CN208360492U - A kind of novel four axis folding storage formula aerial photography aircraft - Google Patents
A kind of novel four axis folding storage formula aerial photography aircraft Download PDFInfo
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- CN208360492U CN208360492U CN201820807056.1U CN201820807056U CN208360492U CN 208360492 U CN208360492 U CN 208360492U CN 201820807056 U CN201820807056 U CN 201820807056U CN 208360492 U CN208360492 U CN 208360492U
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Abstract
The utility model relates to Multi-axis aircraft technical fields, and in particular to a kind of novel four axis folding storage formula aerial photography aircraft.It includes aircraft casing, the aircraft casing is made of upper cover plate and lower plate, the upper cover plate bottom surface is equipped with intelligent control mainboard, it is equipped with that signal dispatcher module, WIFI module, light stream module, contact to earth induction module and power switch in intelligent control mainboard, for the folding rotor by support arm and flight arm, flight arm bottom and support arm front end are rotation connection.The utility model has the advantages that: the utility model innovative design folding rotor structure, change rotor flying component stress condition in landing, reduce the impact stress that rotor is subject to, it is also additionally arranged the highly sensitive sensing device that contacts to earth simultaneously, enable aircraft more slowly steady safer when landing, WIFI signal coverage area is wider, and signal is more stable, assurance and control of more convenient operator to flying vehicles control flight path.
Description
Technical field
The utility model relates to Multi-axis aircraft technical fields, and in particular to the novel four axis folding storage formula of one kind is taken photo by plane winged
Row device.
Background technique
It can capture more niceness and moment by photography, simple camera can no longer meet modern people
For the pursuit that vision stops, also occur the aircraft of many different styles currently on the market, is flown by aircraft in high-altitude
Row is taken photo by plane, and existing aerial photography aircraft volume is more significantly, inconvenient to carry, while some compacts also occur can
All integral structure is used to design with the wing rotor of the aerial photography aircraft of folding, but most small-sized aerial photography devices, designed in this way
Although can achieve the purpose that reduce volume, due to the unbalance stress of integral type wing, do not have when aerial photography device is landed
There is auxiliary body, directly land, biggish impact stress can be generated to wing in the process, rear wing is used for multiple times and is easy to appear not
With the damage of degree, the phenomenon that causing unbalanced landing to bounce, also has probability wing occur and the irreversible situation such as fractures, if
Increasing buffer unit then will increase the weight of aerial photography device, needs to readjust the counterweight of aerial photography device, otherwise will affect flight of taking photo by plane
The performance of having a smooth flight of device.In consideration of it, we design it is a can more preferably disperse the impact stress being subject to when aircraft lands,
Landing more smooth flight device, solves the problems, such as that above-mentioned existing aerial photography aircraft exists.
Summary of the invention
The utility model aim be to provide it is a kind of be able to solve above-mentioned existing aircraft there are the problem of novel four axis
Folding storage formula aerial photography aircraft.
The utility model is accomplished by the following way:
A kind of novel four axis folding storage formula aerial photography aircraft comprising aircraft casing, it is characterised in that: aircraft shell
Body is made of upper cover plate and lower plate, and the upper cover plate bottom surface is equipped with intelligent control mainboard, is equipped with letter in intelligent control mainboard
Breath transceiver module, WIFI module, light stream module, contact to earth induction module and power switch, and battery is equipped in front of power switch and is touched
Piece connects warning flashing lamp in intelligent control mainboard tail portion, and the aircraft casing front end is equipped with adjustable camera, aircraft
Rotor accommodating groove is equipped at left and right sides of shell, the lower plate quadrangle is set there are four rotor installation column, and rotor is installed on column
Folding rotor is installed, lower plate, which is equipped with battery compartment, switch key and contacts to earth, incudes light-transmitting plate, and lower plate tail portion is equipped with light transmission
Cover, the battery compartment are provided with detachable battery, and the folding rotor is by support arm and flight arm, flight arm bottom and branch
Brace front end is rotation connection, and support arm end is provided with mounting hole, and the mounting hole cooperation is mounted on rotor installation column, institute
It states support arm front end and limits iron wire equipped with flight arm, flight arm bottom is equipped with landing bracket, and flight arm is provided with rotor horse
It reaches, rotor bracket is installed above rotor motor, rotor bracket two sides connect foldable flaps.
Further, it is equipped with rotor limit protrusion and locating clamp plate on the inside of the rotor installation column, in support arm bottom
If support arm tail portion is equipped with positioning vertical column, limiting groove and rotor limit protrusion cooperation there are two limiting groove, positioning vertical column with
Locating clamp plate cooperation.
Further, the battery compartment two sides of the bottom are equipped with battery construction opening, are equipped with limit below battery construction opening
Sliding groove, battery compartment front end are equipped with battery clamping groove, are equipped with fixed baffle, the detachable electricity in battery clamping groove top
Pond two sides are equipped with the retention bead that cooperate with battery construction opening, and detachable battery front end is equipped with fixed plate, the fixed plate and
Fixed baffle cooperation, detachable battery tail portion is equipped with concave contact.
Further, the battery clamping groove is step.
Further, the adjustable camera two sides are equipped with support cylinder, and support cylinder frame is placed on turning for bottom front edge of board
In dynamic groove, limit plate is installed at the top of turning groove.
Further, the limit plate shape is " U " font, is equipped with support post, support post bottom below limit plate
It pushes down to contact to earth and incudes light-transmitting plate.
Further, described contact to earth incudes light-transmitting plate below the induction module that contacts to earth, and induction module is aligned with contacting to earth.
Further, the switch key tail portion is against protrusion at the top of power switch.
Further, the flight arm folds vertically and after support arm, and flight arm bottom landing bracket end of contacting to earth is higher than
Lower plate bottom.
The fixed baffle is upturned, and tilting angular range is 5 ° -15 °.
The advantages of novel four axis folding storage formula aerial photography aircraft provided by the utility model, is: described in the utility model one
Novel four axis folding storage formula aerial photography aircraft innovative design folding rotor structure is planted, rotor flying component is changed and is falling
Stress condition when ground reduces the impact stress that rotor is subject to, while being also additionally arranged the highly sensitive sensing device that contacts to earth, can
Real-time synchronization adjusts the revolving speed of four rotors, enables aircraft more slowly steady when landing, is also more convenient aircraft
It adjusts the angle in the sky and direction, the landing bracket of rotor bottom can guarantee after aircraft landing that bottom surface battery compartment etc. will not be with
Ground directly contacts, safer, and using novel WIFI signal module, WIFI signal coverage area is wider, and signal is more
Stablize, assurance and control of more convenient operator to flying vehicles control flight path.
Detailed description of the invention
Fig. 1 is the deployed configuration schematic diagram of the utility model；
Fig. 2 is the intake type structural schematic diagram of the utility model；
Fig. 3 is the lower plate bottom surface structure schematic diagram of the utility model；
Fig. 4 is the lower plate positive structure schematic of the utility model；
Fig. 5 is the intelligent control mainboard structure schematic diagram of the utility model；
Fig. 6 is the folding rotor structural schematic diagram of the utility model；
Fig. 7 is the support arm bottom substance schematic diagram of the utility model；
Fig. 8 is the Detachable battery structure schematic diagram of the utility model；
Fig. 9 is the detachable battery tail structure schematic diagram of the utility model.
Specific embodiment
In order to enable juror to be further understood that the purpose, feature and function of the utility model, below in conjunction with
The present invention will be further described for attached drawing:
It please refers to shown in Fig. 1-9, is the structural schematic diagram for the utility model, the utility model is a kind of novel four axis folding
Folded intake type aerial photography aircraft comprising aircraft casing, it is characterised in that: aircraft casing is by upper cover plate 1 and 2 groups of lower plate
At,
1 bottom surface of upper cover plate is equipped with intelligent control mainboard 3, be equipped in intelligent control mainboard 3 signal dispatcher module 31,
WIFI module 32, light stream module 33, contact to earth induction module 34 and power switch 35, and battery contact is equipped in front of power switch 35
36, warning flashing lamp 4 is connected in 3 tail portion of intelligent control mainboard,
The aircraft casing front end is equipped with adjustable camera 6, is equipped with rotor accommodating groove at left and right sides of aircraft casing
22,
2 four jiaos of the lower plate is set there are four rotor installation column 21, and rotor is installed and is equipped with folding rotor on column 21
5, lower plate 2, which is equipped with battery compartment 7, switch key 27 and contacts to earth, incudes light-transmitting plate 28, and 2 tail portion of lower plate is equipped with translucent cover 26, institute
It states battery compartment 7 and is provided with detachable battery 8,
For the folding rotor 5 by support arm 51 and flight arm 52,52 bottom of flight arm and 51 front end of support arm are to turn
Dynamic connection, 51 end of support arm are provided with mounting hole 57, and the cooperation of mounting hole 57 is mounted on rotor installation column 21, the branch
51 front end of brace is equipped with flight arm and limits iron wire 53,
52 bottom of flight arm is equipped with landing bracket 50, and flight arm 52 is provided with rotor motor 54, on rotor motor 54
Side's installation rotor bracket 56,56 two sides of rotor bracket connect foldable flaps 55.
Further, it is equipped with rotor limit protrusion 24 and locating clamp plate 25 on the inside of the rotor installation column 21, supported
51 bottom of arm is set there are two limiting groove 58, and 51 tail portion of support arm is equipped with positioning vertical column 59, limiting groove 58 and rotor limit convex
24 cooperation out, positioning vertical column 59 and locating clamp plate 25 cooperate.
Further, 7 two sides of the bottom of battery compartment are equipped with battery construction opening 71, are equipped with below battery construction opening 71
Sliding groove 72 is limited, 7 front end of battery compartment is equipped with battery clamping groove 73, and fixed baffle is equipped at the top of battery clamping groove 73
74,8 two sides of detachable battery are equipped with the retention bead 81 cooperated with battery construction opening 71, and 8 front end of detachable battery is set
There is fixed plate 82, the fixed plate 82 cooperates with fixed baffle 74, and 8 tail portion of detachable battery is equipped with concave contact 83.
Further, the battery clamping groove 73 is step.
Further, 6 two sides of adjustable camera are equipped with support cylinder 61, before support 61 frame of cylinder is placed on lower plate 2
In the turning groove 23 at end, limit plate 9 is installed at the top of turning groove 23.
Further, 9 shape of limit plate is " U " font, is equipped with support post 91, support post below limit plate 9
91 bottoms, which are pushed down to contact to earth, incudes light-transmitting plate 28.Limit plate 9 can limit the movement that adjustable camera 6 does vertical direction, while
It can play the role of fixed contact to earth and incude light-transmitting plate 28.
Further, described contact to earth incudes light-transmitting plate 28 positioned at 34 lower section of induction module of contacting to earth, with the induction module 34 that contacts to earth
Alignment.
Further, 27 tail portion of switch key, which is against at the top of power switch 35, protrudes.
Further, the flight arm 52 folds vertically and after support arm 51, and 52 bottom landing bracket 50 of flight arm contacts to earth
End is higher than 2 bottom of lower plate.
The fixed baffle 74 is upturned, and tilting angular range is 5 ° -15 °.
When use, first 8 tail portion of detachable battery is put into battery compartment 7, retention bead 81 is embedded in battery installation and opens
In mouth 71, so that fixed plate 82 pushes down fixed baffle 74, the concave contact 83 of 8 tail portion of detachable battery is directed at battery contact
36, it is then inwardly slided along limit sliding groove 72, until fixed plate 82 slides into fixed 74 end of baffle, fixed baffle 74 resets
It tilts, resists 82 front end of fixed plate at the top of fixed baffle 74, detachable battery 8 installs.
Then four folding rotors 5 being accommodated in rotor accommodating groove 22 are horizontally rotated 90 ° outward, rotor limits at this time
Protrusion 24 is fallen into the limiting groove 58 of 51 bottom of support arm, and folding rotor 5 is fixed, vertical in the positioning by 51 tail portion of support arm
Column 59 sticks on 25 inside of locating clamp plate, prevents folding rotor 5 beyond rotational angle range；Four folding rotors 5 horizontally rotate
After, flight arm 52 is rotated 90 ° along the vertical direction, iron wire 53 is limited by the flight arm of 51 front end of support arm and blocks flight
52 bottom of arm, guarantees that the rotation of flight arm 52 is fixed to vertical direction, is then unfolded respectively foldable on four rotor brackets 56
Fin 55 adjusts the shooting angle of adjustable camera 6.
Long-pressing switch key 27 starts aircraft by power switch 35, until warning flashing lamp 4 to light, can use
The wireless network signal that mobile phone searching WIFI module 32 issues can be checked after being connected to the wireless network signal by system
The picture signal that the adjustable camera 6 acquired to signal dispatcher module 31 takes, the wireless network letter that WIFI module 32 issues
It number can support the manipulation in 30 meters, wide coverage then controls aircraft takeoff, takes photo by plane.Aircraft in the sky, leads to
It crosses built in light flow module 33 and controls folding rotor 5, realize the movement such as aerial spot hover and rotation.Aircraft passes through built-in letter
Breath transceiver module 31 sends the picture that adjustable camera 6 is implemented to take on mobile phone operation interface.Flashing lamp 4 is warned to fly
Row process keeps flashing, serves as a warning, and guarantees flight safety.
After taking photo by plane, control aircraft landing when aircraft is apart from landing face 25cm or so, contacts to earth and incudes mould
Block 34 starts, and incudes the sending detectable signal of light-transmitting plate 28 via contacting to earth by contacting to earth induction module 34, receives feedback signal adjusting
The revolving speed of the rotor motor 54 of four folding rotors 5 makes aircraft keep balance, steadily lands, finally 52 bottom of flight arm
If landing bracket 50 contact to earth, support aircraft.
After taking photo by plane, long-pressing switch key 27 again closes aircraft power, vertically back flight arm 52
Rotation releases the limitation of flight arm limit iron wire 53, and on the same line, folding is packed up foldable for flight arm 52 and support arm 51
Fin 55, then the folding rotor 5 folded is rotated 90 ° in the horizontal direction, it withdraws in rotor accommodating groove 22, rotor limits at this time
Protrusion 24 is fallen into another limiting groove 58 of 51 bottom of support arm, is pressed fixed baffle 74, is released detachable battery forward
8, detachable battery 8 is taken out, aircraft recycling is completed.
Certainly, the above is only the preferred embodiment of the utility model, and the scope of application of the utility model is not limited with this,
Therefore it is all made in the utility model principle it is equivalent change should be included in the protection scope of the utility model.
Claims (10)
1. a kind of novel four axis folding storage formula aerial photography aircraft comprising aircraft casing, it is characterised in that: the aircraft
Shell is made of upper cover plate (1) and lower plate (2),
Upper cover plate (1) bottom surface is equipped with intelligent control mainboard (3), is equipped with signal dispatcher module in intelligent control mainboard (3)
(31), WIFI module (32), light stream module (33), the induction module that contacts to earth (34) and power switch (35), in power switch (35)
Front is equipped with battery contact (36), connects warning flashing lamp (4) in intelligent control mainboard (3) tail portion,
The aircraft casing front end is equipped with adjustable camera (6), and rotor accommodating groove is equipped at left and right sides of aircraft casing
(22),
Lower plate (2) quadrangle is set there are four rotor installation column (21), and rotor, which is installed, is equipped with folding rotation on column (21)
The wing (5), lower plate (2) is equipped with battery compartment (7), switch key (27) and contacting to earth incudes light-transmitting plate (28), and lower plate (2) tail portion fills
Having translucent cover (26), the battery compartment (7) is provided with detachable battery (8),
The folding rotor (5) is made of support arm (51) and flight arm (52), flight arm (52) bottom and support arm
(51) front end is rotation connection, and support arm (51) end is provided with mounting hole (57), and mounting hole (57) cooperation is mounted on rotor
It installs on column (21), support arm (51) front end is equipped with flight arm limit iron wire (53),
Flight arm (52) bottom is equipped with landing bracket (50), and flight arm (52) is provided with rotor motor (54), rotor motor
(54) rotor bracket (56) are installed in top, and rotor bracket (56) two sides connect foldable flaps (55).
2. the novel four axis folding storage formula aerial photography aircraft of one kind according to claim 1, it is characterised in that: the rotor
It installs and is equipped with rotor limit protrusion (24) and locating clamp plate (25) on the inside of column (21), set that there are two limit in support arm (51) bottom
Position groove (58), support arm (51) tail portion are equipped with positioning vertical column (59), limiting groove (58) and rotor limit protrusion (24) cooperation,
Positioning vertical column (59) and locating clamp plate (25) cooperate.
3. the novel four axis folding storage formula aerial photography aircraft of one kind according to claim 1, it is characterised in that: the battery
Storehouse (7) two sides of the bottom are equipped with battery construction opening (71), and limit sliding groove (72), battery are equipped with below battery construction opening (71)
Storehouse (7) front end is equipped with battery clamping groove (73), is equipped at the top of battery clamping groove (73) fixed baffle (74), described removable
It unloads battery (8) two sides and is equipped with the retention bead (81) cooperated with battery construction opening (71), detachable battery (8) front end is equipped with solid
Fixed board (82), the fixed plate (82) and fixed baffle (74) cooperation, detachable battery (8) tail portion are equipped with concave contact
(83).
4. the novel four axis folding storage formula aerial photography aircraft of one kind according to claim 3, it is characterised in that: the battery
Clamping groove (73) is step-like recesses.
5. the novel four axis folding storage formula aerial photography aircraft of one kind according to claim 1, it is characterised in that: described adjustable
Camera (6) two sides are equipped with support cylinder (61), and support cylinder (61) frame is placed on the turning groove (23) of lower plate (2) front end
It is interior, limit plate (9) are installed at the top of turning groove (23).
6. the novel four axis folding storage formula aerial photography aircraft of one kind according to claim 5, it is characterised in that: the limit
Plate (9) shape is " U " font, is equipped with support post (91) below limit plate (9), induction of contacting to earth is pushed down in support post (91) bottom
Light-transmitting plate (28).
7. the novel four axis folding storage formula aerial photography aircraft of one kind according to claim 1, it is characterised in that: described to contact to earth
Induction light-transmitting plate (28) is located at below the induction module (34) that contacts to earth, and is aligned with the induction module that contacts to earth (34).
8. the novel four axis folding storage formula aerial photography aircraft of one kind according to claim 1, it is characterised in that: the switch
Key (27) tail portion is against protrusion at the top of power switch (35).
9. the novel four axis folding storage formula aerial photography aircraft of one kind according to claim 1, it is characterised in that: the flight
Arm (52) folds vertically and after support arm (51), and flight arm (52) bottom landing bracket (50) contacts to earth end higher than lower plate (2)
Bottom.
10. the novel four axis folding storage formula aerial photography aircraft of one kind according to claim 3, it is characterised in that: described solid
Determine baffle (74) to be upturned, tilting angular range is 5 ° -15 °.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820807056.1U CN208360492U (en) | 2018-05-26 | 2018-05-26 | A kind of novel four axis folding storage formula aerial photography aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820807056.1U CN208360492U (en) | 2018-05-26 | 2018-05-26 | A kind of novel four axis folding storage formula aerial photography aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208360492U true CN208360492U (en) | 2019-01-11 |
Family
ID=64930301
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820807056.1U Expired - Fee Related CN208360492U (en) | 2018-05-26 | 2018-05-26 | A kind of novel four axis folding storage formula aerial photography aircraft |
Country Status (1)
| Country | Link |
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| CN (1) | CN208360492U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110963030A (en) * | 2019-12-03 | 2020-04-07 | 徐州飞梦电子科技有限公司 | Unmanned aerial vehicle and using method thereof |
| CN112954092A (en) * | 2021-02-03 | 2021-06-11 | 维沃移动通信有限公司 | Electronic device |
| CN114476037A (en) * | 2021-12-30 | 2022-05-13 | 邓宏彬 | Four-axis eight-paddle mounting aircraft |
-
2018
- 2018-05-26 CN CN201820807056.1U patent/CN208360492U/en not_active Expired - Fee Related
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110963030A (en) * | 2019-12-03 | 2020-04-07 | 徐州飞梦电子科技有限公司 | Unmanned aerial vehicle and using method thereof |
| CN112954092A (en) * | 2021-02-03 | 2021-06-11 | 维沃移动通信有限公司 | Electronic device |
| CN112954092B (en) * | 2021-02-03 | 2023-07-18 | 维沃移动通信有限公司 | Electronic equipment |
| CN114476037A (en) * | 2021-12-30 | 2022-05-13 | 邓宏彬 | Four-axis eight-paddle mounting aircraft |
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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 | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20190111 Termination date: 20190526 |