CN115123567A - Unmanned aerial vehicle nacelle for multi-view panoramic inspection - Google Patents

Unmanned aerial vehicle nacelle for multi-view panoramic inspection Download PDF

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Publication number
CN115123567A
CN115123567A CN202210837564.5A CN202210837564A CN115123567A CN 115123567 A CN115123567 A CN 115123567A CN 202210837564 A CN202210837564 A CN 202210837564A CN 115123567 A CN115123567 A CN 115123567A
Authority
CN
China
Prior art keywords
fixing plate
motor
rack
aerial vehicle
unmanned aerial
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.)
Pending
Application number
CN202210837564.5A
Other languages
Chinese (zh)
Inventor
徐硕
马振宇
杨增祥
陈琳
冯勇
蔡金涛
陈悦
厉剑雄
潘华君
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.)
State Grid Zhejiang Electric Power Co Ltd Wenling Power Supply Co
Original Assignee
State Grid Zhejiang Electric Power Co Ltd Wenling Power Supply Co
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.)
Filing date
Publication date
Application filed by State Grid Zhejiang Electric Power Co Ltd Wenling Power Supply Co filed Critical State Grid Zhejiang Electric Power Co Ltd Wenling Power Supply Co
Priority to CN202210837564.5A priority Critical patent/CN115123567A/en
Publication of CN115123567A publication Critical patent/CN115123567A/en
Pending legal-status Critical Current

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Classifications

    • 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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
    • F16F15/00—Suppression of vibrations in systems; Means or arrangements for avoiding or reducing out-of-balance forces, e.g. due to motion
    • F16F15/02—Suppression of vibrations of non-rotating, e.g. reciprocating systems; Suppression of vibrations of rotating systems by use of members not moving with the rotating systems
    • F16F15/04—Suppression of vibrations of non-rotating, e.g. reciprocating systems; Suppression of vibrations of rotating systems by use of members not moving with the rotating systems using elastic means
    • F16F15/08—Suppression of vibrations of non-rotating, e.g. reciprocating systems; Suppression of vibrations of rotating systems by use of members not moving with the rotating systems using elastic means with rubber springs ; with springs made of rubber and metal
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16M—FRAMES, CASINGS OR BEDS OF ENGINES, MACHINES OR APPARATUS, NOT SPECIFIC TO ENGINES, MACHINES OR APPARATUS PROVIDED FOR ELSEWHERE; STANDS; SUPPORTS
    • F16M11/00—Stands or trestles as supports for apparatus or articles placed thereon ; Stands for scientific apparatus such as gravitational force meters
    • F16M11/02—Heads
    • F16M11/04—Means for attachment of apparatus; Means allowing adjustment of the apparatus relatively to the stand
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16M—FRAMES, CASINGS OR BEDS OF ENGINES, MACHINES OR APPARATUS, NOT SPECIFIC TO ENGINES, MACHINES OR APPARATUS PROVIDED FOR ELSEWHERE; STANDS; SUPPORTS
    • F16M11/00—Stands or trestles as supports for apparatus or articles placed thereon ; Stands for scientific apparatus such as gravitational force meters
    • F16M11/02—Heads
    • F16M11/04—Means for attachment of apparatus; Means allowing adjustment of the apparatus relatively to the stand
    • F16M11/06—Means for attachment of apparatus; Means allowing adjustment of the apparatus relatively to the stand allowing pivoting
    • F16M11/12—Means for attachment of apparatus; Means allowing adjustment of the apparatus relatively to the stand allowing pivoting in more than one direction
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16M—FRAMES, CASINGS OR BEDS OF ENGINES, MACHINES OR APPARATUS, NOT SPECIFIC TO ENGINES, MACHINES OR APPARATUS PROVIDED FOR ELSEWHERE; STANDS; SUPPORTS
    • F16M11/00—Stands or trestles as supports for apparatus or articles placed thereon ; Stands for scientific apparatus such as gravitational force meters
    • F16M11/02—Heads
    • F16M11/18—Heads with mechanism for moving the apparatus relatively to the stand
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Physics & Mathematics (AREA)
  • Acoustics & Sound (AREA)
  • Accessories Of Cameras (AREA)

Abstract

The invention discloses an unmanned aerial vehicle nacelle for multi-view panoramic inspection, which comprises a frame and a holder unit K; the holder unit K comprises a bin inlet and outlet assembly, a damping assembly, a first rotating assembly, a second rotating assembly and a camera. The warehouse inlet and outlet assembly comprises a power mechanism, a rack, a fixed plate, a second gear, a rotating shaft, a fixed seat and a bearing seat; the power mechanism is arranged on the fixing plate and pushes the rack to slide in the rack groove; the shock absorption assembly comprises an upper fixing plate, a shock absorber and a lower fixing plate; the upper fixing plate and the lower fixing plate are respectively arranged at the upper end and the lower end of the shock absorber; the upper fixing plate is hung on the fixed seat; the first rotating assembly comprises a second motor and a supporting frame; the second rotating assembly comprises a third motor, and one end of the camera is fixed on an output shaft of the third motor while the other end is connected to the support frame in a shaft mode. The multifunctional unmanned aerial vehicle pod camera has the advantages that the cloud deck cameras in the pod can be folded and put down, the multifunctional unmanned aerial vehicle pod camera has the characteristics of multiple visual angles, shock resistance, convenience in use and the like, and the multifunctional unmanned aerial vehicle pod camera is suitable for pose adjustment of the multi-view camera of the unmanned aerial vehicle airborne pod.

Description

Unmanned aerial vehicle nacelle for multi-view panoramic inspection
Technical Field
The invention relates to the field of unmanned aerial vehicle pod, in particular to an unmanned aerial vehicle pod for multi-view panoramic inspection.
Background
In recent years, unmanned aerial vehicle wide application is taken in the aviation, topography and geomorphology reconnaissance, transmission line are patrolled and examined, and along with the rapid development of correlation technique, camera formation vision unmanned aerial vehicle system in the unmanned aerial vehicle airborne nacelle is more and more extensive in application, but current airborne nacelle multi-purpose camera can't pack up and hide.
Disclosure of Invention
The invention aims to provide an unmanned aerial vehicle nacelle for multi-view panoramic inspection, which can solve one or more of the technical problems.
In order to achieve the purpose, the technical scheme provided by the invention is as follows:
a unmanned aerial vehicle nacelle for many meshes panorama is patrolled and examined, include
A rack and pan-tilt unit K; the holder unit K comprises a bin inlet and outlet assembly, a damping assembly, a first rotating assembly, a second rotating assembly and a camera;
the warehouse in-out component comprises a power mechanism, a rack, a fixing plate, a second gear, a rotating shaft, a fixing seat and a bearing seat;
the fixing plate is arranged on the rack, a rack groove is formed in the fixing plate, and the rack is arranged in the rack groove; the power mechanism is arranged on the fixing plate and pushes the rack to slide in the rack groove;
the bearing seat is arranged on the fixed plate, the rotating shaft is arranged on the bearing seat, the second gear and the fixed seat are fixed on the rotating shaft,
the second gear is in meshed transmission with the rack, and the fixed seat rotates along with the rotating shaft to turn over;
the shock absorption assembly comprises an upper fixing plate, a shock absorber and a lower fixing plate; the upper fixing plate and the lower fixing plate are respectively arranged at the upper end and the lower end of the shock absorber; the upper fixing plate is hung on the fixing seat;
the first rotating assembly comprises a second motor and a supporting frame; the second motor is fixed on the lower fixing plate, the output shaft of the second motor is vertically downward, the supporting frame is fixed on the output shaft of the second motor,
the second rotating assembly comprises a third motor, the third motor is fixed on the support frame, an output shaft of the third motor is horizontally arranged, and one end of the camera is fixed on the output shaft of the third motor, and the other end of the camera is connected to the support frame in a shaft mode.
Preferably: the power mechanism comprises a first motor, a flange and a first gear; the first motor is mounted on the fixing plate through a flange, the first gear is mounted on an output shaft of the first motor, and the first gear is meshed with the rack.
Preferably, the following components: the holder unit K is at least provided with two groups.
The invention has the technical effects that:
the invention realizes the retraction and the putting down of a plurality of pan-tilt cameras in the nacelle through the gear rack transmission mechanism, has the characteristics of multi-view angle, shock resistance, convenient use and the like, is suitable for the pose adjustment of the multi-view camera of the airborne nacelle of the unmanned aerial vehicle, and has simple structure and easy realization.
Drawings
The accompanying drawings, which are incorporated in and constitute a part of this application, illustrate embodiments of the invention and, together with the description, serve to explain the invention and not to limit the invention.
In the drawings:
FIG. 1 is a schematic perspective view of the present invention;
fig. 2 is a schematic top view of the structure of fig. 1.
Fig. 3 is a schematic view of the cross-sectional structure a-a in fig. 2.
Fig. 4 is a left side view of the structure of fig. 2.
Fig. 5 is a schematic view of the cross-sectional structure B-B in fig. 4.
Fig. 6 is an enlarged schematic view of a portion G in fig. 5.
Fig. 7 is a left side view of the K unit in fig. 5.
Fig. 8 is a schematic perspective view of the K unit in fig. 5.
Fig. 9 is a schematic view of camera shooting down.
Fig. 10 is a schematic view of forward shooting by a camera.
Wherein the figures include the following reference numerals: frame 1, cloud platform unit K, first motor 2, flange 3, first gear 4, rack 5, fixed plate 6, second gear 7, pivot 8, fixing base 9, bearing frame 10, an upper fixed plate 11, bumper shock absorber 12, bottom plate 13, second motor 14, support frame 15, third motor 16, camera 17.
Detailed Description
The present invention will now be described in detail with reference to the drawings and specific embodiments, wherein the exemplary embodiments and descriptions are provided only for the purpose of illustrating the present invention and are not to be construed as unduly limiting the invention.
It should be noted that the embodiments and features of the embodiments in the present application may be combined with each other without conflict. The present invention will be described in detail below with reference to the accompanying drawings in conjunction with embodiments.
It is noted that the terminology used herein is for the purpose of describing particular embodiments only and is not intended to be limiting of example embodiments according to the present application. As used herein, the singular forms "a", "an" and "the" are intended to include the plural forms as well, and it should be understood that when the terms "comprises" and/or "comprising" are used in this specification, they specify the presence of stated features, steps, operations, devices, components, and/or combinations thereof, unless the context clearly indicates otherwise.
It should be noted that the terms "first," "second," and the like in the description and claims of this application and in the drawings described above are used for distinguishing between similar elements and not necessarily for describing a particular sequential or chronological order. It is to be understood that the data so used is interchangeable under appropriate circumstances such that the embodiments of the application described herein are, for example, capable of operation in sequences other than those illustrated or otherwise described herein. Furthermore, the terms "comprises," "comprising," and "having," and any variations thereof, are intended to cover a non-exclusive inclusion, such that a process, method, system, article, or apparatus that comprises a list of steps or elements is not necessarily limited to those steps or elements expressly listed, but may include other steps or elements not expressly listed or inherent to such process, method, article, or apparatus.
Spatially relative terms, such as "above … …," "above … …," "above … …," "above," and the like, may be used herein for ease of description to describe one device or feature's spatial relationship to another device or feature as illustrated in the figures. It will be understood that the spatially relative terms are intended to encompass different orientations of the device in use or operation in addition to the orientation depicted in the figures. For example, if a device in the figures is turned over, devices described as "above" or "on" other devices or configurations would then be oriented "below" or "under" the other devices or configurations. Thus, the exemplary term "above … …" can include both an orientation of "above … …" and "below … …". The device may be otherwise variously oriented (rotated 90 degrees or at other orientations) and the spatially relative descriptors used herein interpreted accordingly.
As shown in fig. 1-8, an unmanned aerial vehicle pod for multi-view panoramic inspection comprises a frame and a holder unit K; the holder unit K comprises a bin inlet and outlet assembly, a damping assembly, a first rotating assembly, a second rotating assembly and a camera. Wherein, cloud platform unit K sets up two sets at least. N group cloud platform unit K can realize multi-angle omnidirectional visual monitoring and detection.
The in-out bin assembly comprises a power mechanism, a rack 5, a fixing plate 6, a second gear 7, a rotating shaft 8, a fixing seat 9 and a bearing seat 10;
the fixing plate 6 is mounted on the rack, a rack groove is formed in the fixing plate 6, and the rack 5 is arranged in the rack groove; the power mechanism is arranged on the fixing plate 6 and pushes the rack 5 to slide in the rack groove;
the bearing seat 10 is installed on the fixing plate 6, the rotating shaft 8 is arranged on the bearing seat 10, the second gear 7 and the fixing seat 9 are fixed on the rotating shaft 8,
the second gear 7 is in meshing transmission with the rack 5, and the fixed seat 9 rotates along with the rotating shaft 8 to turn over;
the shock absorption assembly comprises an upper fixing plate 11, a shock absorber 12 and a lower fixing plate 13; the upper fixing plate 11 and the lower fixing plate 13 are respectively installed at the upper end and the lower end of the damper 12; the upper fixing plate 11 is hung on the fixing seat 9;
the first rotating assembly comprises a second motor 14 and a support frame 15; the second motor 14 is fixed on the lower fixing plate 13, the output shaft of the second motor 14 is vertically downward, the supporting frame 15 is fixed on the output shaft of the second motor 14,
the second rotating assembly comprises a third motor 16, the third motor 16 is fixed on the support frame 15, an output shaft of the third motor 16 is horizontally arranged, and one end of the camera 17 is fixed on the output shaft of the third motor 16, and the other end of the camera 17 is connected to the support frame 15 in a shaft mode.
In the invention, the power mechanism can be a motor gear for pushing a rack, and can also be a cylinder for pushing the rack to slide, without limitation.
Here, the rack 5 pushes the second gear 7 to rotate so as to drive the fixing seat 9 to rotate along with the rotating shaft 8, and the bin inlet and outlet actions of the holder unit K can be realized.
Then, the second motor 14 and the third motor 16 drive the camera 17 to rotate up and down, left and right to adjust the pose of the camera 17, so that the multi-view all-shooting, the landform survey, the power transmission line inspection and the like are realized.
In the course of the work, camera 17 job stabilization is guaranteed all the time to bumper shock absorber 12, avoids causing because unmanned aerial vehicle's shake and shoots the failure.
In some embodiments, shock absorber 12 may be, without limitation, a rubber ball or other commercially available product.
In this embodiment, a specific power mechanism is provided, where the power mechanism includes a first motor 2, a flange 3, and a first gear 4; the first motor 2 is mounted on the fixing plate 6 through a flange 3, the first gear 4 is mounted on an output shaft of the first motor 2, and the first gear 4 is meshed with the rack 5.
The above description is only a preferred embodiment of the present invention and is not intended to limit the present invention, and various modifications and changes may be made by those skilled in the art. Any modification, equivalent replacement, or improvement made within the spirit and principle of the present invention should be included in the protection scope of the present invention.

Claims (3)

1. The utility model provides an unmanned aerial vehicle nacelle for many meshes panorama is patrolled and examined which characterized in that: comprises that
A rack and pan-tilt unit K; the holder unit K comprises a bin inlet and outlet assembly, a damping assembly, a first rotating assembly, a second rotating assembly and a camera;
the in-out bin assembly comprises a power mechanism, a rack (5), a fixing plate (6), a second gear (7), a rotating shaft (8), a fixing seat (9) and a bearing seat (10);
the fixing plate (6) is mounted on the rack, a rack groove is formed in the fixing plate (6), and the rack (5) is arranged in the rack groove; the power mechanism is arranged on the fixing plate (6) and pushes the rack (5) to slide in the rack groove;
the bearing seat (10) is mounted on the fixing plate (6), the rotating shaft (8) is arranged on the bearing seat (10), the second gear (7) and the fixing seat (9) are fixed on the rotating shaft (8), the second gear (7) is in meshing transmission with the rack (5), and the fixing seat (9) rotates along with the rotating shaft (8) to turn over;
the shock absorption assembly comprises an upper fixing plate (11), a shock absorber (12) and a lower fixing plate (13); the upper fixing plate (11) and the lower fixing plate (13) are respectively arranged at the upper end and the lower end of the shock absorber (12); the upper fixing plate (11) is hung on the fixed seat (9);
the first rotating assembly comprises a second motor (14) and a support frame (15); the second motor (14) is fixed on the lower fixing plate (13), the output shaft of the second motor (14) is vertically downward, the supporting frame (15) is fixed on the output shaft of the second motor (14),
the second rotating assembly comprises a third motor (16), the third motor (16) is fixed on the support frame (15), an output shaft of the third motor (16) is horizontally arranged, and one end of the camera (17) is fixed on the output shaft of the third motor (16) and the other end of the camera is connected to the support frame (15) in a shaft mode.
2. The unmanned aerial vehicle pod for multi-purpose panoramic inspection according to claim 1, wherein: the power mechanism comprises a first motor (2), a flange (3) and a first gear (4); the first motor (2) is mounted on the fixing plate (6) through a flange (3), the first gear (4) is mounted on an output shaft of the first motor (2), and the first gear (4) is meshed with the rack (5).
3. The unmanned aerial vehicle pod for multi-purpose panoramic inspection according to claim 1, wherein: the holder unit K is at least provided with two groups.
CN202210837564.5A 2022-07-15 2022-07-15 Unmanned aerial vehicle nacelle for multi-view panoramic inspection Pending CN115123567A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202210837564.5A CN115123567A (en) 2022-07-15 2022-07-15 Unmanned aerial vehicle nacelle for multi-view panoramic inspection

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202210837564.5A CN115123567A (en) 2022-07-15 2022-07-15 Unmanned aerial vehicle nacelle for multi-view panoramic inspection

Publications (1)

Publication Number Publication Date
CN115123567A true CN115123567A (en) 2022-09-30

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ID=83383077

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202210837564.5A Pending CN115123567A (en) 2022-07-15 2022-07-15 Unmanned aerial vehicle nacelle for multi-view panoramic inspection

Country Status (1)

Country Link
CN (1) CN115123567A (en)

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