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 PDF

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Publication number
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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CN
China
Prior art keywords
synchronizing wheel
landing
unmanned plane
fluted disc
bridge
Prior art date
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Withdrawn
Application number
CN201810705201.XA
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Chinese (zh)
Inventor
庄明忠
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Individual
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Individual
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Publication date
Application filed by Individual filed Critical Individual
Priority to CN201810705201.XA priority Critical patent/CN108974342A/en
Publication of CN108974342A publication Critical patent/CN108974342A/en
Withdrawn legal-status Critical Current

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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/04Helicopters
    • B64C27/08Helicopters with two or more rotors
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C25/00Alighting gear
    • B64C25/32Alighting gear characterised by elements which contact the ground or similar surface 
    • B64C25/58Arrangements or adaptations of shock-absorbers or springs
    • B64C25/62Spring shock-absorbers; Springs
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D47/00Equipment not otherwise provided for
    • B64D47/08Arrangements of cameras
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U10/00Type of UAV
    • B64U10/10Rotorcrafts
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U30/00Means for producing lift; Empennages; Arrangements thereof
    • B64U30/20Rotors; Rotor supports
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U50/00Propulsion; Power supply
    • B64U50/10Propulsion
    • B64U50/19Propulsion using electrically powered motors
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U2101/00UAVs specially adapted for particular uses or applications
    • B64U2101/30UAVs specially adapted for particular uses or applications for imaging, photography or videography

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  • 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

A kind of bridge machinery unmanned plane based on bridge security performance
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.
CN201810705201.XA 2018-07-01 2018-07-01 A kind of bridge machinery unmanned plane based on bridge security performance Withdrawn CN108974342A (en)

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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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CN204998766U (en) * 2015-09-25 2016-01-27 浙江海洋学院 Aircraft
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