CN105966602A - Novel unmanned aerial vehicle - Google Patents
Novel unmanned aerial vehicle Download PDFInfo
- Publication number
- CN105966602A CN105966602A CN201610339028.7A CN201610339028A CN105966602A CN 105966602 A CN105966602 A CN 105966602A CN 201610339028 A CN201610339028 A CN 201610339028A CN 105966602 A CN105966602 A CN 105966602A
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- Prior art keywords
- supporting seat
- frame
- unmanned plane
- undercarriage
- storage box
- Prior art date
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- 239000000463 material Substances 0.000 claims description 10
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- 210000001215 vagina Anatomy 0.000 claims 1
- 230000000694 effects Effects 0.000 abstract description 9
- 238000010521 absorption reaction Methods 0.000 abstract 4
- 230000035939 shock Effects 0.000 abstract 4
- 230000033001 locomotion Effects 0.000 description 13
- 238000012544 monitoring process Methods 0.000 description 7
- 230000007613 environmental effect Effects 0.000 description 4
- 238000009434 installation Methods 0.000 description 4
- 230000001681 protective effect Effects 0.000 description 3
- 230000005611 electricity Effects 0.000 description 2
- 238000007689 inspection Methods 0.000 description 2
- 230000000630 rising effect Effects 0.000 description 2
- 241000607479 Yersinia pestis Species 0.000 description 1
- 230000007123 defense Effects 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000011161 development Methods 0.000 description 1
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- 208000037265 diseases, disorders, signs and symptoms Diseases 0.000 description 1
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- 229910052500 inorganic mineral Inorganic materials 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000013507 mapping Methods 0.000 description 1
- 239000011707 mineral Substances 0.000 description 1
- 230000000116 mitigating effect Effects 0.000 description 1
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/02—Undercarriages
- B64C25/04—Arrangement or disposition on aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/02—Undercarriages
- B64C25/08—Undercarriages non-fixed, e.g. jettisonable
- B64C25/10—Undercarriages non-fixed, e.g. jettisonable retractable, foldable, or the like
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/02—Undercarriages
- B64C25/08—Undercarriages non-fixed, e.g. jettisonable
- B64C25/10—Undercarriages non-fixed, e.g. jettisonable retractable, foldable, or the like
- B64C25/12—Undercarriages non-fixed, e.g. jettisonable retractable, foldable, or the like sideways
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/02—Undercarriages
- B64C25/08—Undercarriages non-fixed, e.g. jettisonable
- B64C25/10—Undercarriages non-fixed, e.g. jettisonable retractable, foldable, or the like
- B64C25/18—Operating mechanisms
- B64C25/24—Operating mechanisms electric
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface
- B64C25/58—Arrangements or adaptations of shock-absorbers or springs
- B64C25/62—Spring shock-absorbers; Springs
-
- 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
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U70/00—Launching, take-off or landing arrangements
- B64U70/60—Take-off or landing of UAVs from a runway using their own power
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface
- B64C2025/325—Alighting gear characterised by elements which contact the ground or similar surface specially adapted for helicopters
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Remote Sensing (AREA)
- Operating, Guiding And Securing Of Roll- Type Closing Members (AREA)
- Power-Operated Mechanisms For Wings (AREA)
Abstract
The invention relates to a novel unmanned aerial vehicle, comprising a rack, a landing gear, motors, propellers and shock absorption bases. The landing gear is located at the center position right under the rack and connected with the rack, the number of each of the motors, the propellers and the shock absorption bases is six, the bottom ends of the motors are located on supports, the propellers are installed on the spindles of the motors, and the shock absorption bases are fixed under the supports. The novel unmanned aerial vehicle can be simultaneously applied to taking off and landing under the conditions of mountain areas or uneven grounds and flat grounds, and is high in applicability and good in shock absorption effect; the support devices are adopted, so that the height difference due to uneven sites is made up, the novel unmanned aerial vehicle can be landed stably on uneven sites, and the phenomenon that the unmanned aerial vehicle is broken or damaged caused by the fact that the unmanned aerial vehicle is crash-landed on mountain areas or uneven sites is avoided.
Description
Technical field
The present invention relates to unmanned plane field, a kind of novel unmanned plane.
Background technology
Aircraft be by the mankind manufacture, can fly away from ground, space flight and by people control in endoatmosphere or exoatmosphere
The apparatus flying object flown in space (space), aircraft is divided into airborne vehicle, spacecraft, rocket, guided missile and guided weapon；Nothing
Man-machine is also the one of aircraft, and unmanned plane is utilize that radio robot and the presetting apparatus provided for oneself handle the most manned
Aircraft, can be divided into depopulated helicopter, unmanned fixed-wing aircraft, unmanned multi-rotor aerocraft, unmanned airship from technical standpoint definition
With unmanned parasol etc.；Can be divided into military and civilian by application, military aspect unmanned plane is divided into reconnaissance plane and target drone；At present,
Unmanned plane can be widely applied to country's ecological environmental protection, aeroplane photography, mapping, mineral resources exploration, the condition of a disaster supervision, traffic
Patrol, power-line patrolling, security monitoring, emergent mitigation, emergency command, rain making, national defense safety, land resources exploration,
Town planning, seismic survey, environmental monitoring, forest fire protection, Crop Estimation, protection zone wild animal monitoring, air sampling,
Maritime affairs scout, border make an inspection tour, the prohibition of drug scouting, fire inspection, ecological environmental protection, marine environmental monitoring, land use survey,
Water resources development, crop growth monitoring and the yield by estimation, agricultural operation, Natural calamity monitoring and assessment, urban planning and municipal administration pipe
The fields such as the protection of reason, forest disease and pest and monitoring, digital city.
Many rotor wing unmanned aerial vehicles belong to the one in unmanned plane, and it is less than normal, popular relatively that many rotor wing unmanned aerial vehicles have compact conformation, build
By force, flexibly and the advantage such as flight stability is by extensively in civil and military in motion, and the most popular；But the most rotations
Wing unmanned plane is owing to being accomplished by landing after short flight certain time in cruising time, thus carries out battery altering, supplements the energy,
Also in that this reason causes unmanned plane to be restricted in the most many application, such as unmanned plane is concavo-convex in mountain area or place
Uneven place all cannot be carried out takeoff and landing, the most often occurs unmanned plane uneven because of forced landing to mountain area or place
Place cause unmanned plane to be broken or the phenomenon of breakage.In consideration of it, the invention provides a kind of novel unmanned plane.
Summary of the invention
In order to make up the deficiencies in the prior art, the invention provides a kind of novel unmanned plane.
The present invention to solve its technical problem and realize by the following technical solutions.
A kind of novel unmanned plane, including frame, undercarriage, motor, propeller and damping base；Described undercarriage is positioned at machine
Center position immediately below frame, and undercarriage is connected with frame, central rack structure in the form of annular discs, and central rack is along frame
Central axis uniformly offer fan-shaped material reducing mouth, outside frame, central axis along frame is respectively symmetrically and is provided with six supports,
Bar shaped material reducing mouth is offered, by arranging fan-shaped material reducing mouth and bar shaped material reducing mouth alleviates the weight of frame on support；Described electricity
The quantity of machine, propeller and damping base is six, and motor bottom is fixed on above support, and propeller is arranged on electric machine main shaft,
Damping base is fixed on below support.
Further, described undercarriage includes rise and fall plate, storage box, support means and closing device；The described plate side of being that rises and falls
Shape structure, limit, the plate left and right sides of rising and falling is symmetrically arranged with deck respectively, and the cross section of deck is in " Ω " type structure, card
Seat is for fixing between undercarriage and frame, and uses the deck of " Ω " type structure to be easy to the installation and removal of undercarriage；Institute
The storage box stated is fixed on and rises and falls on plate bottom face, and storage box is made up of housing and inside casing, and housing surrounds " the returning " connected with inside casing
Font stores groove, and inside casing space is for the installation of battery；Described support means quantity is four, and support means head and the tail are sequentially arranged
Surround, with inside casing, " returning " font connected at housing to store in groove；Described closing device quantity is two, closing device symmetry cloth
Put in storage box lower end.
Further, described damping base includes cushion socket and damping spring；The trapezoidal structure of described cushion socket, on cushion socket
End is provided with lead, and cushion socket lower end is provided with round bar, is provided with crosspiece in the middle part of cushion socket, and crosspiece is provided with lower guiding
Post, and upper lead and lower lead be located on the same line, damping spring two ends are rotating around being enclosed within upper lead and lower guiding
On post, when the present invention is when taking off in level land or lands, undercarriage can shrink need not, damping base has directly served as and has risen and fallen
The effect of frame, and damping base reduce the present invention landing land time vibrations, be effectively protected the present invention land landing time
Safety and stability.
Further, described support means includes electric rotating machine, motor cabinet, rotating shaft, bearing, electric pushrod, support bar, props up
Spike seat, shock-proof spring and sensor；Described electric rotating machine is arranged in storage box by motor cabinet, rotating shaft one end and rotation
Electric machine main shaft is attached, and the rotating shaft other end is arranged on storage box medial wall by bearing, in the middle part of electric pushrod upper end and rotating shaft
Being attached, electric pushrod lower end is attached with support bar one end, and the support bar other end is connected with supporting seat, shock-proof spring
Around being enclosed within support bar, sensor is arranged on supporting seat lateral wall, by the rotation rotating drive rotating shaft of electric rotating machine,
And fixing between rotating shaft with electric pushrod be connected, thus driving electric push rod rotates with rotating shaft for center of rotation, pushes away when electronic
When bar turns to vertical with storage box, the rotation of the motor that stops the rotation, start the stretching motion of electric pushrod, due to supporting seat
On sensor is installed, and sensor uses infrared ray sensor, and when electric pushrod touches ground, electric pushrod stops stretching
Long motion, in the present invention, support means quantity is four, when the present invention drops in the place of mountain area or ground relief
When falling to landing, different by the extended length of electric pushrod, thus compensate for the difference in height brought because place is uneven, make
The present invention can carry out stable landing on rough place, and reduce the present invention when landing by shock-proof spring
Jitter.
Further, described closing device includes cover plate, slide block, motorized rails and limited block；Before and after described cover plate, both sides are divided
Not being symmetrically installed with slide block, motorized rails is separately fixed at before and after storage box on lateral wall, and two ends, motorized rails left and right are respectively
Being fixed with limited block, slide block is arranged on motorized rails, by moving left and right of motorized rails band movable slider, thus drives cover plate
Movement, it is achieved that the folding effect of cover plate, closing device serves protective effect to support means.
Further, described supporting seat upper end is provided with sleeve, and sleeve inner is provided with female thread, and support bar lower end is provided with
External screw thread, for threadeding between support bar and the sleeve of supporting seat, supporting seat lower end is provided with a spike, and a spike
Circumferential direction along supporting seat is evenly arranged, and a spike is wedge structure.
When unmanned plane needs landing to land in the area of mountain area or ground relief in-flight, first start motorized rails,
By two lateral movement to the left and right of motorized rails band movable slider, thus drive cover plate two side shifting to the left and right, it is achieved that closing device
Open；Then electric rotating machine is started, by the rotation rotating drive rotating shaft of electric rotating machine, and between rotating shaft and electric pushrod
Fixing connection, thus driving electric push rod rotates with rotating shaft for center of rotation, when electric pushrod turns to vertical with storage box
Time, the rotation of the motor that stops the rotation, start the stretching motion of electric pushrod, owing to being provided with sensor on supporting seat, and pass
Sensor uses infrared ray sensor, when electric pushrod touches ground, and electric pushrod stopping stretching motion, in the present invention,
Support means quantity is four, when the present invention carries out landing landing in the place of mountain area or ground relief, is pushed away by electronic
The extended length of bar is different, thus compensate for the difference in height brought because place is uneven so that the present invention can concavo-convex not
Carry out stable landing on flat place, and reduce the present invention jitter when landing by shock-proof spring, it is to avoid unmanned plane
Because the rough place of forced landing to mountain area or place causes unmanned plane to be broken or the phenomenon of breakage；When unmanned plane lands
When supplementary good power source takes off, packing up support means, close closing device, closing device serves protection and makees support means
With, when unmanned plane lands on level land, undercarriage can shrink need not, damping base has directly served as the effect of undercarriage,
And damping base reduce the present invention landing land time vibrations, be effectively protected the present invention land land time safety and
Stability.
Compared with prior art, the invention have the advantages that
(1) takeoff and landing in the case of the present invention can be simultaneously suitable for mountain area or ground relief and level land, the suitability
Strong and good damping effect.
(2) present invention is by using support means to compensate for the difference in height brought because place is uneven so that the present invention can be
Stable landing is carried out, it is to avoid unmanned plane is because of the rough place of forced landing to mountain area or place on rough place
Unmanned plane is caused to be broken or the phenomenon of breakage.
Accompanying drawing explanation
The present invention is further described with embodiment below in conjunction with the accompanying drawings.
Fig. 1 is the perspective view of the present invention；
Fig. 2 is perspective view when frame of the present invention, motor, propeller and damping base cooperation；
Fig. 3 is the perspective view of undercarriage of the present invention；
Fig. 4 is the perspective view of undercarriage of the present invention (not including closing device)；
Fig. 5 is the upward view of undercarriage of the present invention (not including closing device)；
Fig. 6 is the perspective view of support means of the present invention；
Fig. 7 is the perspective view of damping runners of the present invention.
Detailed description of the invention
For the technological means making the present invention realize, creation characteristic, reach purpose and be easy to understand with effect, below in conjunction with tool
Body illustrates, and the present invention is expanded on further.
As it is shown in figure 1, a kind of novel unmanned plane, including frame 1, undercarriage 2, motor 3, propeller 4 and damping base 5；
Described undercarriage 2 is positioned at center position immediately below frame 1, and undercarriage 2 is connected with frame 1, in the middle part of frame 1 in
In the middle part of disc-shaped structure, and frame 1, the central axis along frame 1 uniformly offers fan-shaped material reducing mouth, along frame outside frame 1
The central axis of 1 is respectively symmetrically and is provided with six supports, and support offers bar shaped material reducing mouth, by arrange fan-shaped material reducing mouth and
Bar shaped material reducing mouth alleviates the weight of frame 1；The quantity of described motor 3, propeller 4 and damping base 5 is six, electricity
Machine 3 bottom is fixed on above support, and propeller 4 is arranged on motor 3 main shaft, and damping base 5 is fixed on below support.
As shown in Fig. 3 to Fig. 7, described undercarriage 2 includes rise and fall plate 21, storage box 22, support means 23 and folding dress
Put 24；The described plate 21 that rises and falls is square structure, and limit, plate 21 left and right sides of rising and falling is symmetrically arranged with deck, and card respectively
The cross section of seat is in " Ω " type structure, and deck is for fixing between undercarriage 2 and frame 1, and uses " Ω " type structure
Deck be easy to the installation and removal of undercarriage 21；Described storage box 22 is fixed on and rises and falls on plate 21 bottom face, storage box
22 are made up of housing and inside casing, and housing surrounds " returning " font connected and stores groove with inside casing, and inside casing space is for the installation of battery；
Described support means 23 quantity is four, and support means 23 head and the tail are sequentially arranged in housing and surround " returning " word connected with inside casing
Type stores in groove；Described closing device 24 quantity is two, and closing device 24 is arranged symmetrically in storage box 22 lower end.
As in figure 2 it is shown, described damping base 5 includes cushion socket 51 and damping spring 52；Described cushion socket 51 is trapezoidal
Structure, cushion socket 51 upper end is provided with lead, and cushion socket 51 lower end is provided with round bar, is provided with horizontal stroke in the middle part of cushion socket 51
Shelves, crosspiece are provided with lower lead, and upper lead and lower lead are located on the same line, and damping spring 52 two ends are divided
Not around being enclosed within upper lead and lower lead, when the present invention is when taking off in level land or lands, undercarriage 2 can shrink not
With, damping base 5 has directly served as the effect of undercarriage 2, and damping base 5 reduces the present invention shake when landing is landed
Dynamic, it is effectively protected the present invention and lands safety and stability when landing.
As shown in Fig. 3 to Fig. 7, described support means 23 includes electric rotating machine 231, motor cabinet 232, rotating shaft 233, axle
Hold 234, electric pushrod 235, support bar 236, supporting seat 237, shock-proof spring 238 and sensor 239；Described rotation
Rotating motor 231 is arranged in storage box 22 by motor cabinet 232, and rotating shaft 233 one end is attached with electric rotating machine 231 main shaft,
Rotating shaft 233 other end is arranged on storage box 22 medial wall by bearing 234, in the middle part of electric pushrod 235 upper end and rotating shaft 233
Being attached, electric pushrod 235 lower end is attached with support bar 236 one end, support bar 236 other end and supporting seat 237
Being connected, shock-proof spring 238 is around being enclosed within support bar 236, and sensor 239 is arranged on supporting seat 237 lateral wall, passes through
Electric rotating machine 231 rotate the rotation driving rotating shaft 233, and fixing between rotating shaft 233 with electric pushrod 235 be connected, thus
Driving electric push rod 235 rotates with rotating shaft 233 for center of rotation, when electric pushrod 235 turns to vertical with storage box 22
Time, the rotation of the motor 231 that stops the rotation, start the stretching motion of electric pushrod 235, owing to being provided with on supporting seat 237
Sensor 239, and sensor 239 uses infrared ray sensor, when electric pushrod 235 touches ground, electric pushrod 235
Stopping stretching motion, in the present invention, support means 23 quantity is four, when the present invention is in mountain area or the field of ground relief
When ground carries out landing landing, the extended length by electric pushrod 235 is different, thus compensate for bringing because place is uneven
Difference in height so that the present invention can carry out stable landing on rough place, and is reduced by shock-proof spring 238
The present invention jitter when landing.
As it is shown on figure 3, described closing device 24 includes cover plate 241, slide block 242, motorized rails 243 and limited block 244；
Before described cover plate, both sides are respectively symmetrically and are provided with slide block 242, before motorized rails 243 is separately fixed at storage box 22 after 241
On rear lateral wall, and motorized rails about 241 is respectively fixed at two ends with limited block 244, and slide block 242 is arranged on motorized rails 243
On, by moving left and right of motorized rails 243 band movable slider 242, thus drive the movement of cover plate 241, it is achieved that cover plate 241
Folding effect, closing device 24 serves protective effect to support means 23.
As shown in Figure 6 and Figure 7, described supporting seat 237 upper end is provided with sleeve, and sleeve inner is provided with female thread,
Strut lower end is provided with external screw thread, for threadeding between support bar and the sleeve of supporting seat 237, and supporting seat 237 lower end
Being provided with spike, and a spike is evenly arranged along the circumferential direction of supporting seat 237, a spike is wedge structure.
When unmanned plane needs landing to land in the area of mountain area or ground relief in-flight, first start motorized rails
243, by two lateral movement to the left and right of motorized rails 243 band movable slider 242, thus drive cover plate 241 two side shifting to the left and right,
Achieve opening of closing device 24；Then start electric rotating machine 231, drive rotating shaft 233 by the rotation of electric rotating machine 231
Rotation, and fixing between rotating shaft 233 with electric pushrod 235 is connected, thus driving electric push rod 235 is with rotating shaft 233 for revolving
Turn center to rotate, when electric pushrod 235 turns to vertical with storage box 22, the rotation of the motor 231 that stops the rotation, open
The stretching motion of dynamic electric pushrod 235, owing to being provided with sensor 239 on supporting seat 237, and sensor 239 uses red
Outer line sensor, when electric pushrod 235 touches ground, electric pushrod 235 stops stretching motion, in the present invention,
Support arrangement 23 quantity is four, when the present invention carries out landing landing in the place of mountain area or ground relief, is pushed away by electronic
The extended length of bar 235 is different, thus compensate for the difference in height brought because place is uneven so that the present invention can be recessed
Carry out stable landing on the place of convex injustice, and reduce the present invention jitter when landing by shock-proof spring 238；Work as nothing
Man-machine landing has supplemented power source when taking off, and packs up support means 23, closes closing device 24, and closing device 24 is to support
Device 23 serves protective effect, when unmanned plane lands on level land, undercarriage 2 can shrink need not, damping base 5
Directly serve as the effect of undercarriage 2, and damping base 5 has reduced the present invention vibrations when landing is landed, and is effectively protected
The present invention is landed safety and stability when landing.
The ultimate principle of the present invention, principal character and advantage have more than been shown and described.Skilled person will appreciate that of the industry,
The present invention is not restricted to the described embodiments, the principle that the present invention is simply described of the description in above-described embodiment and description,
Without departing from the spirit and scope, the present invention also has various changes and modifications, and these changes and improvements both fall within
In scope of the claimed invention.Claimed scope is defined by appending claims and equivalent thereof.
Claims (4)
1. a novel unmanned plane, it is characterised in that: include frame, undercarriage, motor, propeller and damping base；Described
Undercarriage be positioned at center position immediately below frame, and undercarriage is connected with frame, central rack structure in the form of annular discs, and
Central rack uniformly offers fan-shaped material reducing mouth along the central axis of frame, and outside frame, central axis along frame is respectively symmetrically and sets
It is equipped with six supports, support offers bar shaped material reducing mouth；The quantity of described motor, propeller and damping base is six,
Motor bottom is fixed on above support, and propeller is arranged on electric machine main shaft, and damping base is fixed on below support；Wherein:
Described undercarriage includes rise and fall plate, storage box, support means and closing device；The described plate that rises and falls is square structure,
Rise and fall and be symmetrically arranged with deck respectively on limit, the plate left and right sides, and the cross section of deck is in " Ω " type structure；Described stores
Box is fixed on and rises and falls on plate bottom face, and storage box is made up of housing and inside casing, and housing surrounds " returning " font storage connected with inside casing
Put groove；Described support means quantity is four, and support means head and the tail are sequentially arranged in housing and surround " returning " word connected with inside casing
Type stores in groove；Described closing device quantity is two, and closing device is arranged symmetrically in storage box lower end；
Described damping base includes cushion socket and damping spring；The trapezoidal structure of described cushion socket, cushion socket upper end is provided with
Upper lead, cushion socket lower end is provided with round bar, is provided with crosspiece in the middle part of cushion socket, and crosspiece is provided with lower lead, and on
Lead and lower lead are located on the same line, and damping spring two ends are rotating around being enclosed within upper lead and lower lead.
The novel unmanned plane of one the most according to claim 1, it is characterised in that: described support means include electric rotating machine,
Motor cabinet, rotating shaft, bearing, electric pushrod, support bar, supporting seat, shock-proof spring and sensor；Described electric rotating machine
Being arranged in storage box by motor cabinet, rotating shaft one end is attached with electric rotating machine main shaft, and the rotating shaft other end is installed by bearing
On storage box medial wall, being attached in the middle part of electric pushrod upper end and rotating shaft, electric pushrod lower end and support bar one end are carried out even
Connecing, the support bar other end is connected with supporting seat, and shock-proof spring is around being enclosed within support bar, and sensor is arranged on outside supporting seat
On wall.
The novel unmanned plane of one the most according to claim 1, it is characterised in that: described closing device includes cover plate, cunning
Block, motorized rails and limited block；Before and after described cover plate, both sides are respectively symmetrically and are provided with slide block, and motorized rails is separately fixed at storage
Putting before and after box on lateral wall, and be respectively fixed at two ends with limited block about motorized rails, slide block is arranged on motorized rails.
The novel unmanned plane of one the most according to claim 1, it is characterised in that: described supporting seat upper end is provided with set
Cylinder, sleeve inner is provided with female thread, and support bar lower end is provided with external screw thread, is spiral shell between support bar and the sleeve of supporting seat
Stricture of vagina connects, and supporting seat lower end is provided with spike, and a spike is evenly arranged along the circumferential direction of supporting seat, and a spike is
Wedge structure.
Priority Applications (4)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610339028.7A CN105966602B (en) | 2016-05-19 | 2016-05-19 | A kind of unmanned plane |
| CN201711199054.5A CN107933897B (en) | 2016-05-19 | 2016-05-19 | Unmanned aerial vehicle based on infrared ray sensor |
| CN201810082446.1A CN108216588B (en) | 2016-05-19 | 2016-05-19 | Unmanned aerial vehicle |
| CN201711199045.6A CN107985559A (en) | 2016-05-19 | 2016-05-19 | Using the unmanned plane and its method of work of infrared ray sensor |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610339028.7A CN105966602B (en) | 2016-05-19 | 2016-05-19 | A kind of unmanned plane |
Related Child Applications (3)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810082446.1A Division CN108216588B (en) | 2016-05-19 | 2016-05-19 | Unmanned aerial vehicle |
| CN201711199045.6A Division CN107985559A (en) | 2016-05-19 | 2016-05-19 | Using the unmanned plane and its method of work of infrared ray sensor |
| CN201711199054.5A Division CN107933897B (en) | 2016-05-19 | 2016-05-19 | Unmanned aerial vehicle based on infrared ray sensor |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN105966602A true CN105966602A (en) | 2016-09-28 |
| CN105966602B CN105966602B (en) | 2018-01-19 |
Family
ID=56956069
Family Applications (4)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201711199045.6A Withdrawn CN107985559A (en) | 2016-05-19 | 2016-05-19 | Using the unmanned plane and its method of work of infrared ray sensor |
| CN201610339028.7A Expired - Fee Related CN105966602B (en) | 2016-05-19 | 2016-05-19 | A kind of unmanned plane |
| CN201711199054.5A Active CN107933897B (en) | 2016-05-19 | 2016-05-19 | Unmanned aerial vehicle based on infrared ray sensor |
| CN201810082446.1A Active CN108216588B (en) | 2016-05-19 | 2016-05-19 | Unmanned aerial vehicle |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201711199054.5A Active CN107933897B (en) | 2016-05-19 | 2016-05-19 | Unmanned aerial vehicle based on infrared ray sensor |
| CN201810082446.1A Active CN108216588B (en) | 2016-05-19 | 2016-05-19 | Unmanned aerial vehicle |
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Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109353493A (en) * | 2018-09-28 | 2019-02-19 | 许剑聪 | A kind of self-rescue device of drowning unmanned plane equipped with gas generation buoyancy |
| CN112046735A (en) * | 2020-09-17 | 2020-12-08 | 辽宁工程技术大学 | Multifunctional unmanned aerial vehicle undercarriage |
| CN112173115A (en) * | 2020-11-12 | 2021-01-05 | 重庆凯创荣智能科技有限公司 | High-altitude rescue unmanned aerial vehicle with damping device and using method |
| CN114408199A (en) * | 2022-01-28 | 2022-04-29 | 广东皓耘科技有限公司 | Unmanned aerial vehicle positioning and correcting mechanism and undercarriage positioning auxiliary device |
| CN116142515A (en) * | 2023-04-18 | 2023-05-23 | 浙江亿钛数控机械有限公司 | Stably supported unmanned aerial vehicle undercarriage |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110654533A (en) * | 2018-06-29 | 2020-01-07 | 海鹰航空通用装备有限责任公司 | Unmanned aerial vehicle undercarriage |
| CN113525664B (en) * | 2021-09-16 | 2022-01-07 | 速晟电子(深圳)有限公司 | Modularized sensor and unmanned aerial vehicle adaptive to same |
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| CN112173115A (en) * | 2020-11-12 | 2021-01-05 | 重庆凯创荣智能科技有限公司 | High-altitude rescue unmanned aerial vehicle with damping device and using method |
| CN114408199A (en) * | 2022-01-28 | 2022-04-29 | 广东皓耘科技有限公司 | Unmanned aerial vehicle positioning and correcting mechanism and undercarriage positioning auxiliary device |
| CN116142515A (en) * | 2023-04-18 | 2023-05-23 | 浙江亿钛数控机械有限公司 | Stably supported unmanned aerial vehicle undercarriage |
Also Published As
| Publication number | Publication date |
|---|---|
| CN107933897A (en) | 2018-04-20 |
| CN105966602B (en) | 2018-01-19 |
| CN107985559A (en) | 2018-05-04 |
| CN107933897B (en) | 2020-12-04 |
| CN108216588B (en) | 2021-05-25 |
| CN108216588A (en) | 2018-06-29 |
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