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 PDFInfo
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- 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
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- buckle
- bottom case
- shell
- housing
- bracket
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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
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.
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 |
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CN (1) | CN208377054U (en) |
-
2018
- 2018-04-09 CN CN201820494986.6U patent/CN208377054U/en not_active Expired - Fee Related
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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 |