CN110450968A - Quick clamping bracket and its unmanned plane for engineering mapping - Google Patents

Quick clamping bracket and its unmanned plane for engineering mapping Download PDF

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Publication number
CN110450968A
CN110450968A CN201910844327.XA CN201910844327A CN110450968A CN 110450968 A CN110450968 A CN 110450968A CN 201910844327 A CN201910844327 A CN 201910844327A CN 110450968 A CN110450968 A CN 110450968A
Authority
CN
China
Prior art keywords
telescopic rod
clamping bracket
engineering mapping
bullet
quick clamping
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.)
Granted
Application number
CN201910844327.XA
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Chinese (zh)
Other versions
CN110450968B (en
Inventor
黄军荣
黄炜程
姬兵亮
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Zhongjia (guangdong) Engineering Testing Co Ltd
Original Assignee
Zhongjia (guangdong) Engineering Testing Co Ltd
Priority date (The priority date 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 date listed.)
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Publication date
Application filed by Zhongjia (guangdong) Engineering Testing Co Ltd filed Critical Zhongjia (guangdong) Engineering Testing Co Ltd
Priority to CN201910844327.XA priority Critical patent/CN110450968B/en
Publication of CN110450968A publication Critical patent/CN110450968A/en
Application granted granted Critical
Publication of CN110450968B publication Critical patent/CN110450968B/en
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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
    • 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
    • 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
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16MFRAMES, CASINGS OR BEDS OF ENGINES, MACHINES OR APPARATUS, NOT SPECIFIC TO ENGINES, MACHINES OR APPARATUS PROVIDED FOR ELSEWHERE; STANDS; SUPPORTS
    • F16M11/00Stands or trestles as supports for apparatus or articles placed thereon ; Stands for scientific apparatus such as gravitational force meters
    • F16M11/02Heads
    • F16M11/04Means for attachment of apparatus; Means allowing adjustment of the apparatus relatively to the stand
    • F16M11/041Allowing quick release of the apparatus
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16MFRAMES, CASINGS OR BEDS OF ENGINES, MACHINES OR APPARATUS, NOT SPECIFIC TO ENGINES, MACHINES OR APPARATUS PROVIDED FOR ELSEWHERE; STANDS; SUPPORTS
    • F16M13/00Other supports for positioning apparatus or articles; Means for steadying hand-held apparatus or articles
    • F16M13/02Other supports for positioning apparatus or articles; Means for steadying hand-held apparatus or articles for supporting on, or attaching to, an object, e.g. tree, gate, window-frame, cycle
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U2101/00UAVs specially adapted for particular uses or applications
    • 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)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Clamps And Clips (AREA)

Abstract

The present invention discloses a kind of Quick clamping bracket and its unmanned plane for engineering mapping.Quick clamping bracket for engineering mapping includes: support base, elastic control mechanism, clamping device.Support base includes suspension plate and the side wall set on suspension plate edge;Elastic control mechanism includes push-pull rod and bullet;Clamping device includes multiple clamp assemblies;Clamp assemblies include: sleeve, telescopic rod, gripper jaw;Sleeve is fixed on side wall, and telescopic rod is slidably socketed in sleeve, and one end of telescopic rod is held on the side of bullet, and gripper jaw is fixed on the other end of telescopic rod;Clamp assemblies further include elastic component, and elastic component is used to provide elastic force for telescopic rod, so that one end of telescopic rod is held on the side of bullet.Quick clamping bracket of the invention, it is convenient for disassembly and assembly by the way that support base, elastic control mechanism, clamping device is arranged, and stability is good.

Description

Quick clamping bracket and its unmanned plane for engineering mapping
Technical field
The present invention relates to engineering mapping technical field, more particularly to a kind of Quick clamping bracket for engineering mapping and Its unmanned plane.
Background technique
In the prior art, carry out being frequently necessary to be crossed over mountain after mountain when engineering mapping, enter woods paddle it is corresponding to on-site land survey Data, the safety of such mode one side mapping worker cannot ensure completely, and survey and draw low efficiency, the surveying and mapping data distortion factor compared with It is high.Therefore, increasingly paid attention in such a way that unmanned plane is surveyed and drawn.But existing unmanned plane is surveyed and drawn, stability The case where difference, capture apparatus falls off from body, occurs again and again, seriously affects the efficiency of mapping, and due to the frequent slave of capture apparatus Body falls off, and causes the loss damage amount of capture apparatus big, and then cause to survey and draw at high cost.In addition, in the prior art, body and bat The mounting structure for taking the photograph equipment is complicated, troublesome in poeration.
Summary of the invention
The purpose of the present invention is overcoming shortcoming in the prior art, a kind of quick-clamping for engineering mapping is provided Bracket and its unmanned plane, it is convenient for disassembly and assembly, and stability is good.
The purpose of the present invention is achieved through the following technical solutions:
A kind of Quick clamping bracket for engineering mapping, comprising: support base, elastic control mechanism, clamping device;
The support base includes suspension plate and the side wall set on the suspension plate edge;
The elastic control mechanism includes push-pull rod and bullet;The push-pull rod sliding is arranged in the plate of the suspension plate Face center, the bullet are fixed on one end of the push-pull rod;
The clamping device includes multiple clamp assemblies, and multiple clamp assemblies are with the central axis of the support base The distribution of center circular array;
The clamp assemblies include: sleeve, telescopic rod, gripper jaw;The sleeve is fixed on the side wall, described flexible Bar is slidably socketed in the sleeve, and one end of the telescopic rod is held on the side of the bullet, and the gripper jaw is solid Due to the other end of the telescopic rod;
The clamp assemblies further include elastic component, and the elastic component is used to provide elastic force for the telescopic rod, so that One end of the telescopic rod is held on the side of the bullet.
The quantity of the clamp assemblies is four in one of the embodiments,.
The bullet is tetragonous wimble structure in one of the embodiments,.
One end of the telescopic rod is equipped with sphere structure in one of the embodiments, and one end of the telescopic rod passes through The sphere structure is held on the side of the bullet.
The elastic component is spring structure in one of the embodiments,.
The elastic component is socketed on the telescopic rod in one of the embodiments, one end of the elastic component and institute It states side wall to support, the other end of the elastic component is supported with the sphere structure.
The clamp assemblies further include guiding bar in one of the embodiments, and the guiding bar is fixed on the side wall On, guide hole is offered on the gripper jaw, the guiding bar is arranged in the guide hole.
One end of the guiding bar is equipped with stop collar in one of the embodiments,.
Cushion is socketed on the body of rod of the guiding bar in one of the embodiments,.
A kind of unmanned plane further includes drone body including the above-mentioned Quick clamping bracket for engineering mapping, described Quick clamping bracket for engineering mapping is installed on the drone body.
A kind of Quick clamping bracket for engineering mapping of the invention, by setting support base, elastic control mechanism, Clamping device, it is convenient for disassembly and assembly, and stability is good.
Detailed description of the invention
In order to illustrate the technical solution of the embodiments of the present invention more clearly, below will be to needed in the embodiment attached Figure is briefly described, it should be understood that the following drawings illustrates only certain embodiments of the present invention, therefore is not construed as pair The restriction of range for those of ordinary skill in the art without creative efforts, can also be according to this A little attached drawings obtain other relevant attached drawings.
Fig. 1 is the plan view of the Quick clamping bracket for engineering mapping of one embodiment of the invention;
Fig. 2 is the perspective view of the Quick clamping bracket shown in FIG. 1 for engineering mapping;
Fig. 3 is the internal structure chart of the Quick clamping bracket shown in FIG. 1 for engineering mapping;
Fig. 4 is the structure chart of the unmanned plane of one embodiment of the invention.
Specific embodiment
To facilitate the understanding of the present invention, a more comprehensive description of the invention is given in the following sections with reference to the relevant attached drawings.In attached drawing Give better embodiment of the invention.But the invention can be realized in many different forms, however it is not limited to herein Described embodiment.On the contrary, the purpose of providing these embodiments is that making to understand more the disclosure Add thorough and comprehensive.
It should be noted that it can directly on the other element when element is referred to as " being fixed on " another element Or there may also be elements placed in the middle.When an element is considered as " connection " another element, it, which can be, is directly connected to To another element or it may be simultaneously present centering elements.Term as used herein " vertical ", " horizontal ", " left side ", " right side " and similar statement for illustrative purposes only, are not meant to be the only embodiment.
Unless otherwise defined, all technical and scientific terms used herein and belong to technical field of the invention The normally understood meaning of technical staff is identical.Term as used herein in the specification of the present invention is intended merely to description tool The purpose of the embodiment of body, it is not intended that in the limitation present invention.Term " and or " used herein includes one or more Any and all combinations of relevant listed item.
As shown in Figure 1, a kind of Quick clamping bracket 10 for engineering mapping, comprising: support base 100, elastic control Mechanism 200, clamping device 300.
As shown in Fig. 2, support base 100 includes suspension plate 110 and the side wall 120 set on 110 edge of suspension plate.In this reality It applies in example, the square plate structure of suspension plate 110, the quantity of side wall 120 is four, and four side walls 120 are distributed in outstanding respectively The edge of the four edges of hanging plate 110.
As shown in Fig. 2, elastic control mechanism 200 includes push-pull rod 210 and bullet 220.The sliding of push-pull rod 210 is arranged in The plate face center of suspension plate 110, bullet 220 are fixed on one end of push-pull rod 210.In the present embodiment, bullet 220 is four Pyramidal structure.In other embodiments, bullet 220 can also be hexagonal pyramid, eight pyramids etc., can set as the case may be It is fixed.
As shown in Fig. 2, clamping device 300 includes multiple clamp assemblies 310, multiple clamp assemblies 310 are with support base 100 Central axis be center circular array distribution.In the present embodiment, the quantity of clamp assemblies 310 is four.In other implementations In example, clamp assemblies 310 can also be six or eight, can set as the case may be.
As shown in figure 3, clamp assemblies 310 include: sleeve 311, telescopic rod 312, gripper jaw 313.Sleeve 311 is fixed on side On wall 120, telescopic rod 312 is slidably socketed in sleeve 311, and one end of telescopic rod 312 is held on the side of bullet 220, Gripper jaw 313 is fixed on the other end of telescopic rod 312.Further, one end of telescopic rod 312 is equipped with sphere structure 3121, stretches One end of contracting bar 312 is held on the side of bullet 220 by sphere structure 3121, in this way, passing through setting sphere structure 3121, one end of telescopic rod 312 can be made more smooth and slided along the side of bullet 220.
Clamp assemblies 310 further include elastic component 314 (as shown in Figure 3), and elastic component 314 is used to provide bullet for telescopic rod 312 Property power, so that one end of telescopic rod 312 is held on the side of bullet 220.In the present embodiment, elastic component 314 is bullet Spring structure, elastic component 314 are socketed on telescopic rod 312, and one end and the side wall 120 of elastic component 314 support, elastic component 314 it is another One end is supported with sphere structure 3121.Herein it is noted that elastic component 314 is in the state of compression, elastic component 314 is flexible Bar 312 provides elastic force, so that one end of telescopic rod 312 is constantly held on the side of bullet 220.
Further, clamp assemblies 310 further include guiding bar 315 (as shown in Figure 3), and guiding bar 315 is fixed on side wall On 120, guide hole 3131 (as shown in Figure 2) is offered on gripper jaw 313, guiding bar 315 is arranged in guide hole 3131.By setting Guiding bar 315 is set, gripper jaw 313 can be made to reciprocatingly slide along straight line is stable in guiding bar 315.
As shown in figure 3, one end of guiding bar 315 is equipped with stop collar 3151, stop collar 3151 is used to carry out for gripper jaw 313 Limit, prevents gripper jaw 313 to be detached from guiding bar 315 during sliding.
As shown in figure 3, being socketed with cushion 3152 on the body of rod of guiding bar 315, by the way that cushion 3152 is arranged, can subtract Light gripper jaw 313 is in the process of sliding and the impact strength of other component.
As shown in figure 4, the present invention also provides a kind of unmanned plane 20, including the above-mentioned quick-clamping branch for engineering mapping Frame 10 further includes drone body 30, and the Quick clamping bracket 10 for engineering mapping is installed on drone body 30.
The pertinent instruments of engineering mapping can be equipped on to the Quick clamping bracket 10 for being used for engineering mapping, for example, The pertinent instruments of engineering mapping can be video camera, this platform of drone body 30 then be utilized, by engineering mapping Pertinent instruments are transported to a certain designated position, to complete relevant engineering mapping work, greatly improve the efficiency of work, Reduce the working strength of mapping worker.
In the following, being illustrated to the application method of the above-mentioned Quick clamping bracket 10 for engineering mapping:
Push-pull rod 210, push-pull rod 210 and then the movement of bullet 220 of drive thereon are pushed, due to the side of bullet 220 Face is inclined surface, and during bullet 220 is mobile, bullet 220 will push the movement of telescopic rod 312, and telescopic rod 312 is in turn Gripper jaw 313 thereon is driven to move, in this way, four gripper jaws 313 will be located remotely from each other and come, four be located remotely from each other Gripper jaw 313 forms a more spacious space, thus it is possible to very easily set the clamping portion of relevant instrument of surveying and mapping Enter in this spacious space;
When the clamping portion of relevant instrument of surveying and mapping is contained in above-mentioned wide space, push-pull rod is pulled toward opposite direction 210, push-pull rod 210 drives 220 opposite direction of bullet thereon mobile in turn, under the resilient force of elastic component 314, elasticity Part 314 promotes 312 opposite direction of telescopic rod mobile, and the mobile telescopic rod 312 of opposite direction drives gripper jaw 313 to move in turn, In this way, four gripper jaws 313 will be close to each other and be gathered, then, four gripper jaws 313 mutually gathered can be incited somebody to action It blocks the clamping portion of relevant instrument of surveying and mapping, it is known that, by the clamping action of four gripper jaws 313, relevant instrument of surveying and mapping is just It can be stably fixed to the Quick clamping bracket 10 for engineering mapping.
A kind of Quick clamping bracket 10 for engineering mapping of the invention, by the way that support base 100, elastic control is arranged Mechanism 200, clamping device 300, it is convenient for disassembly and assembly, and stability is good.
The embodiments described above only express several embodiments of the present invention, and the description thereof is more specific and detailed, but simultaneously It cannot therefore be construed as limiting the scope of the patent.It should be pointed out that coming for those of ordinary skill in the art It says, without departing from the inventive concept of the premise, various modifications and improvements can be made, these belong to protection of the invention Range.Therefore, the scope of protection of the patent of the invention shall be subject to the appended claims.

Claims (10)

1. a kind of Quick clamping bracket for engineering mapping characterized by comprising support base, elastic control mechanism, folder Hold mechanism;
The support base includes suspension plate and the side wall set on the suspension plate edge;
The elastic control mechanism includes push-pull rod and bullet;The push-pull rod sliding is arranged in the plate face of the suspension plate The heart, the bullet are fixed on one end of the push-pull rod;
The clamping device includes multiple clamp assemblies, and multiple clamp assemblies are centered on the central axis of the support base Circular array distribution;
The clamp assemblies include: sleeve, telescopic rod, gripper jaw;The sleeve is fixed on the side wall, and the telescopic rod is sliding Dynamic to be socketed in the sleeve, one end of the telescopic rod is held on the side of the bullet, and the gripper jaw is fixed on The other end of the telescopic rod;
The clamp assemblies further include elastic component, and the elastic component is used to provide elastic force for the telescopic rod, so that described One end of telescopic rod is held on the side of the bullet.
2. the Quick clamping bracket according to claim 1 for engineering mapping, which is characterized in that the clamp assemblies Quantity is four.
3. the Quick clamping bracket according to claim 2 for engineering mapping, which is characterized in that the bullet is four Pyramidal structure.
4. the Quick clamping bracket according to claim 1 for engineering mapping, which is characterized in that the one of the telescopic rod End is equipped with sphere structure, and one end of the telescopic rod is held on the side of the bullet by the sphere structure.
5. the Quick clamping bracket according to claim 4 for engineering mapping, which is characterized in that the elastic component is bullet Spring structure.
6. the Quick clamping bracket according to claim 5 for engineering mapping, which is characterized in that the elastic component socket In on the telescopic rod, one end of the elastic component is supported with the side wall, the other end of the elastic component and the sphere knot Structure supports.
7. the Quick clamping bracket according to claim 1 for engineering mapping, which is characterized in that the clamp assemblies are also Including guiding bar, the guiding bar is fixed on the side wall, and guide hole is offered on the gripper jaw, and the guiding bar is worn In the guide hole.
8. the Quick clamping bracket according to claim 7 for engineering mapping, which is characterized in that the one of the guiding bar End is equipped with stop collar.
9. the Quick clamping bracket according to claim 8 for engineering mapping, which is characterized in that the bar of the guiding bar Cushion is socketed on body.
10. a kind of unmanned plane, which is characterized in that including being used for the fast of engineering mapping described in any one of claim 1 to 9 Fast clamping bracket further includes drone body, and the Quick clamping bracket for engineering mapping is installed on the unmanned plane sheet On body.
CN201910844327.XA 2019-09-06 2019-09-06 A quick clamping support and unmanned aerial vehicle for engineering survey and drawing Active CN110450968B (en)

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Application Number Priority Date Filing Date Title
CN201910844327.XA CN110450968B (en) 2019-09-06 2019-09-06 A quick clamping support and unmanned aerial vehicle for engineering survey and drawing

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Application Number Priority Date Filing Date Title
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CN110450968A true CN110450968A (en) 2019-11-15
CN110450968B CN110450968B (en) 2024-06-25

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Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111618780A (en) * 2020-05-09 2020-09-04 苏州浪潮智能科技有限公司 Tool is dismantled to CPU base backplate safety cover
CN113264189A (en) * 2021-05-31 2021-08-17 福州外语外贸学院 Commodity circulation unmanned aerial vehicle convenient to keep balance
CN113879552A (en) * 2021-11-08 2022-01-04 日照职业技术学院 Convenient fixing device of surveying instrument for unmanned aerial vehicle surveying and mapping
CN114194406A (en) * 2021-12-16 2022-03-18 江苏大学 Unmanned aerial vehicle carries on platform
CN115681401A (en) * 2022-10-27 2023-02-03 江苏仅鸿智能科技有限公司 Automatic change fixed damping mechanism of powder packagine machine base

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US20120025021A1 (en) * 2010-07-16 2012-02-02 James Jorgensen Payload door and elevator system
CN107618673A (en) * 2017-10-19 2018-01-23 河南焦傲文化传媒有限公司 A kind of unmanned plane link
CN108639343A (en) * 2018-05-03 2018-10-12 日照职业技术学院 A kind of mapping unmanned plane
JP2019035276A (en) * 2017-08-18 2019-03-07 O・T・テクノリサーチ株式会社 Bridge inspection method
CN210618490U (en) * 2019-09-06 2020-05-26 中嘉(广东)工程检测有限公司 A quick clamping support and unmanned aerial vehicle for engineering survey and drawing

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20120025021A1 (en) * 2010-07-16 2012-02-02 James Jorgensen Payload door and elevator system
JP2019035276A (en) * 2017-08-18 2019-03-07 O・T・テクノリサーチ株式会社 Bridge inspection method
CN107618673A (en) * 2017-10-19 2018-01-23 河南焦傲文化传媒有限公司 A kind of unmanned plane link
CN108639343A (en) * 2018-05-03 2018-10-12 日照职业技术学院 A kind of mapping unmanned plane
CN210618490U (en) * 2019-09-06 2020-05-26 中嘉(广东)工程检测有限公司 A quick clamping support and unmanned aerial vehicle for engineering survey and drawing

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111618780A (en) * 2020-05-09 2020-09-04 苏州浪潮智能科技有限公司 Tool is dismantled to CPU base backplate safety cover
CN113264189A (en) * 2021-05-31 2021-08-17 福州外语外贸学院 Commodity circulation unmanned aerial vehicle convenient to keep balance
CN113879552A (en) * 2021-11-08 2022-01-04 日照职业技术学院 Convenient fixing device of surveying instrument for unmanned aerial vehicle surveying and mapping
CN113879552B (en) * 2021-11-08 2023-08-04 日照职业技术学院 Convenient fixing device of surveying instrument for unmanned aerial vehicle survey and drawing
CN114194406A (en) * 2021-12-16 2022-03-18 江苏大学 Unmanned aerial vehicle carries on platform
CN114194406B (en) * 2021-12-16 2024-05-14 江苏大学 Unmanned aerial vehicle carries on platform
CN115681401A (en) * 2022-10-27 2023-02-03 江苏仅鸿智能科技有限公司 Automatic change fixed damping mechanism of powder packagine machine base
CN115681401B (en) * 2022-10-27 2024-01-02 江苏仅鸿智能科技有限公司 Automatic change fixed damping mechanism of powder packagine machine base

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