CN110217387A - A kind of unmanned plane equipped with overboard safeguard structure - Google Patents
A kind of unmanned plane equipped with overboard safeguard structure Download PDFInfo
- Publication number
- CN110217387A CN110217387A CN201910516958.9A CN201910516958A CN110217387A CN 110217387 A CN110217387 A CN 110217387A CN 201910516958 A CN201910516958 A CN 201910516958A CN 110217387 A CN110217387 A CN 110217387A
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- overboard
- safeguard structure
- driving mechanism
- driving
- unmanned plane
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- 230000007246 mechanism Effects 0.000 claims abstract description 40
- 238000004891 communication Methods 0.000 claims abstract description 14
- 238000007789 sealing Methods 0.000 claims description 56
- 230000017525 heat dissipation Effects 0.000 claims description 10
- 230000005611 electricity Effects 0.000 claims description 3
- 238000003780 insertion Methods 0.000 claims description 2
- 230000037431 insertion Effects 0.000 claims description 2
- 238000000034 method Methods 0.000 abstract description 5
- 230000009467 reduction Effects 0.000 description 6
- 210000004262 dental pulp cavity Anatomy 0.000 description 3
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 description 2
- 230000009471 action Effects 0.000 description 2
- 238000005452 bending Methods 0.000 description 2
- 230000007423 decrease Effects 0.000 description 2
- 238000009434 installation Methods 0.000 description 2
- 239000007787 solid Substances 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000008901 benefit Effects 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000008450 motivation Effects 0.000 description 1
- 230000002093 peripheral effect Effects 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/08—Helicopters with two or more rotors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D45/00—Aircraft indicators or protectors not otherwise provided for
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
-
- G—PHYSICS
- G08—SIGNALLING
- G08C—TRANSMISSION SYSTEMS FOR MEASURED VALUES, CONTROL OR SIMILAR SIGNALS
- G08C17/00—Arrangements for transmitting signals characterised by the use of a wireless electrical link
- G08C17/02—Arrangements for transmitting signals characterised by the use of a wireless electrical link using a radio link
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02K—DYNAMO-ELECTRIC MACHINES
- H02K5/00—Casings; Enclosures; Supports
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02K—DYNAMO-ELECTRIC MACHINES
- H02K9/00—Arrangements for cooling or ventilating
- H02K9/02—Arrangements for cooling or ventilating by ambient air flowing through the machine
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Power Engineering (AREA)
- Mechanical Engineering (AREA)
- Computer Networks & Wireless Communication (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Remote Sensing (AREA)
- Power-Operated Mechanisms For Wings (AREA)
- Toys (AREA)
Abstract
The present invention provides a kind of unmanned plane equipped with overboard safeguard structure, more particularly to air vehicle technique field, including drone body, drone body includes body shell, overboard safeguard structure and control system, the lateral wall of body shell is equipped with several rotors, overboard safeguard structure includes the first driving mechanism and window cover board, control system includes control circuit board, controller is provided in control circuit board, driving circuit and wireless communication module, controller is electrically connected with driving circuit and wireless communication module respectively, controller controls the work of the first driving mechanism by driving circuit；First driving mechanism and control system are set in body shell, and the side wall of body shell is equipped with drives window cover board for linear motion so that thermal window turns on or off with the matched thermal window of window cover board, the first driving mechanism.The present invention can close in time thermovent progress waterproof operation by remotely controlling before overboard.
Description
Technical field
The invention belongs to air vehicle technique fields, and in particular to a kind of unmanned plane equipped with overboard safeguard structure.
Background technique
Currently, existing unmanned plane does not have waterproof construction substantially, if directly set unmanned plane progress waterproof sealing
If setting, then inevitable, there are heat dissipation problems again.
Therefore, being badly in need of one kind can guarantee that proper heat reduction is capable of the unmanned plane equipped with overboard safeguard structure of waterproof again.
Summary of the invention
The object of the present invention is to provide a kind of unmanned plane equipped with overboard safeguard structure, the overboard safeguard structure of setting and control
System processed closes thermovent progress waterproof operation by remotely controlling before overboard in time.
The present invention provides the following technical solutions:
A kind of unmanned plane equipped with overboard safeguard structure, including drone body, the drone body include body shell, institute
The lateral wall for stating body shell is equipped with several rotors, further includes overboard safeguard structure and control system, the overboard safeguard structure
Including the first driving mechanism and window cover board, the control system includes control circuit board, is provided in the control circuit board
Controller, driving circuit and wireless communication module, the controller respectively with the driving circuit and the wireless communication
Module electrical connection, the driving circuit are electrically connected with first driving mechanism, and the controller passes through the driving circuit control
Make the first driving mechanism work；First driving mechanism and the control system are set in the body shell, institute
The side wall for stating body shell, which is equipped with, drives the window with the matched thermal window of window cover board, first driving mechanism
Cover board is for linear motion so that the thermal window turns on or off.It is driven equipped with thermal window, window cover board and first
Motivation structure can realize thermal window heat dissipation when operating normally, and can be long-range by control system in emergency shutdown
It controls the first driving mechanism work lid and closes thermal window, realize waterproof sealing.
Preferably, the overboard safeguard structure further includes sealing baffle and the second driving mechanism, and the rotor includes cantilever,
The end of the cantilever is equipped with motor mount, is equipped with rotor motor on the motor mount, on the motor mount
Equipped with heat release hole and horizontal slot, the heat release hole vertically runs through the horizontal slot；It is equipped in each cantilever described
Sealing baffle and second driving mechanism, the sealing baffle is for closing the heat release hole, second driving
Mechanism drives the sealing baffle horizontal reciprocating movement to insertion or leaves the horizontal slot.Heat release hole is set, to rotor
The heat that motor generates radiates, and can be realized and be dissipated when operating normally using the driving sealing baffle movement of the second driving mechanism
Proper heat reduction at hot hole, and heat release hole can be closed rapidly in emergency shutdown, realize waterproof sealing.
Preferably, the motor mount includes end part seal plate, upper mounted plate and bottom plate, fixed plate
It is arranged in parallel on the end part seal plate with the bottom plate, the end part seal plate plugging type is mounted on the cantilever
On open-ended, the groove for installing the rotor motor top is equipped on the downside of fixed plate, described
It is equipped with axis hole at the center of groove, rotating shaft sealing circle is equipped in the axis hole, is equipped on the bottom plate for installing
The heat release hole of the rotor motor lower part is equipped with the horizontal slot, the sealing baffle energy on the bottom plate
The horizontal slot is enough inserted into or left through the end part seal plate.Rotor motor only has upper and lower part to be separately mounted to
On upper mounted plate and bottom plate, and middle part is exposed outside, is conducive to the heat dissipation of rotor motor.
Preferably, guard seal is equipped on the inner wall of side channel up and down of the horizontal slot and at the heat release hole
Circle；When the sealing baffle closes the heat release hole, the sealing baffle is clamped in two guard seals of upper and lower sides
Between circle.It can be realized the waterproof sealing at sealing baffle and heat release hole using guard seal circle.
Preferably, first driving mechanism includes driving motor and driving screw rod, on the output shaft of the driving motor
The driving screw rod is vertically installed, screw thread is equipped with drive seat on the driving screw rod, and the drive seat is equipped with several oblique
Strut, the hound pass through the thermal window and connect the window cover board.This is a kind of specific first driving mechanism
Structure, the form that motor, gear and rack gear also can be used drive window cover board for linear motion.
Preferably, the control circuit board is mounted in the body shell by mounting post, and the driving screw rod is vertical
Through the control circuit board, the control circuit board is equipped with guide rod, and the drive seat is equipped with pilot hole, the guiding
The bar formula of sliding vertically is inserted into the pilot hole.When driving motor and body shell loosen, it may tilt, drive spiral shell
Bar may tilt, and guiding role is played in the setting of guide rod, further ensure that driving screw rod vertical motion.
Preferably, second driving mechanism includes fixed supporting seat, pressure spring and drawstring, and the fixed supporting seat fixation is set
It sets on the inner wall of the cantilever, the both ends of the pressure spring are separately connected the fixed supporting seat and the sealing baffle, are pacifying
The side-walls for filling the body shell of the cantilever are equipped with a cable-through hole, and one end of the drawstring and the sealing baffle are solid
Fixed connection, the other end pass through the cable-through hole and are connected in the drive seat.Utilize drive seat, drawstring, fixed supporting seat, pressure spring
And the cooperation of sealing baffle, the proper heat reduction at heat release hole, and the energy in emergency shutdown can be realized when operating normally
Enough closing heat release holes rapidly, realize waterproof sealing.Second driving mechanism can be identical with the first driving mechanism, that is, each
Independent driving mechanism is installed respectively in cantilever, is driven in contrast, the setting of pressure spring, drawstring is utilized in the first driving mechanism
Motor reduces the weight of entire drone body as power source, simultaneously because the reduction of the number of power source decrease it is scattered
Heat, while controller control is got up conveniently.
Preferably, the number of the cantilever is four, sets that there are four pulley, the pulley and institutes in the control circuit board
Drawstring one-to-one correspondence is stated, a drawstring is turned by a pulley back into the cantilever.It can be real using pulley
Existing drawstring turns at pulley, so that parallel with cantilever axis enter in cantilever afterwards, oblique pull is avoided to cause drawstring friction damage.
Preferably, one end of the drawstring is fixed on the sealing after sequentially passing through the fixed supporting seat and the pressure spring
On the side of baffle.The end of drawstring can be limited using through installation, prevent oblique pull from causing sealing baffle bending damage
It is bad.
Preferably, the thermal window and the window cover board are circle, and the circumferential edges of the window cover board surround
It is provided with waterproof grommet, when the window cover plate lid is closed on the thermal window, the waterproof grommet is clamped in institute
It states between the circumferential edges of window cover board and the edge of the thermal window.It can be realized scuttle edges of boards using waterproof grommet
The sealing performance of edge.
The beneficial effects of the present invention are:
1. being equipped with thermal window, window cover board and the first driving mechanism, thermal window heat dissipation can be realized when operating normally, and
The first driving mechanism work lid can remotely be controlled by control system again in emergency shutdown and close thermal window, realize anti-watertight
Envelope.
2. heat release hole is arranged, the heat generated to rotor motor radiates, and drives sealing gear using the second driving mechanism
Plate movement can realize the proper heat reduction at heat release hole when operating normally, and can close heat dissipation rapidly in emergency shutdown
Waterproof sealing is realized in hole.
3. driving motor is utilized in the first driving mechanism as power source in the setting of pressure spring, drawstring, reduce it is entire nobody
The weight of machine ontology, simultaneously because the reduction of the number of power source decreases heat dissipation capacity, while controller control is got up conveniently.
4. can be realized drawstring at pulley using pulley to turn to, so that parallel with cantilever axis enter in cantilever afterwards, keep away
Exempt from oblique pull and causes drawstring friction damage.
Detailed description of the invention
Attached drawing is used to provide further understanding of the present invention, and constitutes part of specification, with reality of the invention
It applies example to be used to explain the present invention together, not be construed as limiting the invention.In the accompanying drawings:
Fig. 1 is longitudinal profile structure schematic of the invention；
Fig. 2 is vertical view schematic cross-sectional view of the invention；
Fig. 3 is electrical block diagram of the invention.
Wherein in the figure, it is marked as 1, body shell；2, cantilever；3, mounting post；4, control circuit board；5, driving motor；6,
Drive screw rod；7, thermal window；8, window cover board；9, guide rod；10, drawstring；11, drive seat；12, hound；13, anti-watertight
Seal；14, pulley；15, cable-through hole；16, fixed supporting seat；17, sealing baffle；18, pressure spring；19, upper mounted plate；20, end
Sealing plate；21, rotor motor；22, bottom plate；23, rotating shaft sealing circle；24, horizontal slot.
Specific embodiment
As shown in Figure 1-3, a kind of unmanned plane equipped with overboard safeguard structure, including drone body, drone body packet
Include body shell 1, overboard safeguard structure and control system, overboard safeguard structure includes the first driving mechanism, window cover board 8, close
Block plate 17 and the second driving mechanism, the first driving mechanism include driving motor 5 and driving screw rod 6, and the second driving mechanism includes
Fixed supporting seat 16, pressure spring 18 and drawstring 10, the lateral wall of body shell 1 are set there are four rotor, and a rotor includes one outstanding
Arm 2, control system include control circuit board 4, and controller, driving circuit and radio communication mold are provided in control circuit board 4
Block, the specific location and connection relationship of each structure are as follows:
Driving motor 5 and control circuit board 4 are equipped in body shell 1, wherein control circuit board 4 is mounted on machine by mounting post 3
In body shell 1, driving screw rod 6 is vertically installed on the output shaft of driving motor 5, and drives screw rod 6 vertically through control electricity
Road plate 4, screw thread is equipped with drive seat 11 on driving screw rod 6, and pilot hole is equipped in drive seat 11, in control circuit board 4
On be vertically provided with the guide rod 9 that slidingtype is inserted into pilot hole；Circular thermal window is equipped at the top of body shell 1
7, it is externally provided with the circular window cover board 8 that can cover conjunction with it in thermal window 7, two are equipped on the downside of window cover board 8
Root hound 12, the lower end of two hounds 12 are fixedly mounted in drive seat 11, that is, window cover board 8 is oblique by two
Strut 12 is fixed in drive seat 11；The lateral wall of body shell 1 is equipped with the cantilever 2 of four root canal shapes, and the end of cantilever 2 is equipped with electricity
Machine mounting base, motor mount include end part seal plate 20, upper mounted plate 19 and bottom plate 22, upper mounted plate 19 and lower solid
Fixed board 22 is arranged in parallel on end part seal plate 20, and 20 plugging type of end part seal plate is mounted on the end nozzle of cantilever 2 (namely
Block its opening) on, the circular groove for installing 21 top of rotor motor is equipped on the downside of upper mounted plate 19,
It is equipped with circular axis hole at the center of groove, rotating shaft sealing circle 23 is equipped in axis hole, is equipped on bottom plate 22 for pacifying
The heat release hole for filling 21 lower part of rotor motor is equipped with horizontal slot 24 on bottom plate 22, and heat release hole vertically runs through horizontal slot
24；Fixed supporting seat 16 is fixed on the inner wall of cantilever 2, and a fixed support is equipped in the cantilever 2 of four root canal shapes
Seat 16, pressure springs 18 and baffle sealing together 17, pressure spring 18 be resiliently supported at fixed supporting seat 16 and sealing baffle 17 it
Between namely pressure spring 18 both ends connect respectively with fixed supporting seat 16 and sealing baffle 17 and sealing baffle 17 be it is movable,
Sealing baffle 17 can under the action of the second driving mechanism it is horizontal through end part seal plate 20 and be inserted into horizontal slot 24 from
And reaches and closed purpose is carried out to heat release hole；One is equipped on body shell 1 and positioned at the installed position of four cantilevers 2
A cable-through hole 15, is equipped with four drawstrings 10 in drive seat 11, and one end of four drawstrings 10 is connected to the outstanding of four root canal shapes
On sealing baffle 17 in arm 2, the connection cables of drawstring 10 and rotor motor 21 can be easily installed using cable-through hole 15；Control
Device processed is electrically connected with driving circuit and wireless communication module respectively；Driving circuit is electrically connected with driving motor 5, and controller passes through
Driving circuit controls 5 positive and negative rotation of driving motor rotation, so that driving motor 5 works normally.
Specifically, the circumferential edges in window cover board 8 close rear defence around waterproof grommet 13, the lid of window cover board 8 is provided with
Waterstop ring 13 is clamped between the circumferential edges of window cover board 8 and the window edge of thermal window 7.Utilize waterproof grommet 13
It can be realized the sealing performance at 8 edge of window cover board.
Specifically, being equipped with guard seal circle on the inner wall of side channel up and down of horizontal slot 24 and at heat release hole；It is close
When block plate 17 closes heat release hole, sealing baffle 17 is clamped between two guard seal circles of upper and lower sides.Utilize guard seal
Circle can be realized the waterproof sealing at sealing baffle 17 and heat release hole.
Specifically, setting in control circuit board 4, there are four pulleys 14, after four drawstrings 10 are turned to by four pulleys 14 respectively
Into in four cantilevers 2.It can be realized drawstring 10 at pulley 14 using pulley 14 to turn to, thus after parallel with 2 axis of cantilever
Into in cantilever 2, oblique pull is avoided to cause 10 friction damage of drawstring.
Specifically, the end of drawstring 10 sequentially passes through the side for being fixed on sealing baffle 17 after fixed supporting seat 16 and pressure spring 18
Bian Shang.The end of drawstring 10 can be limited using through installation, prevent oblique pull from causing the bending damage of sealing baffle 17.
In the present embodiment, the control module that controller uses existing single-chip computer and its peripheral circuit to constitute, such as 51
Single-chip microcontroller can satisfy the transmitting-receiving control of signal；Wireless communication module can use existing ZigBee radio communication mold
Block or 4G communication module can be realized remote radio communication, and driving motor 5 uses existing stepper motor, can
Positive and negative rotation operation is realized as needed, and driving circuit uses existing stepper drive circuit, can be under controller control action
Realize the positive and negative rotation operation of driving motor 5.
Application method
The unmanned plane of the present embodiment is remotely controlled by flight control staff, when taking off, is sent out by remote controler to wireless communication module
Unlatching control command is sent, controller controls driving motor 5 by driving circuit and rotates forward after receiving unlatching control command, by
Driving screw rod 6 drives drive seat 11 to move up, to be propped up the window cover board 8 of top by two hounds 12, so that machine
Body shell 1 is effectively radiated by thermal window 7；While drive seat 11 moves up, the pulling of You Sigen drawstring 10 four is close
Block plate 17 is moved into the cantilever 2 of tubulose, so that the heat release hole on bottom plate 22 is opened, thus to 21 lower part of rotor motor
Heat release hole at effectively radiated.It is damaged in unmanned plane operation error, rotor motor 21 or external force (such as blast etc.) will
When landing, if lower section is the water surface, flight control staff can promptly be sent to wireless communication module by remote controler and be closed
Control command, controller control driving motor 5 by driving circuit and invert, by driving spiral shell after receiving closing control command
Bar 6 drives drive seat 11 to move down, to be pulled down the window cover board 8 of top by two hounds 12, so that thermal window 7
Place is closed, thus realize waterproof, meanwhile, while drive seat 11 moves down, four drawstrings 10 discharge pulling force, by four
Pressure spring 18 pushes sealing baffle 17 to move into horizontal slot 24, so that the heat release hole on bottom plate 22 is closed in time, from
And to effectively being sealed at the heat release hole of 21 lower part of rotor motor, to realize waterproof.Implementation of the invention needs the behaviour that flies
Control person is prejudged, to close sealing in time before unmanned plane is overboard.
Advantage
It, can be just using the cooperation of driving screw rod 6, drive seat 11, two hounds 12, thermal window 7 and window cover board 8
The heat dissipation of thermal window 7 is often realized when operation, and can be realized waterproof sealing in emergency shutdown；Using drive seat 11, draw
The cooperation of rope 10, fixed supporting seat 16, pressure spring 18 and sealing baffle 17 can be realized at heat release hole just when operating normally
Often heat dissipation, and heat release hole can be closed rapidly in emergency shutdown, realize waterproof sealing.
The foregoing is only a preferred embodiment of the present invention, but scope of protection of the present invention is not limited thereto,
Anyone skilled in the art in the technical scope disclosed by the present invention, according to the technique and scheme of the present invention and its
Inventive concept is subject to equivalent substitution or change, should be covered by the protection scope of the present invention.
Claims (10)
1. a kind of unmanned plane equipped with overboard safeguard structure, including drone body, the drone body include body shell,
The lateral wall of the body shell is equipped with several rotors, which is characterized in that and it further include overboard safeguard structure and control system, it is described
Overboard safeguard structure includes the first driving mechanism and window cover board, and the control system includes control circuit board, the control electricity
Be provided with controller, driving circuit and wireless communication module on the plate of road, the controller respectively with the driving circuit and
The wireless communication module electrical connection, the driving circuit are electrically connected with first driving mechanism, and the controller passes through institute
It states driving circuit and controls the first driving mechanism work；First driving mechanism and the control system are set to the machine
In body shell, the side wall of the body shell is equipped with and the matched thermal window of window cover board, first driving mechanism
Drive the window cover board is for linear motion so that the thermal window turns on or off.
2. the unmanned plane according to claim 1 equipped with overboard safeguard structure, which is characterized in that the overboard safeguard structure
It further include sealing baffle and the second driving mechanism, the rotor includes cantilever, and the end of the cantilever is equipped with motor mount, institute
It states and rotor motor is installed on motor mount, the motor mount is equipped with heat release hole and horizontal slot, the heat release hole
Vertically run through the horizontal slot；The sealing baffle and second driving mechanism are equipped in each cantilever, it is described
For sealing baffle for closing to the heat release hole, second driving mechanism drives the sealing baffle horizontal reciprocating movement
To insertion or leave the horizontal slot.
3. the unmanned plane according to claim 2 equipped with overboard safeguard structure, which is characterized in that the motor mount packet
End part seal plate, upper mounted plate and bottom plate are included, fixed plate and the bottom plate are arranged in parallel in the end
On portion's sealing plate, the end part seal plate plugging type be mounted on the cantilever it is open-ended on, under fixed plate
Side is equipped with the groove for installing the rotor motor top, axis hole is equipped at the center of the groove, in the axis
It is equipped with rotating shaft sealing circle in hole, the heat release hole for installing the rotor motor lower part is equipped on the bottom plate,
On the bottom plate be equipped with the horizontal slot, the sealing baffle can through the end part seal plate be inserted into or from
Open the horizontal slot.
4. the unmanned plane according to claim 2 or 3 equipped with overboard safeguard structure, which is characterized in that described horizontal slotting
Guard seal circle is equipped on the inner wall of side channel up and down of slot and at the heat release hole；It is dissipated when sealing baffle closing is described
When hot hole, the sealing baffle is clamped between two guard seal circles of upper and lower sides.
5. the unmanned plane according to claim 2 or 3 equipped with overboard safeguard structure, which is characterized in that first driving
Mechanism includes driving motor and driving screw rod, is vertically equipped with the driving screw rod on the output shaft of the driving motor, described
Screw thread is equipped with drive seat on driving screw rod, and the drive seat is equipped with several hounds, and the hound passes through the heat dissipation
Window connects the window cover board.
6. the unmanned plane according to claim 5 equipped with overboard safeguard structure, which is characterized in that the control circuit board is logical
It crosses mounting post to be mounted in the body shell, the driving screw rod vertically runs through the control circuit board, the control circuit
Plate is equipped with guide rod, and the drive seat is equipped with pilot hole, and the guide rod formula of sliding vertically is inserted into the pilot hole.
7. the unmanned plane according to claim 6 equipped with overboard safeguard structure, which is characterized in that second driving mechanism
Including fixed supporting seat, pressure spring and drawstring, the fixed supporting seat is fixed on the inner wall of the cantilever, the pressure spring
Both ends are separately connected the fixed supporting seat and the sealing baffle, in the side-walls for the body shell for installing the cantilever
Equipped with a cable-through hole, one end of the drawstring is fixedly connected with the sealing baffle, and the other end is connected across the cable-through hole
In the drive seat.
8. the unmanned plane according to claim 7 equipped with overboard safeguard structure, which is characterized in that the number of the cantilever is
It four, sets in the control circuit board there are four pulley, the pulley and the drawstring correspond, and a drawstring is by one
A pulley turns back into the cantilever.
9. the unmanned plane according to claim 7 or 8 equipped with overboard safeguard structure, which is characterized in that the one of the drawstring
End is fixed on the side of the sealing baffle after sequentially passing through the fixed supporting seat and the pressure spring.
10. the unmanned plane according to claim 1 equipped with overboard safeguard structure, which is characterized in that the thermal window and
The window cover board is circle, and the circumferential edges of the window cover board are around waterproof grommet is provided with, when the scuttle
Plate lid close when on the thermal window, the waterproof grommet be clamped in the window cover board circumferential edges and the heat dissipation
Between the edge of window.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910516958.9A CN110217387B (en) | 2019-06-14 | 2019-06-14 | Unmanned aerial vehicle with falling water protection architecture |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910516958.9A CN110217387B (en) | 2019-06-14 | 2019-06-14 | Unmanned aerial vehicle with falling water protection architecture |
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| CN110217387A true CN110217387A (en) | 2019-09-10 |
| CN110217387B CN110217387B (en) | 2024-01-23 |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114802076A (en) * | 2022-05-18 | 2022-07-29 | 岚图汽车科技有限公司 | Vehicle water falling monitoring sealing protection device and vehicle |
Citations (19)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE4129384A1 (en) * | 1991-09-04 | 1993-03-11 | Deutsche Aerospace | TRANSPORT CONTAINER |
| JP2007006394A (en) * | 2005-06-27 | 2007-01-11 | Fujitsu Ltd | Heat dissipation structure of imaging apparatus |
| CN105775133A (en) * | 2016-03-03 | 2016-07-20 | 致导科技（北京）有限公司 | Waterproof unmanned aerial vehicle |
| KR101663058B1 (en) * | 2016-04-04 | 2016-10-17 | 만진항공건설 주식회사 | Unmanned aerial vehicle for agriculture |
| CN206149689U (en) * | 2016-08-31 | 2017-05-03 | 零度智控（北京）智能科技有限公司 | Unmanned aerial vehicle heat radiation structure and unmanned aerial vehicle |
| CN206569246U (en) * | 2016-12-30 | 2017-10-20 | 易瓦特科技股份公司 | Unmanned plane with waterproof casing |
| CN206611700U (en) * | 2017-04-11 | 2017-11-03 | 北京航景创新科技有限公司 | A kind of radiating proof mechanism of water for electricity tune in plant protection unmanned plane closed shell |
| US20170327222A1 (en) * | 2015-07-31 | 2017-11-16 | Guangzhou Xaircraft Technology Co., Ltd. | Unmanned aerial vehicle and unmanned aerial vehicle body configured for unmanned aerial vehicle |
| CN206968986U (en) * | 2017-06-13 | 2018-02-06 | 张万民 | The multiaxis rotary wind type unmanned plane and fire-extinguishing of rainwater-proof thermal radiation resistant |
| JP2018027719A (en) * | 2016-08-15 | 2018-02-22 | 株式会社菊池製作所 | Rotary vane type unmanned aircraft and radiation dose measurement system |
| CN207106876U (en) * | 2017-07-27 | 2018-03-16 | 河南大域航空科技有限公司 | A kind of rain-proof unmanned plane |
| CN207242027U (en) * | 2017-10-16 | 2018-04-17 | 郑州中核岩土工程有限公司 | Detecting aerial survey unmanned plane |
| CN108341045A (en) * | 2018-03-29 | 2018-07-31 | 南京工业职业技术学院 | Unmanned plane falling protecting device |
| CN108454840A (en) * | 2018-04-03 | 2018-08-28 | 南通科技职业学院 | A kind of unmanned plane of wing waterproof |
| CN108725769A (en) * | 2017-04-19 | 2018-11-02 | 深圳市道通智能航空技术有限公司 | A kind of motor radiating part, motor and aircraft |
| CN109643928A (en) * | 2016-08-22 | 2019-04-16 | Lg伊诺特有限公司 | Motor for unmanned plane and the unmanned plane including the motor |
| CN208868291U (en) * | 2018-07-11 | 2019-05-17 | 深圳市道通智能航空技术有限公司 | Waterproof unmanned plane |
| CN208963304U (en) * | 2018-09-07 | 2019-06-11 | 广州市海高电子科技有限公司 | A kind of unmanned plane with water-proof function |
| CN210852901U (en) * | 2019-06-14 | 2020-06-26 | 南京工业职业技术学院 | Unmanned aerial vehicle with protective structure falls into water |
-
2019
- 2019-06-14 CN CN201910516958.9A patent/CN110217387B/en active Active
Patent Citations (19)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE4129384A1 (en) * | 1991-09-04 | 1993-03-11 | Deutsche Aerospace | TRANSPORT CONTAINER |
| JP2007006394A (en) * | 2005-06-27 | 2007-01-11 | Fujitsu Ltd | Heat dissipation structure of imaging apparatus |
| US20170327222A1 (en) * | 2015-07-31 | 2017-11-16 | Guangzhou Xaircraft Technology Co., Ltd. | Unmanned aerial vehicle and unmanned aerial vehicle body configured for unmanned aerial vehicle |
| CN105775133A (en) * | 2016-03-03 | 2016-07-20 | 致导科技（北京）有限公司 | Waterproof unmanned aerial vehicle |
| KR101663058B1 (en) * | 2016-04-04 | 2016-10-17 | 만진항공건설 주식회사 | Unmanned aerial vehicle for agriculture |
| JP2018027719A (en) * | 2016-08-15 | 2018-02-22 | 株式会社菊池製作所 | Rotary vane type unmanned aircraft and radiation dose measurement system |
| CN109643928A (en) * | 2016-08-22 | 2019-04-16 | Lg伊诺特有限公司 | Motor for unmanned plane and the unmanned plane including the motor |
| CN206149689U (en) * | 2016-08-31 | 2017-05-03 | 零度智控（北京）智能科技有限公司 | Unmanned aerial vehicle heat radiation structure and unmanned aerial vehicle |
| CN206569246U (en) * | 2016-12-30 | 2017-10-20 | 易瓦特科技股份公司 | Unmanned plane with waterproof casing |
| CN206611700U (en) * | 2017-04-11 | 2017-11-03 | 北京航景创新科技有限公司 | A kind of radiating proof mechanism of water for electricity tune in plant protection unmanned plane closed shell |
| CN108725769A (en) * | 2017-04-19 | 2018-11-02 | 深圳市道通智能航空技术有限公司 | A kind of motor radiating part, motor and aircraft |
| CN206968986U (en) * | 2017-06-13 | 2018-02-06 | 张万民 | The multiaxis rotary wind type unmanned plane and fire-extinguishing of rainwater-proof thermal radiation resistant |
| CN207106876U (en) * | 2017-07-27 | 2018-03-16 | 河南大域航空科技有限公司 | A kind of rain-proof unmanned plane |
| CN207242027U (en) * | 2017-10-16 | 2018-04-17 | 郑州中核岩土工程有限公司 | Detecting aerial survey unmanned plane |
| CN108341045A (en) * | 2018-03-29 | 2018-07-31 | 南京工业职业技术学院 | Unmanned plane falling protecting device |
| CN108454840A (en) * | 2018-04-03 | 2018-08-28 | 南通科技职业学院 | A kind of unmanned plane of wing waterproof |
| CN208868291U (en) * | 2018-07-11 | 2019-05-17 | 深圳市道通智能航空技术有限公司 | Waterproof unmanned plane |
| CN208963304U (en) * | 2018-09-07 | 2019-06-11 | 广州市海高电子科技有限公司 | A kind of unmanned plane with water-proof function |
| CN210852901U (en) * | 2019-06-14 | 2020-06-26 | 南京工业职业技术学院 | Unmanned aerial vehicle with protective structure falls into water |
Non-Patent Citations (1)
| Title |
|---|
| 胡彩旗;邵明赫;王存鹏;陈大伟;兰玉彬;王正田: "多旋翼喷雾无人飞行器的设计和试验研究", 农机化研究, no. 3, pages 118 - 123 * |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114802076A (en) * | 2022-05-18 | 2022-07-29 | 岚图汽车科技有限公司 | Vehicle water falling monitoring sealing protection device and vehicle |
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