CN108974342A - A kind of bridge machinery unmanned plane based on bridge security performance - Google Patents
A kind of bridge machinery unmanned plane based on bridge security performance Download PDFInfo
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- CN108974342A CN108974342A CN201810705201.XA CN201810705201A CN108974342A CN 108974342 A CN108974342 A CN 108974342A CN 201810705201 A CN201810705201 A CN 201810705201A CN 108974342 A CN108974342 A CN 108974342A
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- China
- Prior art keywords
- synchronizing wheel
- landing
- unmanned plane
- fluted disc
- bridge
- 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.)
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- 230000003139 buffering effect Effects 0.000 claims abstract description 46
- 230000001681 protective effect Effects 0.000 claims abstract description 6
- 230000001360 synchronised effect Effects 0.000 claims description 36
- 239000002131 composite material Substances 0.000 claims description 24
- 238000013016 damping Methods 0.000 claims description 17
- 239000000203 mixture Substances 0.000 claims description 11
- ATJFFYVFTNAWJD-UHFFFAOYSA-N Tin Chemical compound [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 claims description 10
- 230000005540 biological transmission Effects 0.000 claims description 5
- 239000003292 glue Substances 0.000 claims description 3
- 239000007787 solid Substances 0.000 claims description 2
- 238000003466 welding Methods 0.000 claims description 2
- 230000000694 effects Effects 0.000 claims 1
- 238000000034 method Methods 0.000 abstract description 11
- 230000009975 flexible effect Effects 0.000 abstract description 4
- 230000035939 shock Effects 0.000 abstract description 3
- 238000001514 detection method Methods 0.000 description 8
- 238000010586 diagram Methods 0.000 description 4
- 150000001875 compounds Chemical class 0.000 description 3
- 230000005611 electricity Effects 0.000 description 2
- NJPPVKZQTLUDBO-UHFFFAOYSA-N novaluron Chemical compound C1=C(Cl)C(OC(F)(F)C(OC(F)(F)F)F)=CC=C1NC(=O)NC(=O)C1=C(F)C=CC=C1F NJPPVKZQTLUDBO-UHFFFAOYSA-N 0.000 description 2
- 238000013021 overheating Methods 0.000 description 2
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 2
- 241000237858 Gastropoda Species 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 239000003638 chemical reducing agent Substances 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000004080 punching Methods 0.000 description 1
- 238000000926 separation method Methods 0.000 description 1
Classifications
-
- 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
- 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
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
- B64D47/08—Arrangements of cameras
-
- 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
- B64U30/00—Means for producing lift; Empennages; Arrangements thereof
- B64U30/20—Rotors; Rotor supports
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/10—Propulsion
- B64U50/19—Propulsion using electrically powered motors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
- B64U2101/30—UAVs specially adapted for particular uses or applications for imaging, photography or videography
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Remote Sensing (AREA)
- Studio Devices (AREA)
Abstract
The invention discloses a kind of bridge machinery unmanned planes based on bridge security performance, its structure includes multi-angle observation and landing and buffering device, control panel, radiating block, first rotating vane, second rotating vane, working station indicator, unmanned plane main body, blade rotor, third rotating vane, 4th rotating vane, protective cover, headlamp, multi-angle observation and landing and buffering device are welded in the lower end of unmanned plane main body, control panel is fixed by screws in multi-angle observation and the positive right end of landing and buffering device, the present invention is by being equipped with multi-angle observation and landing and buffering device, when equipment detects bridge, high-definition camera can be with multi-angle rotation, keep equipment more flexible when shooting, convenient for the progress of shooting process, and equipment is in landing, glissando is in place, equipment will not be by excessive shock, pole Big protects apparatus assembly, improves the service life of equipment entirety.
Description
Technical field
The present invention is a kind of bridge machinery unmanned plane based on bridge security performance, belongs to unmanned plane field.
Background technique
UAV referred to as " unmanned plane ", is manipulated using radio robot and the presetting apparatus provided for oneself
Not manned aircraft, or fully or intermittently automatically operated by car-mounted computer.
The equipment of the prior art is when detecting bridge, and since detection process is complex, equipment flexibility is poor,
Detection process is subject to certain restrictions, and after equipment has detected, and will receive biggish impact force during landing, and easy pair
Equipment causes to damage.
Summary of the invention
In view of the deficienciess of the prior art, it is an object of the present invention to provide a kind of bridge machineries based on bridge security performance
With unmanned plane, to solve the equipment of the prior art when detecting to bridge, since detection process is complex, equipment is flexible
Property is poor, and detection process is subject to certain restrictions, and after equipment has detected, and will receive biggish impact during landing
Power is easy the problem of damage is caused to equipment.
To achieve the goals above, the present invention is to realize by the following technical solutions: one kind is based on bridge safty
The bridge machinery unmanned plane of energy, structure includes multi-angle observation and landing and buffering device, control panel, radiating block, first
Rotating vane, the second rotating vane, working station indicator, unmanned plane main body, blade rotor, third rotating vane, the 4th rotation
Rotating vane piece, protective cover, headlamp, the multi-angle observation and landing and buffering device are welded in the lower end of unmanned plane main body, described
Control panel is fixed by screws in multi-angle observation and the positive right end of landing and buffering device, and the headlamp is welded in polygonal
Degree observation is in same level with the positive left end of landing and buffering device, the control panel and headlamp, the protection
Cover is embedded in the left surface of multi-angle observation and landing and buffering device, and the working station indicator is being fitted in unmanned plane main body just
Face, first rotating vane are movably connected on the right front ends of unmanned plane body upper surface, and the second rotating vane machinery connects
It is connected to the right rear end of unmanned plane body upper surface, the third rotating vane is movably connected on the left back of unmanned plane body upper surface
End, the 4th rotating vane are mechanically connected to the left front end of unmanned plane body upper surface, and the blade rotor is revolved through third
The upper surface of rotating vane piece, the third rotating vane is identical as the 4th rotating vane shape size, the multi-angle observation with fall
Ground buffer unit is by rack-driving structure, electric motor starting structure, high-definition camera angle-regulation structure, the first landing and buffering knot
Structure, the second landing and buffering structure, crust of the device composition, right end of the rack-driving structure inside crust of the device are described
Electric motor starting structure is fitted in the upper end inside crust of the device, and the high-definition camera angle-regulation structure is movably connected on device
The left end of interior of shell, lower end of the first landing and buffering structure clearance fit inside crust of the device, second landing
Buffer structure is fitted in the right end of the first landing and buffering structure.
Further, the rack-driving structure is by the first synchronous belt, first gear shaft, the first synchronizing wheel, the first tooth
Item, the first fluted disc, the second synchronous belt, gear turntable, the second rack gear, second gear shaft, bevel gear, first rotating shaft, second
Synchronizing wheel, third synchronizing wheel, third synchronous belt, driving motor composition.
Further, the first synchronizing wheel clearance fit is under the middle section of the first synchronous belt, first synchronous belt
For end ring around the outer ring for being connected to first gear shaft, first rack gear is engaged on the front end of first gear shaft, and described first
Rack gap cooperation is in the lower end of the first fluted disc, and the top ring of first synchronous belt is around being connected to the outer of second gear shaft
Circle, the front end of the second gear shaft and the second rack gap cooperate, and second rack gear is engaged on the upper end of the first fluted disc,
The front end of first fluted disc is sequentially connected by the outer ring of the second synchronous belt and gear turntable, and the bevel gear is engaged on tooth
The positive upper end of turntable is taken turns, the bevel gear is interference fitted in the lower end of first rotating shaft, and the third synchronizing wheel is nested in the
The outer ring of one shaft, second synchronizing wheel are welded in the lower end of driving motor, and second synchronizing wheel passes through third synchronous belt
It is sequentially connected with third synchronizing wheel, second synchronizing wheel is identical as third synchronous belt shape size.
Further, the electric motor starting structure is by the first gag lever post, the second gag lever post, worm screw, matching board, battery, electricity
Pond fixed plate, the first contact block, the second contact block, support plate, decelerating motor composition, the left end and cooperation sheet separation of the worm screw
Cooperation, second gag lever post are welded in the lower end of matching board left surface, tell that the first gag lever post and the second gag lever post are mutually equal
Row, first gag lever post run through the right surface of support plate, and the first contact block glue connection is connected to the upper end of matching board left surface,
Second contact block is fitted in the upper end on the right surface of support plate, the welding battery in the right end of battery retaining boards lower surface,
The decelerating motor is fixed by screws in the left end of battery retaining boards lower surface, and the battery and decelerating motor are in same water
In plane, first synchronizing wheel is nested in the right end of worm screw.
Further, the high-definition camera angle-regulation structure is by the 4th synchronizing wheel, the first composite sync band, second turn
Axis, the first roller, the second fluted disc, fluted disc connecting rod, half fluted disc, high-definition camera, the 5th synchronizing wheel, the second composite sync band,
Round turntable, conveyer belt, second tin roller, the 6th synchronizing wheel, third composite sync band, third roller composition.
Further, the 4th synchronizing wheel is sequentially connected by the front end of the first composite sync band and the first roller, institute
It is identical as second tin roller, third roll form size to state the first roller, the conveyer belt clearance fit in the outer ring of second tin roller,
First roller is connect by conveyer belt with third drum drive, and the front end of the third roller passes through third composite sync band
It is sequentially connected with the 6th synchronizing wheel, the 6th synchronizing wheel is interference fitted in the lower end of the second shaft, and the 5th synchronizing wheel is embedding
It covering in the outer ring of the second shaft, the 5th synchronizing wheel is connected by the rear-end transmission of the second composite sync band and round turntable,
The lower end of the fluted disc connecting rod is movably connected on the front of round turntable, and the upper mechanical of the fluted disc connecting rod is connected to
The front of two fluted discs, second fluted disc are engaged on the upper right side of half fluted disc, and the high-definition camera is welded in a left side for half fluted disc
End, the 4th synchronizing wheel are interference fitted in the lower end of decelerating motor.
Further, first landing and buffering structure is fixed by the first damping spring, fixed plate, first sleeve, first
Frame, the first telescopic mast, the first connection frame, the second connection frame, the second fixed frame, the first fixed column, the first support base composition, institute
State the left end that first sleeve is welded in fixed plate lower surface, first fixed frame is welded in the left end of first sleeve, and described
The upper end of one telescopic mast is slidably connected to the left end of the first fixed frame lower surface, and the upper end of first connection frame is movably connected on
The lower end of the positive right end of first fixed frame, first connection frame is connect with the upper mechanical of the second connection frame, and described first
The lower end of telescopic mast is slidably connected to the left end of the second fixed frame upper surface, and the lower end of second connection frame is movably connected on
The positive right end of two fixed frames, first fixed column are nested in the lower end of first sleeve, and first damping spring is welded in
The upper end of first fixed column, second fixed frame are embedded in the left end of the first fixed column, and first support base is welded in the
The lower end of one fixed column.
Further, second landing and buffering structure is by the second damping spring, second sleeve, third fixed frame, second
Telescopic mast, third connection frame, the 4th connection frame, the 4th fixed frame, the second fixed column, the second support base composition, the third
Fixed frame is welded in the right side of second sleeve, and second fixed column is nested in the lower end of second sleeve, the second damping bullet
Spring is welded in the upper end of the second fixed column, and second support base is nested in the lower end of the second fixed column, and described second is flexible
The upper end of column is slidably connected to the right end of third fixed frame lower surface, and it is solid that the upper end of the third connection frame is movably connected on third
Determine the positive left end of frame, the lower mechanical of the third connection frame is connected to the upper end of the 4th connection frame, the 4th fixed frame
It is welded in the right side of the second fixed column, the lower end of the 4th connection frame is movably connected on the 4th positive left end of fixed frame, institute
The lower end for stating the second telescopic mast is slidably connected to the right end of the 4th fixed frame upper surface.
Further, the radiating block radiates convenient for equipment, prevents apparatus assembly from overheating, and influences equipment use.
Further, the working station indicator learns the working condition of equipment convenient for operator.
Beneficial effect
A kind of bridge machinery unmanned plane based on bridge security performance of the present invention, when in use, operator puts equipment
It sets in suitable place, is then turned on equipment and bridge is detected after equipment lift-off, open driving motor, driving motor turns
Dynamic to make the second synchronizing wheel with rotation, then the second synchronizing wheel drives third synchronizing wheel by third synchronous belt, and then first turn
Axis rotation makes bevel gear with rotation, and then bevel gear drives gear turntable, rotates gear turntable, then gear turntable
The first fluted disc is driven by the second synchronous belt, rotates the first fluted disc, the first fluted disc moves the first rack gear and the second rack gear or so
Dynamic, the first rack gear and the second rack gear rotate first gear shaft and second gear shaft, and then the first synchronous belt pulls first
Synchronizing wheel rotates the first synchronizing wheel, and the rotation of the first synchronizing wheel makes worm screw with rotation, and worm screw rotation makes matching board to moving to left
Dynamic, the first gag lever post and the second gag lever post play the role of limit, and then the first contact block is contacted with the second contact block, battery
Small circuit is switched on, and battery is powered decelerating motor as power supply body, and then decelerating motor rotates, and decelerating motor rotation makes
4th synchronizing wheel drives the first roller to rotate the first roller with rotation, the 4th synchronizing wheel by the first composite sync band, so
The first roller rotates third roller by conveyer belt afterwards, and third roller makes the 6th synchronous rotation by third composite sync band
Dynamic, the rotation of the 6th synchronizing wheel rotates the second shaft, and the rotation of the second shaft rotates the 5th synchronizing wheel, and then the 5th synchronizing wheel is logical
Crossing the second composite sync band rotates round turntable, and round turntable rotates the second fluted disc by fluted disc connecting rod, the second fluted disc
Rotation rotates half fluted disc, and the rotation of half fluted disc makes high-definition camera, so that high-definition camera is can be carried out the shooting of multi-angle, to bridge
Carry out multi-faceted detection, when equipment check after, equipment needs to drop on ground, when by falling, the first support base with
Second support base first with ground face contact, then receives impact force, moves the first fixed column up with the second fixed column, and first
Damping spring is compressed with the second damping spring, offsets the impact force of a part, then the first telescopic mast is moved to the left and is pressed
Contracting, the second telescopic mast move right and are compressed, and counteract the impact force of a part, to protect the peace of apparatus assembly
Entirely.
A kind of bridge machinery unmanned plane based on bridge security performance of the present invention, by being equipped with multi-angle observation and landing
Buffer unit, when equipment detects bridge, high-definition camera can keep equipment more clever when shooting with multi-angle rotation
Living, convenient for the progress of shooting process, and equipment, in landing, in place, equipment will not be by excessive shock, greatly for glissando
Protect apparatus assembly, improve the service life of equipment entirety.
Detailed description of the invention
Upon reading the detailed description of non-limiting embodiments with reference to the following drawings, other feature of the invention,
Objects and advantages will become more apparent upon:
Fig. 1 is a kind of structural schematic diagram of the bridge machinery unmanned plane based on bridge security performance of the present invention；
Fig. 2 is the structural schematic diagram of multi-angle observation of the present invention and landing and buffering device；
Fig. 3 is the structural schematic diagram after high-definition camera angle-regulation structure of the present invention rotation；
Fig. 4 is the first landing and buffering structure of the invention by compressed structural schematic diagram；
In figure: multi-angle observation and landing and buffering device -1, control panel -2, radiating block -3, the first rotating vane -4, the
Two rotating vanes -5, working station indicator -6, unmanned plane main body -7, blade rotor -8, third rotating vane the -9, the 4th rotate
Blade -10, protective cover -11, headlamp -12, rack-driving structure -101, electric motor starting structure -102, high-definition camera angle
Adjustment structure -103, the first landing and buffering structure -104, the second landing and buffering structure -105, crust of the device -106, first synchronize
Band -10101, first gear shaft -10102, the first synchronizing wheel -10103, the first rack gear -10104, the first fluted disc -10105, the
Two synchronous belts -10106, gear turntable -10107, the second rack gear -10108, second gear shaft -10109, bevel gear -
10110, first rotating shaft -10111, the second synchronizing wheel -10112, third synchronizing wheel -10113, third synchronous belt -10114, driving
Motor -10115, the first gag lever post -10201, the second gag lever post -10202, worm screw -10203, matching board -10204, battery -
10205, battery retaining boards -10206, the first contact block -10207, the second contact block -10208, support plate -10209, deceleration electricity
Machine -10210, the 4th synchronizing wheel -10301, the first composite sync band -10302, the second shaft -10303, the first roller -10304,
Second fluted disc -10305, fluted disc connecting rod -10306, half fluted disc -10307, high-definition camera -10308, the 5th synchronizing wheel -
10309, the second composite sync band -10310, round turntable -10311, conveyer belt -10312, second tin roller -10313, the 6th same
Step wheel -10314, third composite sync band -10315, third roller -10316, the first damping spring -10401, fixed plate -
10402, first sleeve -10403, the first fixed frame -10404, the first telescopic mast -10405, the first connection frame -10406, second
Connection frame -10407, the second fixed frame -10408, the first fixed column -10409, the first support base -10410, the second damping bullet
Spring -10501, second sleeve -10502, third fixed frame -10503, the second telescopic mast -10504, third connection frame -10505,
Four connection frames -10506, the 4th fixed frame -10507, the second fixed column -10508, the second support base -10509.
Specific embodiment
To be easy to understand the technical means, the creative features, the aims and the efficiencies achieved by the present invention, below with reference to
Specific embodiment, the present invention is further explained.
Fig. 1-Fig. 4 is please referred to, the present invention provides a kind of bridge machinery unmanned air vehicle technique side based on bridge security performance
Case: its structure includes that multi-angle observation and landing and buffering device 1, control panel 2, radiating block 3, the first rotating vane 4, second revolve
Rotating vane piece 5, unmanned plane main body 7, blade rotor 8, third rotating vane 9, the 4th rotating vane 10, is protected working station indicator 6
Shield 11, headlamp 12, the multi-angle observation and landing and buffering device 1 are welded in the lower end of unmanned plane main body 7, the control
Panel 2 is fixed by screws in multi-angle observation and the positive right end of landing and buffering device 1, and the headlamp 12 is welded in polygonal
Degree observation and the positive left end of landing and buffering device 1, the control panel 2 is in same level with headlamp 12, described
Protective cover 11 is embedded in the left surface of multi-angle observation and landing and buffering device 1, and the working station indicator 6 is fitted in unmanned plane
The front of main body 7, first rotating vane 4 are movably connected on the right front ends of 7 upper surface of unmanned plane main body, second rotation
Blade 5 is mechanically connected to the right rear end of 7 upper surface of unmanned plane main body, and the third rotating vane 9 is movably connected on unmanned owner
The left back end of 7 upper surface of body, the 4th rotating vane 10 is mechanically connected to the left front end of 7 upper surface of unmanned plane main body, described
Blade rotor 8 runs through the upper surface of third rotating vane 9, the third rotating vane 9 and 10 shape size of the 4th rotating vane
Identical, the multi-angle observation and landing and buffering device 1 are by rack-driving structure 101, electric motor starting structure 102, high-definition camera
Head angle-regulation structure 103, the first landing and buffering structure 104, the second landing and buffering structure 105, crust of the device 106 form, institute
Right end of the rack-driving structure 101 inside crust of the device 106 is stated, the electric motor starting structure 102 is fitted in crust of the device
Upper end inside 106, the high-definition camera angle-regulation structure 103 are movably connected on the left end inside crust of the device 106, institute
State lower end of 104 clearance fit of the first landing and buffering structure inside crust of the device 106, second landing and buffering structure 105
It is fitted in the right end of the first landing and buffering structure 104, the rack-driving structure 101 is by the first synchronous belt 10101, first gear
Shaft 10102, the first synchronizing wheel 10103, the first rack gear 10104, the first fluted disc 10105, the second synchronous belt 10106, gear turn
Disk 10107, the second rack gear 10108, second gear shaft 10109, bevel gear 10110, first rotating shaft 10111, second are synchronous
Wheel 10112, third synchronizing wheel 10113, third synchronous belt 10114, driving motor 10115 form, first synchronizing wheel 10103
Clearance fit turns in the middle section of the first synchronous belt 10101, the lower loop of first synchronous belt 10101 around first gear is connected to
The outer ring of axis 10102, first rack gear 10104 are engaged on the front end of first gear shaft 10102, first rack gear
10104 clearance fits are in the lower end of the first fluted disc 10105, and the top ring of first synchronous belt 10101 is around being connected to the second tooth
The outer ring of wheel shaft 10109, the front end of the second gear shaft 10109 and 10108 clearance fit of the second rack gear, described second
Rack gear 10108 is engaged on the upper end of the first fluted disc 10105, and the front end of first fluted disc 10105 passes through the second synchronous belt 10106
It being sequentially connected with the outer ring of gear turntable 10107, the bevel gear 10110 is engaged on the positive upper end of gear turntable 10107,
The bevel gear 10110 is interference fitted in the lower end of first rotating shaft 10111, and the third synchronizing wheel 10113 is nested in first
The outer ring of shaft 10111, second synchronizing wheel 10112 are welded in the lower end of driving motor 10115, second synchronizing wheel
10112 are sequentially connected by third synchronous belt 10114 and third synchronizing wheel 10113, and second synchronizing wheel 10112 and third are same
Step 10114 shape size of band is identical, and the electric motor starting structure 102 is by the first gag lever post 10201, the second gag lever post 10202, snail
Bar 10203, matching board 10204, battery 10205, battery retaining boards 10206, the first contact block 10207, the second contact block
10208, support plate 10209, decelerating motor 10210 form, the left end of the worm screw 10203 and 10204 clearance fit of matching board,
Second gag lever post 10202 is welded in the lower end of 10204 left surface of matching board, tells the first gag lever post 10201 and the second limit
Position bar 10202 is parallel to each other, and first gag lever post 10201 runs through the right surface of support plate 10209, first contact block
10207 glue connections are connected to the upper end of 10204 left surface of matching board, and second contact block 10208 is fitted in the right table of support plate 10209
The upper end in face, the battery 10205 are welded in the right end of 10206 lower surface of battery retaining boards, and the decelerating motor 10210 passes through
Screw is fixed on the left end of 10206 lower surface of battery retaining boards, and the battery 10205 is in same water with decelerating motor 10210
In plane, first synchronizing wheel 10103 is nested in the right end of worm screw 10203, the high-definition camera angle-regulation structure 103
By the 4th synchronizing wheel 10301, the first composite sync band 10302, the second shaft 10303, the first roller 10304, the second fluted disc
10305, fluted disc connecting rod 10306, half fluted disc 10307, high-definition camera 10308, the 5th synchronizing wheel 10309, second are compound same
It is compound same to walk band 10310, round turntable 10311, conveyer belt 10312, second tin roller 10313, the 6th synchronizing wheel 10314, third
Band 10315, the composition of third roller 10316 are walked, the 4th synchronizing wheel 10301 passes through the first composite sync band 10302 and first
The front end of roller 10304 is sequentially connected, and first roller 10304 and second tin roller 10313,10316 shape of third roller are big
Small identical, 10312 clearance fit of conveyer belt passes through conveying in the outer ring of second tin roller 10313, first roller 10304
Band 10312 and third roller 10316 are sequentially connected, and the front end of the third roller 10316 passes through third composite sync band 10315
It is sequentially connected with the 6th synchronizing wheel 10314, the 6th synchronizing wheel 10314 is interference fitted in the lower end of the second shaft 10303, institute
The outer ring that the 5th synchronizing wheel 10309 is nested in the second shaft 10303 is stated, the 5th synchronizing wheel 10309 is compound same by second
Step band 10310 is connect with the rear-end transmission of round turntable 10311, and the lower end of the fluted disc connecting rod 10306 is movably connected on circle
The front of shape turntable 10311, the upper mechanical of the fluted disc connecting rod 10306 is connected to the front of the second fluted disc 10305, described
Second fluted disc 10305 is engaged on the upper right side of half fluted disc 10307, and the high-definition camera 10308 is welded in half fluted disc 10307
Left end, the 4th synchronizing wheel 10301 are interference fitted in the lower end of decelerating motor 10210, first landing and buffering structure 104
By the first damping spring 10401, fixed plate 10402, first sleeve 10403, the first fixed frame 10404, the first telescopic mast
10405, the first connection frame 10406, the second connection frame 10407, the second fixed frame 10408, the first fixed column 10409, first
It supports pedestal 10410 to form, the first sleeve 10403 is welded in the left end of 10402 lower surface of fixed plate, first fixed frame
10404 are welded in the left end of first sleeve 10403, and the upper end of first telescopic mast 10405 is slidably connected to the first fixed frame
The left end of 10404 lower surfaces, the upper end of first connection frame 10406 are movably connected on the positive right side of the first fixed frame 10404
End, the lower end of first connection frame 10406 are connect with the upper mechanical of the second connection frame 10407, first telescopic mast
10405 lower end is slidably connected to the left end of 10408 upper surface of the second fixed frame, and the lower end of second connection frame 10407 is living
Dynamic to be connected to the positive right end of the second fixed frame 10408, first fixed column 10409 is nested under first sleeve 10403
End, first damping spring 10401 are welded in the upper end of the first fixed column 10409, and second fixed frame 10408 is embedded in the
The left end of one fixed column 10409, first support base 10410 are welded in the lower end of the first fixed column 10409, and described second
Landing and buffering structure 105 is by the second damping spring 10501, second sleeve 10502, third fixed frame 10503, the second telescopic mast
10504, third connection frame 10505, the 4th connection frame 10506, the 4th fixed frame 10507, the second fixed column 10508, second
It supports pedestal 10509 to form, the third fixed frame 10503 is welded in the right side of second sleeve 10502, second fixed column
10508 are nested in the lower end of second sleeve 10502, and second damping spring 10501 is welded in the upper of the second fixed column 10508
End, second support base 10509 are nested in the lower end of the second fixed column 10508, the upper end of second telescopic mast 10504
It is slidably connected to the right end of 10503 lower surface of third fixed frame, the upper end of the third connection frame 10505 is movably connected on third
The positive left end of fixed frame 10503, the lower mechanical of the third connection frame 10505 are connected to the upper of the 4th connection frame 10506
End, the 4th fixed frame 10507 are welded in the right side of the second fixed column 10508, and the lower end of the 4th connection frame 10506 is living
Dynamic to be connected to the positive left end of the 4th fixed frame 10507, it is fixed that the lower end of second telescopic mast 10504 is slidably connected to the 4th
The right end of 10507 upper surface of frame, the radiating block 3 radiate convenient for equipment, prevent apparatus assembly from overheating, influencing equipment makes
With the working station indicator 6 learns the working condition of equipment convenient for operator.
Decelerating motor 10210 described in this patent refers to that the conglomerate of speed reducer and motor, this conglomerate generally also may be used
Referred to as gear motor or gear motor are to simplify design, saving space using the advantages of decelerating motor.
When in use, equipment is placed on suitable place by operator, equipment is then turned on, after equipment lift-off, to bridge
It being detected, opens driving motor 10115, the rotation of driving motor 10115 makes the second synchronizing wheel 10112 with rotation, and then the
Two synchronizing wheels 10112 drive third synchronizing wheel 10113 by third synchronous belt 10114, and the then rotation of first rotating shaft 10111 makes umbrella
Shape gear 10110 is with rotation, and then bevel gear 10110 drives gear turntable 10107, rotates gear turntable 10107, so
Backgear turntable 10107 drives the first fluted disc 10105 by the second synchronous belt 10106, rotates the first fluted disc 10105, and first
Fluted disc 10105 moves left and right the first rack gear 10104 with the second rack gear 10108, the first rack gear 10104 and the second rack gear 10108
Rotate first gear shaft 10102 and second gear shaft 10109, then the first synchronous belt 10101 pulls the first synchronizing wheel
10103, rotate the first synchronizing wheel 10103, the rotation of the first synchronizing wheel 10103 makes worm screw 10203 with rotation, worm screw 10203
Rotation is moved to the left matching board 10204, and the first gag lever post 10201 and the second gag lever post 10202 play the role of limit, then
First contact block 10207 is contacted with the second contact block 10208, and the small circuit of battery 10205 is switched on, and battery 10205 is as confession
Electric body is powered decelerating motor 10210, and then decelerating motor 10210 rotates, and the rotation of decelerating motor 10210 makes the 4th to synchronize
Wheel 10301 drives the first roller 10304 to make first with rotation, the 4th synchronizing wheel 10301 by the first composite sync band 10302
Roller 10304 rotates, and then the first roller 10304 rotates third roller 10316 by conveyer belt 10312, third roller
10316 rotate the 6th synchronizing wheel 10314 by third composite sync band 10315, and the rotation of the 6th synchronizing wheel 10314 makes second turn
Axis 10303 rotates, and the rotation of the second shaft 10303 rotates the 5th synchronizing wheel 10309, and then the 5th synchronizing wheel 10309 passes through the
Two composite sync bands 10310 rotate round turntable 10311, and round turntable 10311 makes the second tooth by fluted disc connecting rod 10306
Disk 10305 rotates, and the rotation of the second fluted disc 10305 rotates half fluted disc 10307, and the rotation of half fluted disc 10307 makes high-definition camera
10308, so that high-definition camera 10308 is can be carried out the shooting of multi-angle, multi-faceted detection is carried out to bridge, when equipment checks out
Bi Hou, equipment needs to drop on ground, when by falling, the first support base 10410 and 10509 elder generation of the second support base and ground
Contact, then receives impact force, moves the first fixed column 10409 up with the second fixed column 10508, the first damping spring
10401 are compressed with the second damping spring 10501, offset the impact force of a part, then the first telescopic mast 10405 is moved to the left
And compressed, the second telescopic mast 10504 moves right and is compressed, and counteracts the impact force of a part, sets to protect
The safety of slave component.
The present invention solves the equipment of the prior art when detecting to bridge, since detection process is complex, equipment
Flexibility is poor, and detection process is subject to certain restrictions, and after equipment has detected, and will receive biggish punching during landing
Power is hit, is easy that equipment is caused to damage, the present invention is combined with each other by above-mentioned component, when equipment detects bridge,
High-definition camera can keep equipment more flexible when shooting with multi-angle rotation, and convenient for the progress of shooting process, and equipment is being fallen
When ground, in place, equipment will not greatly be protected apparatus assembly by excessive shock to glissando, improve equipment entirety
Service life.
The above shows and describes the basic principles and main features of the present invention and the advantages of the present invention, for this field skill
For art personnel, it is clear that invention is not limited to the details of the above exemplary embodiments, and without departing substantially from spirit of the invention or
In the case where essential characteristic, the present invention can be realized in other specific forms.Therefore, in all respects, should all incite somebody to action
Embodiment regards exemplary as, and is non-limiting, the scope of the present invention by appended claims rather than on state
Bright restriction, it is intended that including all changes that fall within the meaning and scope of the equivalent elements of the claims in the present invention
It is interior.Any reference signs in the claims should not be construed as limiting the involved claims.
In addition, it should be understood that although this specification is described in terms of embodiments, but not each embodiment is only wrapped
Containing an independent technical solution, this description of the specification is merely for the sake of clarity, and those skilled in the art should
It considers the specification as a whole, the technical solutions in the various embodiments may also be suitably combined, forms those skilled in the art
The other embodiments being understood that.
Claims (8)
1. a kind of bridge machinery unmanned plane based on bridge security performance, structure includes that multi-angle observation and landing and buffering fill
Set (1), control panel (2), radiating block (3), the first rotating vane (4), the second rotating vane (5), working station indicator
(6), unmanned plane main body (7), blade rotor (8), third rotating vane (9), the 4th rotating vane (10), protective cover (11), photograph
Bright lamp (12), it is characterised in that:
The multi-angle observation and landing and buffering device (1) are welded in the lower end of unmanned plane main body (7), the control panel (2)
It is fixed by screws in multi-angle observation and landing and buffering device (1) positive right end, the headlamp (12) is welded in polygonal
Degree observation and landing and buffering device (1) positive left end, the control panel (2) and headlamp (12) are in same level
On, the protective cover (11) is embedded in the left surface of multi-angle observation and landing and buffering device (1), the working station indicator
(6) it is fitted in the front of unmanned plane main body (7), first rotating vane (4) is movably connected on unmanned plane main body (7) upper surface
Right front ends, second rotating vane (5) is mechanically connected to the right rear end of unmanned plane main body (7) upper surface, the third rotation
Rotating vane piece (9) is movably connected on the left back end of unmanned plane main body (7) upper surface, and the 4th rotating vane (10) is mechanically connected to
The left front end of unmanned plane main body (7) upper surface, the blade rotor (8) run through the upper surface of third rotating vane (9), and described the
Three rotating vanes (9) are identical as the 4th rotating vane (10) shape size；
The multi-angle observation and landing and buffering device (1) are by rack-driving structure (101), electric motor starting structure (102), high definition
Camera angle adjusts structure (103), the first landing and buffering structure (104), the second landing and buffering structure (105), crust of the device
(106) it forms；
The rack-driving structure (101) right end internal embedded in crust of the device (106), electric motor starting structure (102) patch
The upper end internal in crust of the device (106) is closed, the high-definition camera angle-regulation structure (103) is movably connected on crust of the device
(106) internal left end, the first landing and buffering structure (104) clearance fit lower end internal in crust of the device (106), institute
State the right end that the second landing and buffering structure (105) is fitted in the first landing and buffering structure (104).
2. a kind of bridge machinery unmanned plane based on bridge security performance according to claim 1, it is characterised in that: institute
State rack-driving structure (101) by the first synchronous belt (10101), first gear shaft (10102), the first synchronizing wheel (10103),
First rack gear (10104), the first fluted disc (10105), the second synchronous belt (10106), gear turntable (10107), the second rack gear
(10108), second gear shaft (10109), bevel gear (10110), first rotating shaft (10111), the second synchronizing wheel
(10112), third synchronizing wheel (10113), third synchronous belt (10114), driving motor (10115) composition.
3. a kind of bridge machinery unmanned plane based on bridge security performance according to claim 2, it is characterised in that: institute
The first synchronizing wheel (10103) clearance fit is stated in the middle section of the first synchronous belt (10101), first synchronous belt (10101)
Lower loop is engaged on first gear shaft around the outer ring for being connected to first gear shaft (10102), first rack gear (10104)
(10102) front end, the first rack gear (10104) clearance fit are synchronous in the lower end of the first fluted disc (10105), described first
The top ring of band (10101) around the outer ring for being connected to second gear shaft (10109), the second gear shaft (10109)
Front end and the second rack gear (10108) clearance fit, second rack gear (10108) are engaged on the upper end of the first fluted disc (10105),
The front end of first fluted disc (10105) is driven by the outer ring of the second synchronous belt (10106) and gear turntable (10107) to be connected
It connects, the bevel gear (10110) is engaged on gear turntable (10107) positive upper end, bevel gear (10110) interference
In the lower end of first rotating shaft (10111), the third synchronizing wheel (10113) is nested in the outer ring of first rotating shaft (10111) for cooperation,
Second synchronizing wheel (10112) is welded in the lower end of driving motor (10115), and second synchronizing wheel (10112) passes through the
Three synchronous belts (10114) and third synchronizing wheel (10113) are sequentially connected, second synchronizing wheel (10112) and third synchronous belt
(10114) shape size is identical.
4. a kind of bridge machinery unmanned plane based on bridge security performance according to claim 1, it is characterised in that: institute
Electric motor starting structure (102) is stated by the first gag lever post (10201), the second gag lever post (10202), worm screw (10203), matching board
(10204), battery (10205), battery retaining boards (10206), the first contact block (10207), the second contact block (10208), branch
Fagging (10209), decelerating motor (10210) composition, the left end of the worm screw (10203) and matching board (10204) clearance fit,
Second gag lever post (10202) is welded in the lower end of matching board (10204) left surface, tell the first gag lever post (10201) with
Second gag lever post (10202) is parallel to each other, and first gag lever post (10201) runs through the right surface of support plate (10209), described
First contact block (10207) glue connection is connected to the upper end of matching board (10204) left surface, the second contact block (10208) fitting
In the upper end on support plate (10209) right surface, the battery (10205) is welded in the right side of battery retaining boards (10206) lower surface
End, the decelerating motor (10210) are fixed by screws in the left end of battery retaining boards (10206) lower surface, the battery
(10205) it is in same level with decelerating motor (10210).
5. a kind of bridge machinery unmanned plane based on bridge security performance according to claim 1, it is characterised in that: institute
High-definition camera angle-regulation structure (103) is stated by the 4th synchronizing wheel (10301), the first composite sync band (10302), second turn
Axis (10303), the first roller (10304), the second fluted disc (10305), fluted disc connecting rod (10306), half fluted disc (10307), height
Clear camera (10308), the 5th synchronizing wheel (10309), the second composite sync band (10310), round turntable (10311), conveying
Band (10312), second tin roller (10313), the 6th synchronizing wheel (10314), third composite sync band (10315), third roller
(10316) it forms.
6. a kind of bridge machinery unmanned plane based on bridge security performance according to claim 5, it is characterised in that: institute
The 4th synchronizing wheel (10301) is stated to be sequentially connected by the front end of the first composite sync band (10302) and the first roller (10304),
First roller (10304) is identical as second tin roller (10313), third roller (10316) shape size, the conveyer belt
(10312) clearance fit is in the outer ring of second tin roller (10313), first roller (10304) by conveyer belt (10312) with
Third roller (10316) transmission connection, the front end of the third roller (10316) by third composite sync band (10315) with
The transmission connection of 6th synchronizing wheel (10314), the 6th synchronizing wheel (10314) are interference fitted under the second shaft (10303)
End, the 5th synchronizing wheel (10309) are nested in the outer ring of the second shaft (10303), and the 5th synchronizing wheel (10309) passes through
Second composite sync band (10310) is connect with the rear-end transmission of round turntable (10311), the fluted disc connecting rod (10306)
Lower end is movably connected on the front of round turntable (10311), and the upper mechanical of the fluted disc connecting rod (10306) is connected to second
The front of fluted disc (10305), second fluted disc (10305) are engaged on the upper right side of half fluted disc (10307), the high-definition camera
Head (10308) is welded in the left end of half fluted disc (10307).
7. a kind of bridge machinery unmanned plane based on bridge security performance according to claim 1, it is characterised in that: institute
The first landing and buffering structure (104) is stated by the first damping spring (10401), fixed plate (10402), first sleeve (10403),
One fixed frame (10404), the first telescopic mast (10405), the first connection frame (10406), the second connection frame (10407), second are consolidated
Determine frame (10408), the first fixed column (10409), the first support base (10410) composition, first sleeve (10403) welding
In the left end of fixed plate (10402) lower surface, first fixed frame (10404) is welded in the left end of first sleeve (10403),
The upper end of first telescopic mast (10405) is slidably connected to the left end of the first fixed frame (10404) lower surface, and described first connects
The upper end for connecing frame (10406) is movably connected on the first fixed frame (10404) positive right end, first connection frame (10406)
Lower end connect with the upper mechanical of the second connection frame (10407), the lower end of first telescopic mast (10405) is slidably connected to
The lower end of the left end of the second fixed frame (10408) upper surface, second connection frame (10407) is movably connected on the second fixed frame
(10408) positive right end, first fixed column (10409) are nested in the lower end of first sleeve (10403), and described first subtracts
Shake spring (10401) is welded in the upper end of the first fixed column (10409), and second fixed frame (10408) is fixed embedded in first
The left end of column (10409), first support base (10410) are welded in the lower end of the first fixed column (10409).
8. a kind of bridge machinery unmanned plane based on bridge security performance according to claim 1, it is characterised in that: institute
The second landing and buffering structure (105) is stated by the second damping spring (10501), second sleeve (10502), third fixed frame
(10503), the second telescopic mast (10504), third connection frame (10505), the 4th connection frame (10506), the 4th fixed frame
(10507), the second fixed column (10508), the second support base (10509) composition, the third fixed frame (10503) are welded in
The right side of second sleeve (10502), second fixed column (10508) are nested in the lower end of second sleeve (10502), and described
Two damping springs (10501) are welded in the upper end of the second fixed column (10508), and second support base (10509) is nested in
The upper end of the lower end of second fixed column (10508), second telescopic mast (10504) is slidably connected to third fixed frame
(10503) upper end of the right end of lower surface, the third connection frame (10505) is being movably connected on third fixed frame (10503) just
The left end in face, the lower mechanical of the third connection frame (10505) are connected to the upper end of the 4th connection frame (10506), and described
Four fixed frames (10507) are welded in the right side of the second fixed column (10508), the lower end activity of the 4th connection frame (10506)
It is connected to the 4th fixed frame (10507) positive left end, it is solid that the lower end of second telescopic mast (10504) is slidably connected to the 4th
Determine the right end of frame (10507) upper surface.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810705201.XA CN108974342A (en) | 2018-07-01 | 2018-07-01 | A kind of bridge machinery unmanned plane based on bridge security performance |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810705201.XA CN108974342A (en) | 2018-07-01 | 2018-07-01 | A kind of bridge machinery unmanned plane based on bridge security performance |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108974342A true CN108974342A (en) | 2018-12-11 |
Family
ID=64539215
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810705201.XA Withdrawn CN108974342A (en) | 2018-07-01 | 2018-07-01 | A kind of bridge machinery unmanned plane based on bridge security performance |
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| Country | Link |
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| CN (1) | CN108974342A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112878180A (en) * | 2021-04-09 | 2021-06-01 | 王国爱 | Based on unmanned aerial vehicle bridge pile foundation pore-forming detection device |
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