CN105966602B - A kind of unmanned plane - Google Patents
A kind of unmanned plane Download PDFInfo
- Publication number
- CN105966602B CN105966602B CN201610339028.7A CN201610339028A CN105966602B CN 105966602 B CN105966602 B CN 105966602B CN 201610339028 A CN201610339028 A CN 201610339028A CN 105966602 B CN105966602 B CN 105966602B
- Authority
- CN
- China
- Prior art keywords
- support
- unmanned plane
- frame
- supporting seat
- undercarriage
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
Links
Classifications
-
- 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 present invention relates to a kind of new unmanned plane, including frame, undercarriage, motor, propeller and damping base；Described undercarriage is located at center position immediately below frame, and undercarriage is connected with frame, the quantity of described motor, propeller and damping base is six, and motor bottom is fixed on above support, propeller is arranged on electric machine main shaft, and damping base is fixed on below support.The present invention can be applied to the takeoff and landing in the case of mountain area or ground relief and level land, strong applicability and good damping effect simultaneously；And the difference in height that compensate for bringing because place is uneven by using support meanss, the present invention is allowd to carry out stable landing on rough place, avoiding unmanned plane, either the rough place in place causes unmanned plane to be broken or damaged phenomenon because of forced landing to mountain area.
Description
Technical field
The present invention relates to unmanned plane field, a kind of specifically unmanned plane.
Background technology
Aircraft is to be manufactured by the mankind, can fly away from ground, controlled in space flight and by people in endoatmosphere or big
The apparatus flying object of the gas-bearing formation external space (space) flight, aircraft are divided into airborne vehicle, spacecraft, rocket, guided missile and guided weapon；
Unmanned plane is also one kind of aircraft, and unmanned plane is manipulated not using radio robot and the presetting apparatus provided for oneself
Manned aircraft, from technical standpoint definition can be divided into depopulated helicopter, unmanned fixed-wing aircraft, unmanned multi-rotor aerocraft, nobody
Dirigible and unmanned parasol etc.；It can be divided into by application field military with civilian, military aspect unmanned plane is divided into reconnaissance plane and target drone；
At present, unmanned plane can be widely applied to national ecological environmental protection, aeroplane photography, mapping, mineral resources exploration, the condition of a disaster monitoring,
Traffic patrolling, 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, the monitoring of protection zone wild animal, air sampling, sea
Thing scouting, border tour, prohibition of drug scouting, fire inspection, ecological environmental protection, marine environmental monitoring, land use survey, water money
It is source exploitation, crop growth monitoring and the yield by estimation, agricultural operation, Natural calamity monitoring and assessment, urban planning and municipal administration, gloomy
The field such as the protection of woods pest and disease damage and monitoring, digital city.
One kind that multi-rotor unmanned aerial vehicle belongs in unmanned plane, multi-rotor unmanned aerial vehicle have that compact-sized, build is less than normal, popular
Change relatively strong, motion flexibly and the advantages that flight stability by extensively in civil and military, and quite it is popular；But at present
Multi-rotor unmanned aerial vehicle after short flight certain time in cruising time due to, with regard to needing to be landed, so as to carry out battery altering, supplementing
The energy, also in that this reason causes unmanned plane to be restricted in very many applications, such as unmanned plane in mountain area or
The rough place in place can not carry out takeoff and landing, and unmanned plane also often occurs because of forced landing to mountain area or field
The rough place in ground causes unmanned plane to be broken or damaged phenomenon.In consideration of it, the invention provides a kind of unmanned plane.
The content of the invention
In order to make up the deficiencies in the prior art, the invention provides a kind of unmanned plane.
The present invention to be solved its technical problem and use following technical scheme to realize.
A kind of unmanned plane, including frame, undercarriage, motor, propeller and damping base；Described undercarriage is located at frame
Underface center position, and undercarriage is connected with frame, central rack structure in the form of annular discs, and central rack is along frame
Central axis uniformly offers fan-shaped material reducing mouth, and central axis of the shell outside along frame is respectively symmetrically provided with six supports,
Bar shaped material reducing mouth is offered on support, by setting fan-shaped material reducing mouth and bar shaped material reducing mouth to alleviate the weight of frame；Described
The quantity of motor, propeller and damping base is six, and motor bottom is fixed on above support, and propeller is arranged on electric machine main shaft
On, damping base is fixed on below support.
Further, described undercarriage includes rise and fall plate, storage box, support meanss and closing device；The described plate that rises and falls
Be square structure, and deck is respectively symmetrically arranged with plate left and right sides of rising and falling, and the cross section of deck is in " Ω " type structure,
The fixation that deck is used between undercarriage and frame, and use the deck of " Ω " type structure to be easy to the installation and removal of undercarriage；
Described storage box, which is fixed on, to be risen and fallen on plate bottom face, and storage box is made up of housing and inside casing, and housing surrounds what is connected with inside casing
" returning " font stores groove, and inside casing space is used for the installation of battery；Described support meanss quantity is four, and support meanss head and the tail are successively
It is arranged in housing " returning " font connected is surrounded with inside casing and stores in groove；Described closing device quantity is two, closing device pair
Title is arranged in storage box lower end.
Further, described damping base includes cushion socket and damping spring；The trapezoidal structure of described cushion socket, damping
Seat upper 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, is provided with down on crosspiece
Lead, and upper lead and lower lead are located on the same line, damping spring both ends rotating around be enclosed on upper lead and
On lower lead, when the present invention is when level land is taken off or is landed, undercarriage, which can shrink, not to be had to, and damping base directly serves as
The effect of undercarriage, and damping base reduces the present invention in vibrations when landing of landing, and is effectively protected drop of the present invention
Fall safety and stability when landing.
Further, described support meanss include electric rotating machine, motor cabinet, rotating shaft, bearing, electric pushrod, support bar, branch
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 madial wall by bearing, in electric pushrod upper end and rotating shaft
Portion is attached, and electric pushrod lower end is attached with support bar one end, and the support bar other end is connected with supporting seat, shock-absorbing bullet
Around being enclosed on support bar, sensor is arranged on supporting seat lateral wall spring, passes through turn of the rotational band turn axle of electric rotating machine
It is dynamic, and be fixedly connected between rotating shaft and electric pushrod, so as to which driving electric push rod is rotated by pivot of rotating shaft, work as electricity
When dynamic push rod turns to vertical with storage box, the rotation for the motor that stops the rotation, start the stretching motion of electric pushrod, due to support
Sensor is installed on runners, and sensor uses infrared ray sensor, when electric pushrod touches ground, electric pushrod stops
Only stretching motion, in the present invention, support meanss quantity are four, when the present invention enters in the place of mountain area or ground relief
It is different by the extended length of electric pushrod when row landing is landed, so as to compensate for the height brought because place is uneven
Difference so that the present invention can carry out stable landing on rough place, and reduce the present invention by shock-proof spring and exist
Jitter during landing.
Further, described closing device includes cover plate, sliding block, motorized rails and limited block；Two before and after described cover plate
Side is respectively symmetrically provided with sliding block, and motorized rails are separately fixed on the front and rear lateral wall of storage box, and motorized rails or so two
End is respectively fixed with limited block, and sliding block is arranged on motorized rails, by motorized rails moving left and right with movable slider, so as to band
The movement of dynamic cover plate, realizes the folding effect of cover plate, and closing device serves protective effect to support meanss.
Further, described supporting seat upper end is provided with sleeve, and sleeve inner is provided with internal thread, and support bar lower end is set
External screw thread is equipped with, to be threadedly coupled between support bar and the sleeve of supporting seat, supporting seat lower end is provided with support feet, and props up
Spike is evenly arranged along the circumferential direction of supporting seat, and support feet is wedge structure.
When unmanned plane in-flight needs landing to land in the area in mountain area or ground relief, start first electronic
Guide rail, by the left and right two lateral movement of the motorized rails with movable slider, so as to drive cover plate, both sides are moved to the left and right, are realized out
Attach together the opening put；Then electric rotating machine is started, by the rotation of the rotational band turn axle of electric rotating machine, and rotating shaft pushes away with electronic
It is fixedly connected between bar, so as to which driving electric push rod is rotated by pivot of rotating shaft, when electric pushrod turns to and stores up
Put box it is vertical when, the rotation for the motor that stops the rotation, start the stretching motion of electric pushrod, due to being provided with sensing on supporting seat
Device, and sensor uses infrared ray sensor, when electric pushrod touches ground, electric pushrod stops stretching motion, at this
In invention, support meanss quantity is four, when the present invention carries out landing in mountain area or the place of ground relief to land, is led to
Cross that the extended length of electric pushrod is different, so as to compensate for the difference in height brought because place is uneven so that the present invention can
To carry out stable landing on rough place, and jitter of the present invention in landing is reduced by shock-proof spring,
Avoiding unmanned plane, either the rough place in place causes unmanned plane to break or damaged show because of forced landing to mountain area
As；When unmanned plane landing, which has supplemented power source, takes off, support meanss are packed up, close closing device, closing device is to support
Device serves protective effect, and when unmanned plane is landed on level land, undercarriage, which can shrink, not to be had to, and damping base directly fills
When the effect of undercarriage, and damping base reduces vibrations of the present invention when landing landing, is effectively protected the present invention
Safety and stability when landing is landed.
Compared with prior art, the present invention has advantages below：
(1) present invention can be applied to the takeoff and landing in the case of mountain area or ground relief and level land simultaneously,
Strong applicability and good damping effect.
(2) difference in height that the present invention compensate for bringing because place is uneven by using support meanss so that the present invention
Stable landing can be carried out on rough place, avoids unmanned plane because of forced landing to mountain area or place bumps not
Flat place causes unmanned plane to be broken or damaged phenomenon.
Brief description of the drawings
The present invention is further described with reference to the accompanying drawings and examples.
Fig. 1 is the dimensional structure diagram of the present invention；
Fig. 2 is dimensional structure diagram when frame, motor, propeller and damping base of the present invention coordinate；
Fig. 3 is the dimensional structure diagram of undercarriage of the present invention；
Fig. 4 is the dimensional structure diagram 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 dimensional structure diagram of support meanss of the present invention；
Fig. 7 is the dimensional structure diagram of damping runners of the present invention.
Embodiment
In order that the technical means, the inventive features, the objects and the advantages of the present invention are easy to understand, tie below
Conjunction is specifically illustrating, and the present invention is expanded on further.
As shown in figure 1, a kind of unmanned plane, including frame 1, undercarriage 2, motor 3, propeller 4 and damping base 5；It is described
Undercarriage 2 be located at the underface center position of frame 1, and undercarriage 2 is connected with frame 1, the middle part of frame 1 knot in the form of annular discs
Structure, and the middle part of frame 1 uniformly offers fan-shaped material reducing mouth, central shaft of the outside of frame 1 along frame 1 along the central axis of frame 1
Line is respectively symmetrically provided with six supports, and bar shaped material reducing mouth is offered on support, by setting 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, and the bottom of motor 3 is fixed
Above support, propeller 4 is arranged on the main shaft of motor 3, 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 meanss 23 and folding dress
Put 24；The described plate 21 that rises and falls is square structure, and deck, and deck are respectively symmetrically arranged with the left and right sides of plate 21 of rising and falling
Cross section be in " Ω " type structure, the fixation that deck is used between undercarriage 2 and frame 1, and using the deck of " Ω " type structure
It is easy to the installation and removal of undercarriage 2；Described storage box 22, which is fixed on, to rise and fall on the bottom face of plate 21, and storage box 22 is by housing
Formed with inside casing, housing surrounds " returning " font connected with inside casing and stores groove, and inside casing space is used for the installation of battery；Described branch
The quantity of support arrangement 23 is four, and the head and the tail of support meanss 23, which are sequentially arranged in housing " returning " font connected is surrounded with inside casing, stores groove
It is interior；The described quantity of closing device 24 is two, and closing device 24 is arranged symmetrically in the lower end of storage box 22.
As shown in Fig. 2 described damping base 5 includes cushion socket 51 and damping spring 52；Described cushion socket 51 is in ladder
Shape structure, the upper end of cushion socket 51 are provided with lead, and the lower end of cushion socket 51 is provided with round bar, and the middle part of cushion socket 51 is provided with horizontal stroke
Grade, lower lead is provided with crosspiece, and upper lead and lower lead are located on the same line, the both ends of damping spring 52 point
Not around being enclosed on upper lead and lower lead, when the present invention is when level land is taken off or is landed, 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 in shake when landing of landing
It is dynamic, it is effectively protected safety and stability when present invention landing is landed.
As shown in Fig. 3 to Fig. 7, described support meanss 23 include electric rotating machine 231, motor cabinet 232, rotating shaft 233, bearing
234th, electric pushrod 235, support bar 236, supporting seat 237, shock-proof spring 238 and sensor 239；Described electric rotating machine
231 are arranged in storage box 22 by motor cabinet 232, and the one end of rotating shaft 233 is attached with the main shaft of electric rotating machine 231, rotating shaft 233
The other end is arranged on the madial wall of storage box 22 by bearing 234, and the upper end of electric pushrod 235 is attached with the middle part of rotating shaft 233,
The lower end of electric pushrod 235 is attached with the one end of support bar 236, and the other end of support bar 236 is connected with supporting seat 237, shock-absorbing
Around being enclosed on support bar 236, sensor 239 is arranged on the lateral wall of supporting seat 237 spring 238, passes through electric rotating machine 231
The rotation of rotational band turn axle 233, and be fixedly connected between rotating shaft 233 and electric pushrod 235, so as to driving electric push rod 235
With rotating shaft 233 be pivot rotated, when electric pushrod 235 turns to it is vertical with storage box 22 when, stop the rotation motor
231 rotation, start the stretching motion of electric pushrod 235, due to being provided with sensor 239, and sensor on supporting seat 237
239 use infrared ray sensor, and when electric pushrod 235 touches ground, electric pushrod 235 stops stretching motion, in this hair
In bright, the quantity of support meanss 23 is four, when the present invention carries out landing in mountain area or the place of ground relief to land, is led to
Cross that the extended length of electric pushrod 235 is different, so as to compensate for the difference in height brought because place is uneven so that the present invention
Stable landing can be carried out on rough place, and the present invention trembling in landing is reduced by shock-proof spring 238
Dynamic property.
As shown in figure 3, described closing device 24 includes cover plate 241, sliding block 242, motorized rails 243 and limited block 244；
The described front and rear sides of cover plate 241 are respectively symmetrically provided with sliding block 242, before motorized rails 243 are separately fixed at storage box 22
Afterwards on lateral wall, and the left and right ends of motorized rails 243 are respectively fixed with limited block 244, and sliding block 242 is arranged on motorized rails 243
On, by the moving left and right with movable slider 242 of motorized rails 243, so as to drive the movement of cover plate 241, realize cover plate 241
Folding effect, closing device 24 serve protective effect to support meanss 23.
As shown in Figure 6 and Figure 7, the described upper end of supporting seat 237 is provided with sleeve, and sleeve inner is provided with internal thread,
Support bar lower end is provided with external screw thread, to be threadedly coupled between support bar and the sleeve of supporting seat 237, under supporting seat 237
End is provided with support feet, and circumferential direction of the support feet along supporting seat 237 is evenly arranged, and support feet is wedge structure.
When unmanned plane in-flight needs landing to land in the area in mountain area or ground relief, start first electronic
Guide rail 243, by the left and right two lateral movement of the motorized rails 243 with movable slider 242, so as to drive the both sides to the left and right of cover plate 241
It is mobile, realize the opening of closing device 24；Then start electric rotating machine 231, pass through the rotational band turn axle of electric rotating machine 231
233 rotation, and be fixedly connected between rotating shaft 233 and electric pushrod 235, so as to which driving electric push rod 235 is with rotating shaft 233
Pivot is rotated, when electric pushrod 235 turns to it is vertical with storage box 22 when, the rotation for the motor 231 that stops the rotation, open
The stretching motion of dynamic electric pushrod 235, due to being provided with sensor 239 on supporting seat 237, and sensor 239 is using infrared
Line sensor, when electric pushrod 235 touches ground, electric pushrod 235 stops stretching motion, in the present invention, support dress
It is four to put 23 quantity, when the present invention carries out landing in mountain area or the place of ground relief to land, passes through electric pushrod
235 extended length is different, so as to compensate for the difference in height brought because place is uneven so that the present invention can be in bumps
Stable landing is carried out on uneven place, and jitter of the present invention in landing is reduced by shock-proof spring 238；When nobody
When machine landing has supplemented power source and taken off, support meanss 23 are packed up, close closing device 24, closing device 24 is to support meanss
23 serve protective effect, and when unmanned plane is landed on level land, undercarriage 2, which can shrink, not to be had to, and damping base 5 is direct
The effect of undercarriage 2 is act as, and damping base 5 reduces vibrations of the present invention when landing landing, is effectively protected this
Safety and stability when invention landing is landed.
The basic principles, principal features and advantages of the present invention have been shown and described above.The technical staff of the industry should
Understand, the present invention is not limited to the above embodiments, and the description in above-described embodiment and specification simply illustrates the present invention
Principle, without departing from the spirit and scope of the present invention, various changes and modifications of the present invention are possible, and these change and changed
Enter all fall within the protetion scope of the claimed invention.The claimed scope of the invention is by appended claims and its equivalent
Define.
Claims (4)
- A kind of 1. unmanned plane, it is characterised in that：Including frame, undercarriage, motor, propeller and damping base；Described rises and falls Frame is located at center position immediately below frame, and undercarriage is connected with frame, central rack structure in the form of annular discs, and in frame Central axis of the portion along frame uniformly offers fan-shaped material reducing mouth, and central axis of the shell outside along frame is respectively symmetrically provided with Six supports, bar shaped material reducing mouth is offered on support；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 meanss and closing device；The described plate that rises and falls is square structure, Deck is respectively symmetrically arranged with plate left and right sides of rising and falling, and the cross section of deck is in " Ω " type structure；Described stores Box, which is fixed on, to be risen and fallen 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 meanss quantity is four, and support meanss head and the tail are sequentially arranged in housing and " returning " word connected is surrounded with inside casing Type is stored 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 are set There is upper lead, cushion socket lower end is provided with round bar, is provided with crosspiece in the middle part of cushion socket, lower lead is provided with crosspiece, and Upper lead and lower lead are located on the same line, and damping spring both ends are rotating around being enclosed on upper lead and lower lead On.
- A kind of 2. unmanned plane according to claim 1, it is characterised in that：It is mechanical, electrical that described support meanss include electric rotating Support, rotating shaft, bearing, electric pushrod, support bar, supporting seat, shock-proof spring and sensor；Described electric rotating machine passes through electricity Support is arranged in storage box, and rotating shaft one end is attached with electric rotating machine main shaft, and the rotating shaft other end is arranged on storage by bearing To put on box madial wall, with being attached in the middle part of rotating shaft, electric pushrod lower end is attached with support bar one end for electric pushrod upper end, The support bar other end is connected with supporting seat, and for shock-proof spring around being enclosed on support bar, sensor is arranged on supporting seat lateral wall On.
- A kind of 3. unmanned plane according to claim 1, it is characterised in that：Described closing device includes cover plate, sliding block, electricity Dynamic guide rail and limited block；Described cover plate front and rear sides are respectively symmetrically provided with sliding block, and motorized rails are separately fixed at storage box Front and rear lateral wall on, and motorized rails left and right ends are respectively fixed with limited block, and sliding block is arranged on motorized rails.
- A kind of 4. unmanned plane according to claim 1, it is characterised in that：Described supporting seat upper end is provided with sleeve, Sleeve inner is provided with internal thread, and support bar lower end is provided with external screw thread, is screw thread between support bar and the sleeve of supporting seat Connection, supporting seat lower end is provided with support feet, and support feet is evenly arranged along the circumferential direction of supporting seat, and support feet is wedge Shape 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 CN105966602A (en) | 2016-09-28 |
| CN105966602B true 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 |
Family Applications Before (1)
| 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 |
Family Applications After (2)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| 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 |
Country Status (1)
| Country | Link |
|---|---|
| CN (4) | CN107985559A (en) |
Cited By (1)
| 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 |
Families Citing this family (6)
| 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 |
| CN112046735B (en) * | 2020-09-17 | 2024-05-28 | 辽宁工程技术大学 | Multifunctional unmanned aerial vehicle landing gear |
| CN112173115B (en) * | 2020-11-12 | 2022-05-13 | 观典防务技术股份有限公司 | Use method of high-altitude rescue unmanned aerial vehicle with damping device |
| 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 |
| 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 |
| CN116142515B (en) * | 2023-04-18 | 2023-06-27 | 浙江亿钛数控机械有限公司 | Stably supported unmanned aerial vehicle undercarriage |
Family Cites Families (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6715714B2 (en) * | 2001-09-24 | 2004-04-06 | Larry Dan Temple | Landing gear for model airplane |
| CN101746500B (en) * | 2009-12-03 | 2012-10-03 | 李子赫 | Device for compensating the difference of height by which a helicopter lands on a non-horizontal ground and the method thereof |
| US8973861B2 (en) * | 2012-10-29 | 2015-03-10 | Shenzhen Hubsan Technology Co., Ltd. | Tetra-propeller aircraft |
| CA2815885C (en) * | 2013-05-15 | 2018-05-15 | Draganfly Innovations Inc. | Compact unmanned rotary aircraft |
| CN204161620U (en) * | 2014-10-16 | 2015-02-18 | 云南电网公司红河供电局 | The full landform retractable landing gear of depopulated helicopter |
| CN104787319A (en) * | 2015-04-23 | 2015-07-22 | 张�杰 | Four-rotor aircraft provided with telescopic and foldable undercarriages |
| CN104787309B (en) * | 2015-05-12 | 2016-11-09 | 厦门大学 | Rotor wing unmanned aerial vehicle undercarriage |
| CN204916163U (en) * | 2015-06-19 | 2015-12-30 | 深圳一电科技有限公司 | Foot rest and unmanned aerial vehicle |
| CN204956904U (en) * | 2015-09-14 | 2016-01-13 | 南京工程学院 | Many rotor crafts intelligence alighting carriage and control system thereof |
| CN205055438U (en) * | 2015-09-21 | 2016-03-02 | 重庆燕蓝科技有限公司 | A buffering undercarriage for model aeroplane and model ship aircraft |
| CN205098463U (en) * | 2015-10-22 | 2016-03-23 | 郑州大学 | Full topography helicopter undercarriage |
| CN205113694U (en) * | 2015-11-21 | 2016-03-30 | 长沙学院 | Buffering foot rest of rotor craft |
-
2016
- 2016-05-19 CN CN201711199045.6A patent/CN107985559A/en not_active Withdrawn
- 2016-05-19 CN CN201610339028.7A patent/CN105966602B/en not_active Expired - Fee Related
- 2016-05-19 CN CN201711199054.5A patent/CN107933897B/en active Active
- 2016-05-19 CN CN201810082446.1A patent/CN108216588B/en active Active
Cited By (1)
| 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 |
Also Published As
| Publication number | Publication date |
|---|---|
| CN107933897A (en) | 2018-04-20 |
| CN107985559A (en) | 2018-05-04 |
| CN105966602A (en) | 2016-09-28 |
| CN107933897B (en) | 2020-12-04 |
| CN108216588B (en) | 2021-05-25 |
| CN108216588A (en) | 2018-06-29 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN105966602B (en) | A kind of unmanned plane | |
| CN105966599B (en) | A kind of aircraft | |
| CN105952842B (en) | A kind of power-line patrolling unmanned plane charging base station damping device | |
| CN106114884B (en) | A kind of unmanned plane based on Stewart parallel institutions stops charging station | |
| CN105730686B (en) | A kind of multi-rotor aerocraft based on Stewart six-degree-of-freedom parallel connection mechanisms | |
| CN106143938B (en) | A kind of thunderstorm weather electric power Drones for surveillance's bus stop | |
| CN105966608B (en) | A kind of aircraft landing gear | |
| CN105966605A (en) | Delta parallel mechanism-based six-rotor aircraft | |
| CN106184796A (en) | A kind of on-air radio network detecting unmanned plane charging station damped platform | |
| CN106122361A (en) | A kind of multi-rotor aerocraft intelligent docking equipment | |
| CN105914844B (en) | A kind of multidimensional damping type unmanned plane charging station | |
| CN106081144B (en) | A kind of power-line patrolling unmanned plane charging base station | |
| CN105857585B (en) | A kind of unmanned plane undercarriage suitable for mountain area flight | |
| CN106026273B (en) | A kind of power-line patrolling unmanned plane charging equipment based on delta parallel institutions | |
| CN105882944B (en) | A kind of unmanned plane undercarriage with dual shock absorption function | |
| CN106005464B (en) | A kind of energy-saving unmanned plane energy ancillary equipment | |
| CN106051034B (en) | A kind of electric power reconnoitres flying robot and stops charging equipment vibration-damped table | |
| CN106184795B (en) | A kind of plant protection unmanned plane charging station | |
| CN105978458B (en) | A kind of adjustable supporting | |
| CN106184797B (en) | A kind of UAV Intelligent stop equipment | |
| CN105909926A (en) | Vibration reducing device for unmanned aerial vehicle charging base station based on Stewart parallel mechanism | |
| CN106005465B (en) | A kind of electric power Drones for surveillance bus stop masking device | |
| CN105966606B (en) | A kind of telescopic type aircraft damping |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| CB03 | Change of inventor or designer information | ||
| CB03 | Change of inventor or designer information |
Inventor after: Liu De Inventor after: Li Jing Inventor after: Zhao Guanbao Inventor before: Zheng Linlin |
|
| TA01 | Transfer of patent application right | ||
| TA01 | Transfer of patent application right |
Effective date of registration: 20171128 Address after: 224000 in Jiangsu province in the south of Yancheng City District Xindu Street big data Industrial Park South Chong Building Room 1766 (CND) Applicant after: Yancheng Haina Media Co., Ltd. Address before: 246001 Anhui Province, Anqing City Yingjiang District Changfeng Township Ma Wo Street No. 2-7-90 Applicant before: Zheng Linlin |
|
| 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: 20180119 Termination date: 20180519 |