned plane is affected, when serious The problem of also easily causing remote sensing unmanned plane to damage.
To achieve the above object, the utility model provides the following technical solutions: a kind of remote sensing being readily disassembled maintenance nobody Machine, including casing assembly, flight component and peace tear component open, and the casing assembly includes bottom case, the first shell, second housing and falls Ground frame, first shell are located on the right side of the bottom case upper surface, and buckle and fix with the bottom case, and the second housing is located at Close to the left side of first shell on the left of the bottom case upper surface, the second housing is fixed with the bottom case, described Floor stand is located at the bottom case lower surface, and is fixedly connected with the bottom case, and the flight component includes photographing module, bracket buckle Fixing seat, first support button, second support button, propeller mounting rod, propeller and antiwind cap, the photographing module are located at described It on the right side of bottom case lower surface, and is fixedly connected with the bottom case, the bracket buckle fixed seating is in second housing left side wall top Portion, and being fixedly connected with the second housing, the first support button bit in bracket button fixing seat upper surface, and with it is described Bracket button fixing seat is hinged, and the second support button bit is fixed in bracket button fixing seat lower surface, and with the bracket buckle Seat is hinged, and the propeller mounting rod, the propeller installation are equipped between the first support button and the second support button Bar is fixed with the first support button and the second support buckle button, and the propeller is located at table on the propeller mounting rod Face, and be rotatablely connected with the propeller mounting rod, the antiwind cap is located at propeller mounting rod upper surface close to described The lateral wall of propeller, the antiwind cap are fixedly connected with the propeller mounting rod, the photographing module and external power supply electricity Property connection, it is described peace tear open component include bottom case buckle, shell card slot, the first shell buckle, second housing buckle, bracket buckle buckle With bracket buckle card slot, the bottom case buckle is located at front on the left of the bottom case upper surface, and is fixedly connected with the bottom case, described Second housing inside front surface left bottom is equipped with the shell card slot, and the first shell buckle is located on first shell Front on the left of surface, and be fixedly connected with first shell, the second housing buckle is located at first shell lower surface In front of left side, and it is fixedly connected with first shell, the bracket buckle buckle is located at the second support and buckles in front of surface, And be fixedly connected with the second support button, the first support button inside front surface is equipped with the bracket buckle card slot.
Preferably, first shell and the second housing and the bottom case are buckled and described by first shell Second housing buckle buckle is fixed.
Preferably, the bottom case is buckled with the second housing by the bottom case and the shell card slot is fixed.
Preferably, the antiwind cap is with the propeller mounting rod by being plugged and fixed.
Preferably, shaft, the first support button and the bracket button fixing seat are equipped with inside the bracket button fixing seat It is hinged by the shaft with the second support button and the bracket button fixing seat.
Compared with prior art, the utility model has the beneficial effects that passing through the front setting bottom on the left of bottom case upper surface Shell buckles and opens up shell card slot in second housing inside front surface left bottom, convenient to pass through bottom case buckle and shell card slot card Fixed bottom case and second housing are closed, makes the simpler convenience of installing and dismounting between bottom case and second housing, by the first shell Front the first shell of setting buckles on the left of upper surface and front setting second housing buckles on the left of the first shell lower surface, convenient By the first shell buckle and second housing buckle, fixed second housing and bottom case are buckled, the first shell, second housing and bottom are made Installing and dismounting is more convenient between shell, bracket buckle buckle is arranged in front of surface and in first support button by buckling in second support Inside front surface opens up bracket buckle card slot, convenient to fix second support button and the by bracket buckle buckle and bracket buckle card slot buckle One bracket buckle facilitates installing and dismounting propeller mounting rod and propeller, by pacifying in propeller for fixing propeller mounting rod It fills bar upper surface and antiwind cap is set, facilitate protection propeller mounting rod and propeller junction, reduce linear sundries winding, ensure The normal use of remote sensing unmanned plane.
Detailed description of the invention
Fig. 1 is the structural schematic diagram of the utility model;
Fig. 2 is the structure top view of the utility model;
Fig. 3 is the first shell mechanism schematic diagram in the utility model;
In figure: 10- casing assembly, 11- bottom case, the first shell of 12-, 13- second housing, 14- floor stand, 20- flight crew Part, 21- photographing module, 22- bracket button fixing seat, 23- first support button, 24- second support button, 25- propeller mounting rod, 26- propeller, 27- antiwind cap, 30- peace tear component open, 31- bottom case buckle, 32- shell card slot, the first shell of 33- buckle, 34- the Two shells buckle, 35- bracket buckle buckle, 36- bracket buckle card slot.
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. 1-3 is please referred to, the utility model provides a kind of technical solution: a kind of remote sensing unmanned plane being readily disassembled maintenance, Component 30 is torn open including casing assembly 10, flight component 20 and peace, and casing assembly 10 includes bottom case 11, outside the first shell 12, second Shell 13 and floor stand 14, the first shell 12 are located on the right side of 11 upper surface of bottom case, and buckle and fix with bottom case 11, and second housing 13 Close to the left side of the first shell 12 on the left of 11 upper surface of bottom case, second housing 13 is fixed with bottom case 11, and floor stand 14 It is fixedly connected in 11 lower surface of bottom case, and with bottom case 11, flight component 20 includes photographing module 21, bracket button fixing seat 22, the One bracket buckle 23, second support button 24, propeller mounting rod 25, propeller 26 and antiwind cap 27, photographing module 21 are located at bottom case It on the right side of 11 lower surfaces, and is fixedly connected with bottom case 11, bracket button fixing seat 22 is located at 13 left side wall of second housing top, and with the Two shells 13 are fixedly connected, and first support button 23 is located at 22 upper surface of bracket button fixing seat, and hinged with bracket button fixing seat 22, Second support button 24 is located at 22 lower surface of bracket button fixing seat, and hinged with bracket button fixing seat 22, first support button 23 and the It is equipped with propeller mounting rod 25, propeller mounting rod 25 and first support button 23 between two bracket buckles 24 and second support button 24 blocks Button is fixed, and propeller 26 is located at 25 upper surface of propeller mounting rod, and is rotatablely connected with propeller mounting rod 25, antiwind cap 27 In 25 upper surface of propeller mounting rod close to the lateral wall of propeller 26, antiwind cap 27 is fixedly connected with propeller mounting rod 25, Photographing module 21 and external power supply are electrically connected, and it includes bottom case buckle 31, shell card slot 32, the first shell buckle that peace, which tears component 30 open, 33, second housing buckle 34, bracket buckle buckle 35 and bracket buckle card slot 36, before bottom case buckle 31 is located on the left of 11 upper surface of bottom case Side, and be fixedly connected with bottom case 11,13 inside front surface left bottom of second housing is equipped with shell card slot 32, the first shell buckle 33 are located at front on the left of 12 upper surface of the first shell, and are fixedly connected with the first shell 12, and second housing buckle 34 is located at first Front on the left of 12 lower surface of shell, and be fixedly connected with the first shell 12, bracket buckle buckle 35 is located at table on second support button 24 Side in front, and be fixedly connected with second support button 24,23 inside front surface of first support button is equipped with bracket buckle card slot 36.
In the present embodiment, 21 model 205M of photographing module, bottom case buckles 31 surfaces and offers clamping screw thread, and bottom case is arranged Buckle 31 and open up shell card slot 32, it is convenient by bottom case buckle 31 and shell card slot 32 be fixed bottom case 11 and second housing 13, the first shell buckle 33 and second housing buckle 34 surfaces and offer clamping screw thread, and the first shell of setting buckles 33 and second Shell buckle 34 facilitates the fixed second housing 13 of buckle and bottom case 11, bracket buckle to buckle 35 surfaces and offer clamping screw thread, is arranged Bracket buckle buckles 35 and opens up bracket buckle card slot 36, facilitates the fixed second support button 24 of buckle and first support button 23, for admittedly Determine propeller mounting rod 25.
In the present embodiment, setting bottom case buckles 31 and opens up shell card slot 32, convenient to pass through bottom case buckle 31 and shell Card slot 32 is fixed bottom case 11 and second housing 13, makes the simpler side of installing and dismounting between bottom case 11 and second housing 13 Just, the first shell of setting buckles 33 and second housing buckle 34, facilitates the fixed second housing 13 of buckle and bottom case 11, makes outside first Installing and dismounting is more convenient between shell 12, second housing 13 and bottom case 11, and setting bracket buckle buckles 35 and opens up bracket buckle card slot 36, facilitate the fixed second support button 24 of buckle and first support button 23 to facilitate installing and dismounting for fixing propeller mounting rod 25 Propeller mounting rod 25 and propeller 26.
Further, the first shell 12 passes through the first shell buckle 33 and second housing card with second housing 13 and bottom case 11 34 buckle of button is fixed.
In the present embodiment, the first shell 12 and second is fixed by the first shell buckle 33 and 34 buckle of second housing buckle Shell 13 and bottom case 11 keep installing and dismounting between the first shell 12, second housing 13 and bottom case 11 more convenient.
Further, bottom case 11 is fixed with second housing 13 by bottom case buckle 31 and shell card slot 32.
In the present embodiment, it is fixed bottom case 11 and second housing 13 by bottom case buckle 31 and shell card slot 32, makes bottom The simpler convenience of installing and dismounting between shell 11 and second housing 13.
Further, antiwind cap 27 is with propeller mounting rod 25 by being plugged and fixed.
In the present embodiment, by the way that antiwind cap 27 and propeller mounting rod 25 is plugged and fixed, both installation antiwind caps easy to disassemble 27, and facilitate protection propeller mounting rod 25 and 26 junction of propeller, linear sundries winding is reduced, ensures remote sensing unmanned plane Normal use.
Further, shaft, first support button 23 and bracket button fixing seat 22 and the are equipped with inside bracket button fixing seat 22 Two bracket buckles 24 and bracket button fixing seat 22 are hinged by shaft.
It is convenient to pass through the hinged first support of shaft by being equipped with shaft inside bracket button fixing seat 22 in the present embodiment Button 23 and bracket button fixing seat 22 and second support button 24 and bracket button fixing seat 22, for buckling fixed propeller mounting rod 25, facilitate installing and dismounting propeller mounting rod 25 and propeller 26.
The working principle and process for using of the utility model: after the utility model installs, remote sensing unmanned plane is full of Power supply, starting remote sensing unmanned plane switch carry out remote sensing control shooting, and antiwind cap 27 will protect propeller mounting rod in shooting process 25 ensure the normal use of remote sensing unmanned plane not by the winding of linear sundries with 26 junction of propeller, when needing detachable maintaining, Remote sensing unmanned plane switch is closed, first passes through and is connected between opening bracket buckle buckle 35 and bracket buckle card slot 36, remove propeller peace Bar 25 and propeller 26 are filled, then by pushing the first shell buckle 33 and second housing buckle 34 open, removes second housing 13, finally The first shell 12 is extracted, is repaired, maintenance terminates, and installs back the first shell 12, second housing 13,25 and of propeller mounting rod Propeller 26, starting remote sensing unmanned plane switch, continues normal use.
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 (5)

1. a kind of remote sensing unmanned plane for being readily disassembled maintenance, it is characterised in that: including casing assembly (10), flight component (20) and Peace is torn open component (30), and the casing assembly (10) includes bottom case (11), the first shell (12), second housing (13) and floor stand (14), first shell (12) is located on the right side of the bottom case (11) upper surface, and buckles and fix with the bottom case (11), described Second housing (13) is located at the left side on the left of the bottom case (11) upper surface close to first shell (12), the second housing (13) be fixed with the bottom case (11), the floor stand (14) is located at the bottom case (11) lower surface, and with the bottom case (11) it is fixedly connected, the flight component (20) includes that photographing module (21), bracket button fixing seat (22), first support are buckled (23), second support button (24), propeller mounting rod (25), propeller (26) and antiwind cap (27), the photographing module (21) It on the right side of the bottom case (11) lower surface, and is fixedly connected with the bottom case (11), the bracket button fixing seat (22) is located at At the top of second housing (13) left side wall, and it is fixedly connected with the second housing (13), first support button (23) position In bracket button fixing seat (22) upper surface, and hingedly with the bracket button fixing seat (22), the second support button (24) Positioned at bracket button fixing seat (22) lower surface, and hingedly with the bracket button fixing seat (22), the first support button (23) the propeller mounting rod (25), the propeller mounting rod (25) and institute are equipped between the second support button (24) It states first support button (23) and the second support button (24) buckle is fixed, the propeller (26) is located at propeller installation Bar (25) upper surface, and be rotatablely connected with the propeller mounting rod (25), the antiwind cap (27) is located at propeller peace Bar (25) upper surface is filled close to the lateral wall of the propeller (26), the antiwind cap (27) and the propeller mounting rod (25) Be fixedly connected, the photographing module (21) and external power supply are electrically connected, the peace tear open component (30) include bottom case buckle (31), Shell card slot (32), the first shell buckle (33), second housing buckle (34), bracket buckle buckle (35) and bracket buckle card slot (36), the bottom case buckle (31) is located at front on the left of the bottom case (11) upper surface, and is fixedly connected with the bottom case (11), Second housing (13) the inside front surface left bottom is equipped with the shell card slot (32), and first shell buckles (33) position The front on the left of the first shell (12) upper surface, and be fixedly connected with first shell (12), the second housing card It detains (34) and is located at front on the left of the first shell (12) lower surface, and be fixedly connected with first shell (12), the branch Frame buckle, which buckles (35) and is located at the second support, to be buckled in front of (24) upper surface, and is fixedly connected with the second support button (24), First support button (23) inside front surface is equipped with the bracket buckle card slot (36).
2. a kind of remote sensing unmanned plane for being readily disassembled maintenance according to claim 1, it is characterised in that: first shell (12) pass through first shell buckle (33) and the second housing card with the second housing (13) and the bottom case (11) (34) buckle is detained to fix.
3. a kind of remote sensing unmanned plane for being readily disassembled maintenance according to claim 1, it is characterised in that: the bottom case (11) It is fixed with the second housing (13) by bottom case buckle (31) and the shell card slot (32).
4. a kind of remote sensing unmanned plane for being readily disassembled maintenance according to claim 1, it is characterised in that: the antiwind cap (27) with the propeller mounting rod (25) by being plugged and fixed.
5. a kind of remote sensing unmanned plane for being readily disassembled maintenance according to claim 1, it is characterised in that: the bracket buckle is solid Shaft, the first support button (23) and the bracket button fixing seat (22) and the second support button are equipped with inside reservation (22) (24) and the bracket button fixing seat (22) is hinged by the shaft.
CN201820494986.6U 2018-04-09 2018-04-09 A kind of remote sensing unmanned plane being readily disassembled maintenance Expired - Fee Related CN208377054U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201820494986.6U CN208377054U (en) 2018-04-09 2018-04-09 A kind of remote sensing unmanned plane being readily disassembled maintenance

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201820494986.6U CN208377054U (en) 2018-04-09 2018-04-09 A kind of remote sensing unmanned plane being readily disassembled maintenance

Publications (1)

Publication Number Publication Date
CN208377054U true CN208377054U (en) 2019-01-15

Family

ID=64975948

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201820494986.6U Expired - Fee Related CN208377054U (en) 2018-04-09 2018-04-09 A kind of remote sensing unmanned plane being readily disassembled maintenance

Country Status (1)

Country Link
CN (1) CN208377054U (en)

Similar Documents

Publication Publication Date Title
CN107428413A (en) Unmanned vehicle with three wings configuration
JP2022523605A (en) Unmanned aircraft with integrated renewable energy automatic charging system
CN206141810U (en) Unmanned vehicles and frame thereof
CN208377054U (en) A kind of remote sensing unmanned plane being readily disassembled maintenance
CN204231558U (en) Portable emergency supervising device
CN104843191B (en) Contactless smart rain insensitive device for unmanned plane
CN209037840U (en) A kind of unmanned plane wing safeguard structure
CN206345016U (en) Delay to fall protection device and unmanned plane in the air
CN209148037U (en) A kind of novel agricultural monitoring using remote sensing vehicle
CN206417173U (en) The body cover and unmanned plane of a kind of unmanned plane
CN108732308A (en) A kind of gas measurement device based on eight rotor wing unmanned aerial vehicles
CN207725615U (en) The self-balancing wing of unmanned plane
CN204623831U (en) The portable quadrotor of rotor arm replaceable
CN209148490U (en) A kind of PM2.5 environment monitoring device
CN106531925A (en) Power cabin
CN208689776U (en) A kind of emulation cockpit panel module for flight simulation
CN104518271A (en) Portable automatic star finding system
CN206456551U (en) A kind of Intelligent unattended aircraft
CN209691106U (en) A kind of city commander parking guidance screen shade
CN205819558U (en) aircraft rotor driver mounting seat
CN205030047U (en) A shield cover for on multiaxis aircraft
CN110654538A (en) Weather detection unmanned aerial vehicle
CN208070033U (en) A kind of protective device of unmanned plane
CN207029573U (en) A kind of unmanned plane night flight lamp wireless control system
CN210488887U (en) Flight simulator shell

Legal Events

Date Code Title Description
GR01 Patent grant
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20190115

Termination date: 20200409

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