CN209921633U - Unmanned aerial vehicle assembly every single move adjusts structure - Google Patents
Unmanned aerial vehicle assembly every single move adjusts structure Download PDFInfo
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- CN209921633U CN209921633U CN201920353128.4U CN201920353128U CN209921633U CN 209921633 U CN209921633 U CN 209921633U CN 201920353128 U CN201920353128 U CN 201920353128U CN 209921633 U CN209921633 U CN 209921633U
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Abstract
The utility model discloses an unmanned aerial vehicle assembly every single move adjusts structure relates to the mechanical equipment field of making. The pitching device comprises a pitching base, a pitching rail and a rectangular frame, wherein the pitching base supports the pitching rail through a triangular support assembly, universal wheels are arranged at four corners of the bottom of the pitching base, and the rectangular frame is supported on the pitching rail; the pitching base and the rectangular frame are both rectangular structures consisting of long and short rod-shaped components, through grooves with the same shape are formed in the four side faces of each rod-shaped component, and a cylindrical channel penetrates through the central axis of each rod-shaped component; the bottom end of the triangular support component is fixed on the pitching base through a bolt structure, a pulley is clamped at the top end of the triangular support component, and the pitching rail is connected with the pulley support; a horizontally fixed rectangular plate is arranged at the end of the pitching rail; and the rectangular plate is fixedly supported by the rectangular frame.
Description
Technical Field
The utility model relates to a mechanical equipment makes the field, in particular to structure is adjusted in unmanned aerial vehicle assembly every single move.
Background
The fixed wing aircraft can replace people to accomplish aerial work, improves work efficiency, liberates the labour, and its application in the field of electric power patrols line, forest fire prevention, fire control, security protection is constantly growing. The main lift of the fixed-wing aircraft comes from the relative motion of the wings and the air, so the fixed-wing aircraft has to have a certain relative speed without air to fly with the lift.
The aircraft need inspect connecting portion after finishing production, and traditional fixed inspection mode is humanized, and can't detect out whether complete balance of aircraft is whole.
Disclosure of Invention
The utility model aims to provide a: the utility model provides an unmanned aerial vehicle assembles every single move and adjusts structure supports fixed every single move track through the triangular supports subassembly to through the spacing cooperation between triangular supports subassembly and the every single move track, make the every single move track can carry out the every single move operation along the slip direction of pulley. The triangular support component is formed by combining a support frame A, a support frame B, a bolt structure and a pulley, is suitable for large-scale production and processing, and is convenient to install, material-saving and light in weight. The junction of shaft-like part adopts triangle fastener and right angle fastener to carry out fixed connection, and stability is high, can prevent that the junction from taking place deformation, and simple installation.
The utility model adopts the technical scheme as follows:
an unmanned aerial vehicle assembly pitching adjusting structure comprises a pitching base, a pitching rail and a rectangular frame, wherein the pitching rail is supported on the pitching base through a triangular support assembly, universal wheels are arranged at four corners of the bottom of the pitching base, and the rectangular frame is supported on the pitching rail; the pitching base and the rectangular frame are both rectangular structures consisting of long and short rod-shaped components, through grooves with the same shape are formed in the four side faces of each rod-shaped component, and a cylindrical channel penetrates through the central axis of each rod-shaped component; the bottom end of the triangular support component is fixed on the pitching base through a bolt structure, a pulley is clamped at the top end of the triangular support component, and the pitching rail is connected with the pulley support; a horizontally fixed rectangular plate is arranged at the end of the pitching rail; and the rectangular plate is fixedly supported by the rectangular frame.
The utility model provides a structure is adjusted in every single move suitable for unmanned aerial vehicle every single move assembly that rolls supports fixed every single move track through triangular supports subassembly to through the spacing cooperation between triangular supports subassembly and the every single move track, make the every single move track can carry out the every single move operation along the slip direction of pulley. Be equipped with a logical groove that runs through on the support frame B, be equipped with the logical groove that a plurality of runs through on the every single move track, because the every single move track is circular-arc, then slides on the triangular supports subassembly along with the every single move track, always has logical groove and the logical groove coincidence on the support frame B on the every single move track in the horizontal direction, so lead to the inslot and can wear to insert the gag lever post for the orbital position of fixed every single move.
Further, the triangular support component comprises a support frame A and a support frame B, and in the vertical direction, the height of the support frame B is larger than that of the support frame A.
The utility model discloses a support frame A and support frame B support every single move base and every single move track to be connected, and specific support mode does, and during circular-arc every single move track passed support frame B, erect in support frame A and on, support frame A and the pulley groove top of hugging closely support frame A and along the lower border of every single move track promptly, and support frame B's pulley groove's below is hugged closely along the last border of every single move track. The utility model discloses a triangular supports subassembly is formed by support frame A, support frame B, bolt structure, pulley combination, and its suitable large-scale production processing, and simple to operate, the material province, the quality is light.
Furthermore, the pitching track is composed of arc-shaped plates which are parallel in the horizontal direction, and a cross rod is connected between the arc-shaped plates; the pitching rail is also provided with a plurality of through holes which horizontally penetrate through the pitching rail, and the through holes are axially symmetrical in the vertical direction by taking the central axis of the pitching rail as an axis.
The pitching rail of the utility model comprises a plurality of through holes, wherein the annular hole consists of two semicircles and a rectangle, which is used for reducing the overall mass of the pitching rail and reducing production materials; the diameter of the circular hole A is equal to that of a semicircle on the annular hole, and the circular hole A is used for supplementing when the diameter of the circular hole A is not enough to arrange another annular hole; the circular hole B is matched with a bolt on the support frame B and used for fixing the inclined position of the arc-shaped support piece.
Further, the pitch base comprises two long rod parts and at least two short rod parts.
The utility model discloses a every single move base is except the frame construction who comprises two stock parts and two short rod parts, frame construction is last, and the axis department of perpendicular to stock part still is provided with a short rod part, can further stabilize every single move base to improve its stability, prevent that rectangular frame from taking place deformation.
The triangular fastener is in a triangular prism shape, and the height of the triangular fastener is equal to that of the rod-shaped component; the triangular fastener also comprises a triangular prism-shaped inner space.
Further, the triangular fastener is arranged at the vertical connection position of the rod-shaped component.
At least two triangular fasteners are arranged at the vertical joint of each rod-shaped component. The connecting mode of long rod part and short rod part in every single move base is, and two long rod parts are placed in parallel, and two short rod parts are respectively clamped at the two ends of long rod part, namely the end of short rod part, and are supported at the tail end of the side face of long rod part. Because the cross sections of the long rod part and the short rod part are the same and are square, the vertical connection part of one rod-shaped part can be stably fixed only by two triangular fasteners.
The rectangular fastener is formed by splicing two rectangular plates and one square plate into a right-angle shape, and the width of the rectangular fastener is equal to that of the rod-shaped part.
Further, the right-angle fastener is arranged on the top of the joint of the rectangular frame.
To sum up, owing to adopted above-mentioned technical scheme, the beneficial effects of the utility model are that:
1. the utility model relates to an unmanned aerial vehicle assembles every single move and adjusts structure supports fixed every single move track through the triangular supports subassembly to through the spacing cooperation between triangular supports subassembly and the every single move track, make the every single move track can carry out the every single move operation along the slip direction of pulley.
2. The utility model relates to an unmanned aerial vehicle assembly every single move adjusts structure, triangular supports subassembly is formed by support frame A, support frame B, bolt structure, pulley combination, and its suitable large-scale production processing, and simple to operate uses the material to economize, and the quality is light.
3. The utility model relates to an unmanned aerial vehicle assembles every single move and adjusts structure, the junction of shaft-like part adopts triangle fastener and right angle fastener to carry out fixed connection, and stability is high, can prevent that the junction from taking place deformation, and simple installation.
Drawings
The invention will now be described, by way of example, with reference to the accompanying drawings, in which:
fig. 1 is a schematic view of the present invention;
fig. 2 is a front view of the present invention;
FIG. 3 is a schematic view of the rod-like member and triangular support assembly of the present invention;
in the figure, 1-pitching base, 11-rod-shaped part, 12-through groove, 13-cylindrical channel, 2-triangular support component, 21-support frame A, 22-support frame B, 23-pulley, 3-pitching track, 31-rectangular plate, 32-cross bar, 33-through hole, 4-rectangular frame, 5-universal wheel, 6-triangular fastener and 7-right-angle fastener.
Detailed Description
All of the features disclosed in this specification, or all of the steps in any method or process so disclosed, may be combined in any combination, except combinations of features and/or steps that are mutually exclusive.
It is noted that relational terms such as "first" and "second," and the like, may be used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions. Also, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus. Without further limitation, an element defined by the phrase "comprising an … …" does not exclude the presence of other identical elements in a process, method, article, or apparatus that comprises the element.
The present invention will be described in detail with reference to fig. 1, 2 and 3.
Example 1
An unmanned aerial vehicle assembly pitching adjusting structure is shown in fig. 1, fig. 2 and fig. 3, and comprises a pitching base 1, a pitching rail 3 and a rectangular frame 4, wherein the pitching base 1 supports the pitching rail 3 through a triangular support component 2, four corners of the bottom of the pitching base 1 are provided with universal wheels 5, and the rectangular frame 4 is supported on the pitching rail 3; the pitching base 1 and the rectangular frame 4 are both rectangular structures consisting of long and short rod-shaped components 11, through grooves 12 with the same shape are arranged on the four side faces of the rod-shaped components 11, and a cylindrical channel 13 penetrates through the central axis of the rod-shaped components 11; the bottom end of the triangular support component 2 is fixed on the pitching base 1 through a bolt structure, a pulley 23 is clamped at the top end of the triangular support component, and the pitching rail 3 is in supporting connection with the pulley 23; a horizontally fixed rectangular plate 31 is arranged at the end of the pitching rail 3; the rectangular plate 31 supports and fixes the rectangular frame 4.
The utility model provides a structure is adjusted in every single move suitable for unmanned aerial vehicle every single move assembly that rolls supports fixed every single move track 3 through triangular supports subassembly 2 to through the spacing cooperation between triangular supports subassembly 2 and the every single move track 3, make every single move track 3 can carry out the every single move operation along the slip direction of pulley 23. Be equipped with a logical groove that runs through on the support frame B22, be equipped with the logical groove that a plurality of runs through on the every single move track 3, because every single move track 3 is circular-arcly, then along with every single move track 3 slides on triangular supports subassembly 2, always has logical groove and the logical groove coincidence on the support frame B22 on the every single move track 3 in the horizontal direction, so lead to the inslot and can wear to insert the gag lever post for the orbital position of fixed every single move.
Example 2
The present embodiment is different from embodiment 1 in that the triangular support assembly 2 comprises a support bracket a21 and a support bracket B22, and the height of the support bracket B22 is greater than that of the support bracket a21 in the vertical direction.
The utility model discloses a support frame A21 and support frame B22 support every single move base 1 and every single move track 3 and be connected, and specific support mode does, and in circular-arc every single move track 3 passed support frame B22, erect in support frame A21 and last, the pulley groove top of support frame A21 and was hugged closely to the lower border of every single move track 3 promptly, and the below of the pulley groove of support frame B22 is hugged closely to the last border of every single move track 3. The utility model discloses a triangular supports subassembly 2 is formed by support frame A21, support frame B22, bolt structure, the combination of pulley 23, and its suitable large-scale production processing, and simple to operate, and the material province, the quality is light.
Example 3
The difference between the embodiment and embodiment 1 is that the pitching rail 3 is composed of arc-shaped plates parallel in the horizontal direction, and a cross bar 32 is connected between the arc-shaped plates; the pitching rail 3 is further provided with a plurality of through holes 33 which horizontally penetrate through the pitching rail 3, and the through holes 33 are axially symmetrical in the vertical direction by taking the central axis of the pitching rail 3 as an axis.
The pitching rail 3 of the utility model comprises a plurality of through holes 33, wherein the annular hole consists of two semicircles and a rectangle, which is used for reducing the overall quality of the pitching rail and reducing production materials; the diameter of the circular hole A is equal to that of a semicircle on the annular hole, and the circular hole A is used for supplementing when the diameter of the circular hole A is not enough to arrange another annular hole; the through groove is matched with the through groove on the support frame B22 by a bolt for fixing the inclined position of the arc-shaped support piece.
Example 4
The present embodiment is different from embodiment 1 in that the pitch base 1 includes two long pole parts and at least two short pole parts.
The utility model discloses a every single move base 1 is except the frame construction who comprises two stock parts and two short rod parts, frame construction is last, and the axis department of perpendicular to stock part still is provided with a short rod part, can carry out further firm with every single move base 1 to improve its stability, prevent that rectangular frame 4 from taking place deformation.
Example 5
The present embodiment is different from embodiment 1 in that the present embodiment further includes a triangular fastener 6, the triangular fastener 6 is triangular prism-shaped, and the height of the triangular fastener 6 is equal to the height of the rod-shaped member 11; the triangular fastener 6 also includes a triangular prism-like interior space therein.
The triangular fastener 6 is disposed at a vertical junction of the rod-like member 11.
At least two triangular fasteners 6 are arranged at the vertical joint of each rod-shaped part 11. The connecting mode of long rod part and quarter butt part does in every single move base 1, and two long rod parts parallel placement, two quarter butt parts clamp respectively in the both ends of long rod part, and the end of quarter butt part supports in the end of the side of long rod part promptly. Since the long rod member and the short rod member have the same cross section and are square, only two triangular fasteners 6 are needed to stably fix the vertical connection of one rod-shaped member 11.
Example 6
The difference between the embodiment and the embodiment 1 is that the invention further comprises a right-angle fastener 7, wherein the right-angle fastener 7 is formed by splicing two rectangular plates and one square plate into a right-angle shape, and the width of the right-angle fastener 7 is equal to that of the rod-shaped part 11.
The right-angle fastener 7 is arranged on the top of the joint of the rectangular frame 4.
The above description is only for the preferred embodiment of the present invention, but the protection scope of the present invention is not limited thereto, and any person skilled in the art can be covered within the protection scope of the present invention without the changes or substitutions conceived by the inventive work within the technical scope disclosed by the present invention. Therefore, the protection scope of the present invention should be subject to the protection scope defined by the claims.
Claims (8)
1. The utility model provides an unmanned aerial vehicle assembles every single move and adjusts structure which characterized in that: the pitching device comprises a pitching base (1), a pitching track (3) and a rectangular frame (4), wherein the pitching track (3) is supported on the pitching base (1) through a triangular support component (2), universal wheels (5) are arranged at four corners of the bottom of the pitching base (1), and the rectangular frame (4) is supported on the pitching track (3); the pitching base (1) and the rectangular frame (4) are both rectangular structures consisting of long and short rod-shaped parts (11), through grooves (12) with the same shape are formed in the four side faces of the rod-shaped parts (11), and cylindrical channels (13) penetrate through the central axis of the rod-shaped parts (11); the bottom end of the triangular support component (2) is fixed on the pitching base (1) through a bolt structure, a pulley (23) is clamped at the top end of the triangular support component, and the pitching rail (3) is in supporting connection with the pulley (23); a horizontally fixed rectangular plate (31) is arranged at the end of the pitching rail (3); and the rectangular frame (4) is supported and fixed on the rectangular plate (31).
2. The unmanned aerial vehicle mounting pitch adjustment structure of claim 1, wherein: the triangular support component (2) comprises a support frame A (21) and a support frame B (22), and in the vertical direction, the height of the support frame B (22) is larger than that of the support frame A (21).
3. The unmanned aerial vehicle mounting pitch adjustment structure of claim 1, wherein: the pitching rail (3) is composed of arc-shaped plates which are parallel in the horizontal direction, and a cross rod (32) is connected between the arc-shaped plates; the pitching rail (3) is further provided with a plurality of through holes (33) which horizontally penetrate through the pitching rail (3), and the through holes (33) are axially symmetrical in the vertical direction by using the central axis of the pitching rail (3).
4. The unmanned aerial vehicle mounting pitch adjustment structure of claim 1, wherein: the pitch base (1) comprises two long pole parts and at least two short pole parts.
5. The unmanned aerial vehicle mounting pitch adjustment structure of claim 1, wherein: the triangular fastening piece (6) is triangular prism-shaped, and the height of the triangular fastening piece (6) is equal to that of the rod-shaped component (11); the triangular fastener (6) also comprises a triangular prism-shaped inner space.
6. The unmanned aerial vehicle mounting pitch adjustment structure of claim 5, wherein: the triangular fastener (6) is arranged at the vertical connection position of the rod-shaped component (11).
7. The unmanned aerial vehicle mounting pitch adjustment structure of claim 1, wherein: the novel steel plate bending machine is characterized by further comprising a right-angle fastener (7), wherein the right-angle fastener (7) is formed by splicing two rectangular plates and one square plate into a right-angle shape, and the width of the right-angle fastener (7) is equal to that of the rod-shaped component (11).
8. The unmanned aerial vehicle mounting pitch adjustment structure of claim 7, wherein: the right-angle fastener (7) is arranged at the top of the joint of the rectangular frame (4).
Priority Applications (1)
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CN201920353128.4U CN209921633U (en) | 2019-03-20 | 2019-03-20 | Unmanned aerial vehicle assembly every single move adjusts structure |
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CN201920353128.4U CN209921633U (en) | 2019-03-20 | 2019-03-20 | Unmanned aerial vehicle assembly every single move adjusts structure |
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CN209921633U true CN209921633U (en) | 2020-01-10 |
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