CN209921637U - A device for unmanned aerial vehicle every single move assembly that rolls - Google Patents

Abstract

The utility model discloses a device for unmanned aerial vehicle rolling pitching assembly, including a pitching base, a pitching track, a rolling support seat and a rolling fixing frame, a triangular support component is fixed on the long edge of the pitching base through a bolt, and the top end of the triangular support component is movably connected with a first roller wheel, the pitching track is movably connected with the first roller wheel; a rectangular plate is fixed on the end face of the pitching rail, the rolling support seat is fixed on the rectangular plate through a bolt, a rolling support frame is fixed on the short edge of the rolling support seat through a bolt, and a second roller is movably connected onto the rolling support frame; the fixed frame that rolls includes the auxiliary rod and can dismantle two circular shape cardboard that roll of connection at the auxiliary rod both ends, the cardboard that rolls passes through second gyro wheel swing joint on the top of the support frame that rolls. The utility model discloses stable in structure, effectual simulation unmanned aerial vehicle side flies, various flight attitudes such as upset, every single move, is convenient for verify top data.

Description

A device for unmanned aerial vehicle every single move assembly that rolls

Technical Field

The utility model relates to an unmanned aerial vehicle field, concretely relates to a device that is used for unmanned aerial vehicle every single move assembly that rolls.

Background

A drone is an unmanned aircraft that is operated by a radio remote control device and a self-contained program control device. The machine has no cockpit, but is provided with an automatic pilot, a program control device and other equipment. The personnel on the ground, the naval vessel or the mother aircraft remote control station can track, position, remotely control, telemeter and digitally transmit the personnel through equipment such as a radar. The aircraft can take off like a common airplane under the radio remote control or launch and lift off by a boosting rocket, and can also be thrown into the air by a mother aircraft for flying. During recovery, the aircraft can land automatically in the same way as the common aircraft landing process, and can also be recovered by a parachute or a barrier net for remote control. Can be repeatedly used for many times. The method is widely used for aerial reconnaissance, monitoring, communication, anti-submergence, electronic interference and the like.

Unmanned aerial vehicle can replace people to accomplish aerial work, improves work efficiency, liberation labour, and its application in the field of electric power patrols line, forest fire prevention, fire control, security protection constantly increases. Unmanned aerial vehicle need carry out the simulation test before putting into service, simulation unmanned aerial vehicle flight attitude and verification top data etc. and current simulation testing arrangement is deficient relatively, can not effectual simulation unmanned aerial vehicle side fly, various flight attitudes such as upset, every single move, and single structure, stability is not good.

SUMMERY OF THE UTILITY MODEL

The utility model aims to provide a: the utility model provides a device that is used for unmanned aerial vehicle every single move assembly that rolls, from supreme every single move base that has set gradually down, every single move track, the supporting seat that rolls and the mount that rolls, support every single move track and the mount that rolls, through the flight of every single move track simulation aircraft every single move, through the mount that rolls simulation unmanned aerial vehicle side of simulation fly, upset etc. to solve current emulation testing arrangement and can not fly by effectual simulation unmanned aerial vehicle side, various flight attitudes such as upset, every single move, and single structure, the not good problem of stability.

The utility model adopts the technical scheme as follows:

the utility model relates to a device for unmanned aerial vehicle every single move assembly that rolls, including every single move base, every single move track, the supporting seat that rolls and the mount that rolls, every single move base and the supporting seat that rolls are the rectangle frame, there is the triangular support subassembly through the bolt fastening on the long limit of every single move base, and the top swing joint of triangular support subassembly has first gyro wheel, every single move track and first gyro wheel swing joint, the every single move base supports the every single move track through the triangular support subassembly, and the every single move track is perpendicular to the plane that the every single move base is located and can roll along the long limit direction of every single move base; a rectangular plate is fixed on the end face of the pitching rail, the rolling support seat is fixed on the rectangular plate through a bolt, the long edge of the rolling support seat is opposite to the long edge of the pitching base, the short edge of the rolling support seat is parallel to the short edge of the pitching base, a rolling support frame is fixed on the short edge of the rolling support seat through a bolt, and a second roller is movably connected onto the rolling support frame; the mount that rolls includes the auxiliary rod and can dismantle two circular shape cardboards that roll of connection at the auxiliary rod both ends, the cardboard that rolls passes through second gyro wheel swing joint on the top of the support frame that rolls to support through the support frame that rolls, two cardboard perpendicular to that roll the plane at supporting seat place, and the projection can roll along the minor face direction of the supporting seat that rolls on the minor face of supporting seat that rolls.

The existing simulation test device can not effectively simulate various flight attitudes such as unmanned aerial vehicle side flight, overturning, pitching and the like, and has single structure and poor stability. The utility model comprises a pitching base, a pitching rail, a rolling support seat and a rolling fixing frame, wherein the pitching base and the rolling support seat are rectangular frames, there is triangular support assembly on the long limit of every single move base through bolt fixed mounting, every single move base has two long limits, two long limit last triangular support assembly mutual symmetry parallel, triangular support assembly's top swing joint has first gyro wheel, the every single move track is through first gyro wheel movable mounting on triangular support assembly, triangular support assembly is used for supporting the every single move track, every single move base passes through triangular support assembly and realizes the support to the every single move track, the every single move track is symmetrical with the ascending axis in vertical direction when being in level, through being fixed with rectangular panel on the orbital terminal surface of every single move, the supporting seat that rolls passes through the bolt fastening on rectangular panel, make the every single move track to roll the supporting seat and stabilize and support, the supporting seat that rolls realizes the every single move along with the every single move track rolls. The utility model discloses there is the support frame that rolls through bolt fixed mounting on the minor face of supporting seat that rolls, swing joint has the second gyro wheel on the support frame that rolls, two cardboard swing joint that roll of mount are on the second gyro wheel, the support frame that rolls is to rolling the cardboard support with the support frame that rolls, the cardboard that rolls passes through the upset of second gyro wheel, unmanned aerial vehicle's aircraft nose and tail are arranged in respectively on two cardboards that roll of the mount that roll, the cardboard that rolls rotates, unmanned aerial vehicle is along with the cardboard upset that rolls, and, roll and realize the every single move flight gesture about the every single move track, effectively simulate unmanned aerial vehicle flight, be convenient for verify the top data.

Furthermore, each side of the pitching base and the rolling support seat is a square steel tube, through grooves along the length direction are formed in four side faces of the square steel tube, and a cylindrical channel coincident with the central axis is further formed in the square steel tube. By adopting the structure, the through grooves on the long rod and the short rod are convenient for installing bolts, so that various supporting assemblies and connecting pieces can be fixed, the optional positions of the through grooves on the long rod and the short rod can be installed, bolt holes do not need to be formed, the triangular supporting assemblies and the rolling supporting frame can be conveniently adjusted in the installing position, and the device is simple and convenient.

Furthermore, a right-angle connecting piece and a right-angle fastener are further arranged at the joint of the square steel pipe. Adopt above-mentioned structure, right angle connection spare is used for connecting each square steel pipe, makes every single move base and each limit of the supporting seat of rolling connect perpendicularly, and right angle fastener is right angled triangle's triangular prism for the cross section, and right angle fastener passes through the bolt and installs the inboard at the rectangle frame, and two cylinders of right angle fastener are hugged closely to the rectangle frame medial surface, make right angle fastener's right angle and the right angle coincidence of rectangle frame to consolidate the perpendicular connection between the square steel pipe.

Furthermore, a fixing rod which is vertically connected with the long edge is further arranged on the pitching base. By adopting the structure, the fixed rod can strengthen the stability of the pitching base.

Further, the pitching rail comprises two parallel arc-shaped plates in the horizontal direction, and a cross rod is connected between the two 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 axisymmetric with the central axis of the pitching rail in the vertical direction. By adopting the structure, the pitching rail formed by the two arc-shaped plates can roll through the first roller, and the two rolling clamping plates can roll in parallel and synchronously under the connection action of the cross rod; the through holes on the pitching rails can reduce the weight of the pitching rails and reduce the material cost for manufacturing the device.

Furthermore, the triangular support assembly comprises a support frame A and a support frame B, in the vertical direction, the height of the support frame B is greater than that of the support frame A, two support frames B are arranged on two sides of the support frame A, a first roller on the support frame A is positioned above the pitching rail, and a first roller of the support frame B is positioned below the pitching rail; the support frame A is also provided with a first positioning rod. By adopting the structure, the pitching rail is clamped between the first rollers of the support frame A and the two support frames B, so that the pitching rail is conveniently supported by the triangular support assembly, and the rolling stability of the pitching rail and the overall uniformity of the simulated flight device are improved; when needs location every single move track, make unmanned aerial vehicle keep certain every single move gesture, be provided with the locating hole that matches with first locating lever on the support frame A, utilize first locating lever to run through support frame A and every single move track, can fix a position every single move track, stop the roll.

Further, the screens hole that is used for fixed unmanned aerial vehicle is all seted up at the center of two cardboards that roll, and the axis level coincidence in two cardboard and the screens hole that rolls, the cardboard that rolls crosses face diameter etc. and divide into two semicircle cardboards, and the contact site of two semicircle cardboards is provided with the lug and the recess of mutual matching respectively to the contact site of two semicircle cardboards all is provided with fastener along axial both ends. Adopt above-mentioned structure, open fastener, part two semicircle cardboards, it is downthehole to arrange the screens of the cardboard that rolls respectively in unmanned aerial vehicle's aircraft nose and tail, and two semicircle cardboards pass through the lug and merge together with the recess, block unmanned aerial vehicle to it is fixed through fastener, realize fixed to unmanned aerial vehicle, the cardboard that is convenient for roll rolls on the second gyro wheel.

Further, still including fixing the locating support on the supporting seat that rolls, be provided with the second locating lever on the locating support, be provided with the locating hole that matches with the second locating lever on the cardboard that rolls. Adopt above-mentioned structure, when needs location cardboard that rolls, make unmanned aerial vehicle keep certain posture of turning on one's side, roll and be provided with the locating hole that matches with the second locating lever on the cardboard, utilize the second locating lever to run through locating support and the cardboard that rolls, can stop the cardboard location that rolls.

Furthermore, universal wheels are arranged at four corners of the bottom of the pitching base. Adopt above-mentioned structure, the pitching device that rolls of the whole unmanned aerial vehicle flight of simulation of being convenient for removes.

To sum up, owing to adopted this technical scheme, the beneficial effects of the utility model are that:

1. the utility model relates to a device that is used for unmanned aerial vehicle every single move assembly that rolls has set gradually every single move base, every single move track, the supporting seat that rolls and the mount that rolls from supreme down, connects every single move base and the supporting seat that rolls through triangular supports subassembly and the support frame that rolls, supports its stable in structure, the adjustment fixed position of being convenient for to every single move track and the mount that rolls.

2. The utility model relates to a device that is used for unmanned aerial vehicle every single move assembly that rolls, every single move track roll through first gyro wheel left and right sides, can simulate aircraft every single move flight, and the mount that rolls rotates on the second gyro wheel, can simulate unmanned aerial vehicle side flight, upset etc. effectual simulation unmanned aerial vehicle side flight, various flight attitudes such as upset, every single move.

3. The utility model relates to a device for unmanned aerial vehicle pitching assembly that rolls, run through support frame A and every single move track through first locating lever, can position every single move track, stop rolling and pass; run through locating support and the cardboard that rolls through the second locating lever, can stop rolling with the cardboard location that rolls, make unmanned aerial vehicle keep specific flight attitude, be convenient for verify top data.

Drawings

In order to more clearly illustrate the technical solutions of the embodiments of the present invention, the drawings needed to be used in the embodiments are briefly described below, it should be understood that the following drawings only illustrate some embodiments of the present invention, and therefore should not be considered as limiting the scope, for those skilled in the art, other related drawings can be obtained according to the drawings without creative efforts, and the proportional relationship of each component in the drawings in the present specification does not represent the proportional relationship in the actual material selection design, and is only a schematic diagram of the structure or the position, in which:

fig. 1 is a schematic structural diagram of the present invention;

fig. 2 is a front view of the present invention;

fig. 3 is a side view of the present invention;

fig. 4 is a plan view of the present invention.

Reference numerals in the drawings indicate:

1-pitching base, 101-through groove, 102-channel, 103-right-angle connecting piece, 104-right-angle fastener, 105-fixed rod, 2-pitching rail, 201-arc plate, 202-cross rod, 203-through hole, 3-rolling supporting seat, 4-rolling fixed frame, 401-auxiliary rod, 402-rolling clamping plate, 403-clamping hole, 404-fastening device, 5-triangular supporting component, 501-supporting frame A, 502-supporting frame B, 503-first positioning rod, 6-first roller, 7-rectangular plate, 8-rolling supporting frame, 9-second roller, 10-positioning frame, 11-second positioning rod and 12-universal wheel.

Detailed Description

In order to make the objects, technical solutions and advantages of the present invention more clearly understood, the present invention is further described in detail below with reference to the accompanying drawings and embodiments. It should be understood that the specific embodiments described herein are for purposes of illustration only and are not intended to limit the invention, i.e., the described embodiments are only some, but not all embodiments of the invention. The components of embodiments of the present invention, as generally described and illustrated in the figures herein, may be arranged and designed in a wide variety of different configurations.

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.

Thus, the following detailed description of the embodiments of the present invention, presented in the accompanying drawings, is not intended to limit the scope of the invention, as claimed, but is merely representative of selected embodiments of the invention. Based on the embodiment of the present invention, all other embodiments obtained by the person skilled in the art without creative work belong to the protection scope of the present invention.

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.

The present invention will be described in detail with reference to the accompanying drawings.

Example one

As shown in fig. 1-4, the utility model relates to a device for unmanned aerial vehicle pitching assembly that rolls, including pitch base 1, pitch track 2, roll supporting seat 3 and roll mount 4, pitch base 1 and roll supporting seat 3 are the rectangle frame, be fixed with triangular support subassembly 5 through the bolt on the long limit of pitch base 1, and the top swing joint of triangular support subassembly 5 has first gyro wheel 6, pitch track 2 and first gyro wheel 6 swing joint, pitch base 1 supports pitch track 2 through triangular support subassembly 5, pitch track 2 is perpendicular to the plane that pitch base 1 is located and can roll along the long limit direction of pitch base 1; a rectangular plate 7 is fixed on the end face of the pitching rail 2, the rolling support seat 3 is fixed on the rectangular plate 7 through a bolt, the long edge of the rolling support seat 3 is over against the long edge of the pitching base 1, the short edge of the rolling support seat 3 is parallel to the short edge of the pitching base 1, a rolling support frame 8 is fixed on the short edge of the rolling support seat 3 through a bolt, and a second roller 9 is movably connected onto the rolling support frame 8; roll mount 4 includes auxiliary rod 401 and can dismantle two circular shape cardboard 402 that roll of connection at auxiliary rod 401 both ends, cardboard 402 that rolls is through 9 swing joint of second gyro wheel on the top of support frame 8 that rolls to support through the support frame 8 that rolls, the plane at cardboard 402 perpendicular to support seat 3 place that rolls for two, and the projection can roll along the minor face direction of support seat 3 that rolls on the minor face of support seat 3 that rolls.

The existing simulation test device can not effectively simulate various flight attitudes such as unmanned aerial vehicle side flight, overturning, pitching and the like, and has single structure and poor stability. The utility model discloses every single move base 1, every single move track 2, roll supporting seat 3 and roll mount 3, every single move base 1 and roll supporting seat 3 are the rectangle frame, install triangle support assembly 5 through the bolt fastening on the long limit of every single move base 1, every single move base 1 has two long limits, the triangle support assembly 5 on two long limits is symmetrical parallel each other, the top of triangle support assembly 5 is swing joint with first gyro wheel 6, every single move track 2 is swing joint on triangle support assembly 5 through first gyro wheel 6, triangle support assembly 5 is used for supporting every single move track 2, every single move base 1 realizes the support to every single move track 2 through triangle support assembly 5, every single move track 2 is symmetrical with the axis in the vertical direction when being in the level, through being fixed with rectangle panel 7 on the terminal surface of every single move track 2, roll supporting seat 3 passes through the bolt fastening on rectangle panel 7, the pitching rail 2 is used for stably supporting the rolling support seat 3, and the rolling support seat 3 rolls left and right on the long edge of the pitching base 1 along with the pitching rail 2 to realize pitching. The utility model discloses there is rolling support frame 8 through bolt fixed mounting on the minor face of support seat 3 that rolls, swing joint has second gyro wheel 9 on the support frame 8 that rolls, two cardboard 402 swing joint that roll of mount 4 are on second gyro wheel 9, support seat 3 and the support frame 8 that rolls are to rolling cardboard 402 support, cardboard 402 that rolls overturns through second gyro wheel 9 upset, unmanned aerial vehicle's aircraft nose and tail are arranged in respectively on two cardboard 402 that roll of mount 4 that roll, cardboard 402 that rolls rotates, unmanned aerial vehicle is along with the upset of cardboard 402 that rolls, and roll and realize the every single move flight gesture about every single move track 2, effectively simulate unmanned aerial vehicle flight, be convenient for verify the top data, stability is good.

Example two

The embodiment is to further explain the present invention.

As shown in fig. 1 and 4, in this embodiment, on the basis of the first embodiment, in a preferable scheme of this embodiment, each side of the pitch base 1 and the roll support base 3 is a square steel tube, through grooves 101 are formed in four side surfaces of the square steel tube along the length direction, and the square steel tube is further provided with a cylindrical passage 102 coinciding with the central axis. By adopting the structure, the through grooves 101 on the square steel pipe are convenient for installing bolts, so that various supporting components and connecting pieces can be fixed, the mounting bolts can be installed at any position of the through grooves 101 on the square steel pipe, bolt holes do not need to be formed, the triangular supporting components 5 and the rolling supporting frame 8 are convenient to adjust the installation position, and the mounting structure is simple and convenient.

In a preferable scheme of this embodiment, a right-angle connector 103 and a right-angle fastener 104 are further disposed at the joint of the square steel tube. Adopt above-mentioned structure, right angle connector 103 is used for connecting each square steel pipe, makes every single side vertical connection of every single move base 1 and roll supporting seat 3, and right angle fastener 104 is right triangle's triangular prism for the cross section, and right angle fastener 104 passes through the bolt to be installed in the inboard of rectangle frame, and two cylinders of right angle fastener 104 are hugged closely to the rectangle frame medial surface, make right angle fastener 104's right angle and the right angle coincidence of rectangle frame to consolidate the vertical connection between the square steel pipe.

In a preferable scheme of this embodiment, the pitching base 1 is further provided with a vertical connection long-side fixing rod 105. With the above structure, the fixing lever 105 can reinforce the stability of the pitch base 1.

EXAMPLE III

The embodiment is to further explain the present invention.

As shown in fig. 1 to 3, in this embodiment, on the basis of the above, in a preferable scheme of this embodiment, the pitch track 2 includes two parallel arc-shaped plates 201 in the horizontal direction, and a cross bar 202 is further connected between the two arc-shaped plates 201; the pitching rail 2 is further provided with a plurality of through holes 203 which horizontally penetrate through the pitching rail 2, and the through holes 203 are axisymmetric with the central axis of the pitching rail 2 in the vertical direction. By adopting the structure, the pitching track 2 formed by the two arc-shaped plates 201 can roll through the first roller 6, and the two rolling clamping plates 402 can roll in parallel and synchronously under the connection action of the cross bar 202; the through holes 203 on the pitch track 2 can reduce the weight of the pitch track 2 and also reduce the material cost for manufacturing the device.

Example four

The embodiment is to further explain the present invention.

As shown in fig. 1 to 3, in this embodiment, based on the above, in a preferred scheme of this embodiment, the triangular support assembly 5 includes a support frame a501 and a support frame B502, and in the vertical direction, the height of the support frame B502 is greater than the height of the support frame a501, two support frames B502 are disposed on two sides of the support frame a501, the first roller 6 on the support frame a501 is located above the pitching rail 2, and the first roller 6 of the support frame B502 is located below the pitching rail 2; the support frame a501 is further provided with a first positioning rod 503. By adopting the structure, the pitching rail 2 is clamped between the first rollers 6 of the support frame A501 and the two support frames B502, so that the triangular support component 5 can support the pitching rail 2 conveniently, and the rolling stability of the pitching rail 2 and the overall uniformity of the simulated flight device are improved; when needs location every single move track 2, when making unmanned aerial vehicle keep certain every single move gesture, be provided with the locating hole that matches with first locating lever 503 on the support frame A501, utilize first locating lever 503 to run through support frame A501 and every single move track 2, can fix a position every single move track 2, stop the roll.

EXAMPLE five

The embodiment is to further explain the present invention.

As shown in fig. 1-3, this embodiment is on the basis of the aforesaid, in this embodiment an optimal scheme, screens hole 403 that is used for fixed unmanned aerial vehicle is all seted up at the center of two cardboard 402 that roll, and the horizontal coincidence of the axis in two cardboard 402 and screens holes 403 that roll, the cardboard 402 that rolls crosses face diameter etc. and divide into two semicircle cardboards, and the contact site of two semicircle cardboard is provided with mutually supporting lug and recess respectively to the contact site of two semicircle cardboard all is provided with fastener 404 along axial both ends. Adopt above-mentioned structure, open fastener 404, part two semicircle cardboards, arrange unmanned aerial vehicle's aircraft nose and tail in the screens hole 403 of the cardboard 402 that rolls respectively, two semicircle cardboards pass through the lug and the recess merges together, block unmanned aerial vehicle to it is fixed through fastener 404, realize fixed to unmanned aerial vehicle, the cardboard 402 that is convenient for roll rolls on second gyro wheel 9. Preferentially, cardboard 402 that rolls all adopts the aluminium board, in this embodiment, cardboard 402 radius that rolls for placing the aircraft nose is greater than the cardboard 402 that rolls that is used for placing the unmanned aerial vehicle afterbody, and be used for still being provided with the round hole on the cardboard 402 that rolls of placing the unmanned aerial vehicle aircraft nose, be convenient for alleviate the great weight of cardboard 402 that rolls of radius, it is that the weight of two cardboard 402 that rolls differs little, it is preferred, two sets up two auxiliary rods between the cardboard 402 that rolls, make cardboard 402 that rolls keep unified rotation, improve the rotation synchronism that rolls.

EXAMPLE six

The embodiment is to further explain the present invention.

As shown in fig. 1 to 3, in this embodiment, on the basis of the above, in a preferable scheme of this embodiment, the turning device further includes a positioning bracket 10 fixed on the turning support base 3, the positioning bracket 10 is provided with a second positioning rod 11, and the turning chuck plate 402 is provided with a positioning hole matched with the second positioning rod 11. Adopt above-mentioned structure, when needs location cardboard 402 that rolls, make unmanned aerial vehicle keep certain posture of turning on one's side, roll and be provided with the locating hole that matches with second locating lever 11 on the cardboard 402, utilize second locating lever 11 to run through locating support 10 and the cardboard 402 that rolls, can stop rolling cardboard 402 location.

EXAMPLE seven

The embodiment is to further explain the present invention.

As shown in fig. 1 to 3, in the present embodiment, based on the above, in a preferable scheme of the present embodiment, universal wheels 12 are disposed at four corners of the bottom of the pitching base 1. Adopt above-mentioned structure, the pitching device that rolls of the whole unmanned aerial vehicle flight of simulation of being convenient for removes.

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 (9)

1. The utility model provides a device that is used for unmanned aerial vehicle pitch assembly that rolls which characterized in that: the pitching device comprises a pitching base (1), a pitching track (2), a rolling support seat (3) and a rolling fixing frame (4), wherein the pitching base (1) and the rolling support seat (3) are rectangular frames, a triangular support component (5) is fixed on a long edge of the pitching base (1) through a bolt, the top end of the triangular support component (5) is movably connected with a first roller (6), the pitching track (2) is movably connected with the first roller (6), the pitching base (1) supports the pitching track (2) through the triangular support component (5), and the pitching track (2) is perpendicular to a plane where the pitching base (1) is located and can roll along the long edge direction of the pitching base (1); a rectangular plate (7) is fixed on the end face of the pitching rail (2), the rolling support seat (3) is fixed on the rectangular plate (7) through a bolt, the long edge of the rolling support seat (3) is just opposite to the long edge of the pitching base (1), the short edge of the rolling support seat (3) is parallel to the short edge of the pitching base (1), a rolling support frame (8) is fixed on the short edge of the rolling support seat (3) through a bolt, and a second roller (9) is movably connected onto the rolling support frame (8); roll mount (4) including auxiliary rod (401) and can dismantle two circular shape cardboard (402) that roll of connection at auxiliary rod (401) both ends, cardboard (402) that roll through second gyro wheel (9) swing joint on the top of rolling support frame (8) to support through rolling support frame (8), two planes that cardboard (402) perpendicular to roll supporting seat (3) place roll, and the projection can roll along the minor face direction of rolling supporting seat (3) on the minor face of rolling supporting seat (3).

2. The device for unmanned aerial vehicle roll-pitch assembly of claim 1, wherein: each side of the pitching base (1) and the rolling support seat (3) is a square steel tube, through grooves (101) along the length direction are formed in four side faces of the square steel tube, and a cylindrical channel (102) coinciding with the central axis is further formed in the square steel tube.

3. The device for unmanned aerial vehicle roll-pitch assembly according to claim 2, wherein: the joint of the square steel pipe is also provided with a right-angle connecting piece (103) and a right-angle fastener (104).

4. The device for unmanned aerial vehicle roll pitch assembly of claim 3, wherein: the pitching base (1) is also provided with a fixing rod (105) which is vertically connected with the long edge.

5. The device for unmanned aerial vehicle roll-pitch assembly of claim 1, wherein: the pitching track (2) comprises two parallel arc-shaped plates (201) in the horizontal direction, and a cross rod (202) is connected between the two arc-shaped plates (201); still be equipped with a plurality of through-hole (203) that the level runs through every single move track (2) on every single move track (2), and through-hole (203) use every single move track (2) axis on vertical direction as the axial symmetry.

6. The device for unmanned aerial vehicle roll-pitch assembly of claim 1, wherein: the triangular support assembly (5) comprises a support frame A (501) and a support frame B (502), in the vertical direction, the height of the support frame B (502) is larger than that of the support frame A (501), two support frames B (502) are arranged on two sides of the support frame A (501), a first roller (6) on the support frame A (501) is located above the pitching track (2), and a first roller (6) of each support frame B (502) is located below the pitching track (2); the support frame A (501) is also provided with a first positioning rod (503).

7. The device for unmanned aerial vehicle roll-pitch assembly of claim 1, wherein: clamping hole (403) that are used for fixed unmanned aerial vehicle are all seted up at the center of two cardboard (402) that roll, and the axis level coincidence of two cardboard (402) and clamping hole (403) that roll, the cardboard that rolls (402) cross face diameter etc. and divide into two semicircle cardboards, and the contact site of two semicircle cardboards is provided with the lug and the recess of mutual matching respectively to the contact site of two semicircle cardboards all is provided with fastener (404) along axial both ends.

8. The device for unmanned aerial vehicle roll-pitch assembly of claim 1, wherein: still including fixing locating support (10) on support seat (3) rolls, be provided with second locating lever (11) on locating support (10), be provided with the locating hole that matches with second locating lever (11) on cardboard (402) rolls.

9. The device for unmanned aerial vehicle roll-pitch assembly of claim 1, wherein: the four corners of the bottom of the pitching base (1) are provided with universal wheels (12).

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