CN214446328U - Part frame is used in aircraft spare part maintenance - Google Patents

Abstract

The utility model relates to a spare part technical field just discloses an aircraft spare part is part frame for maintenance, the on-line screen storage device comprises a base, four shock tubes of bottom fixedly connected with of base, the spacing post of interior roof fixedly connected with of shock tube, a spring has been cup jointed in the outside of spacing post, the bottom fixedly connected with snubber block of a spring, the bottom fixedly connected with universal wheel of snubber block, the rotary slot has been seted up at the top of base, the inside of rotary slot is rotated and is connected with the rotary block, the card hole has all been seted up with the front and the back in the left and right sides of base, the cross slot has been seted up on the right side of rotary block, No. two springs of left side wall fixedly connected with of cross slot, the right side fixedly connected with shell fragment of No. two springs. This aircraft spare part maintenance is with part frame can be convenient for the staff and remove, improves stability simultaneously to can be convenient for the staff and receive and release, can adjust the direction simultaneously.

Description

Part frame is used in aircraft spare part maintenance

Technical Field

The utility model relates to a spare part technical field specifically is an aircraft spare part is part frame for maintenance.

Background

The aircraft can be classified into two categories, i.e., military aircraft and civil aircraft according to their purposes, the military aircraft refers to the aircraft used in various military fields, and the civil aircraft refers to all non-military-purpose aircraft (such as passenger aircraft, cargo aircraft, agricultural aircraft, sports aircraft, ambulance aircraft, test research aircraft, and the like).

At present, when the existing part frame for maintaining the airplane parts is used, certain defects exist, and because the general part frame for maintaining the airplane parts is a fixing device and is inconvenient for workers to move, the part frame needs to be carried at every time, so that the maintenance efficiency is reduced, the placing position is limited, the direction cannot be rotated, and the inconvenience in operation is brought to the workers in sequence, so that the part frame for maintaining the airplane parts is provided for solving the problems.

SUMMERY OF THE UTILITY MODEL

Technical problem to be solved

The utility model provides a not enough to prior art, the utility model provides an aircraft spare part is part frame for maintenance has possessed and has been convenient for remove simultaneously and be convenient for retrieve and adjust advantages such as direction, has solved current aircraft spare part is part frame for maintenance when using, is not convenient for remove and the problem of adjusting the direction.

(II) technical scheme

For the above-mentioned purpose of being convenient for remove the recovery of being convenient for simultaneously and adjust the direction of realizing, the utility model provides a following technical scheme: a part rack for maintaining aircraft parts comprises a base, wherein four shock-absorbing cylinders are fixedly connected to the bottom of the base, a limiting column is fixedly connected to the inner top wall of each shock-absorbing cylinder, a first spring is sleeved on the outer side of the limiting column, a shock-absorbing block is fixedly connected to the bottom of the first spring, a universal wheel is fixedly connected to the bottom of the shock-absorbing block, a rotary groove is formed in the top of the base, a rotary block is rotatably connected to the inside of the rotary groove, clamping holes are formed in the left side and the right side of the base, clamping holes are formed in the front side and the back side of the base, a transverse groove is formed in the right side of the rotary block, a second spring is fixedly connected to the left side wall of the transverse groove, a spring plate is fixedly connected to the right side of the second spring, a connecting column is fixedly connected to the top of the rotary block, a rotary plate is fixedly connected to the top of the connecting column, two support columns are fixedly connected to the top of the rotary plate, and four grooves are formed in the left side wall and the right side walls of the two support columns, the utility model discloses a socket for two, including the support column, the inboard fixedly connected with pivot of recess, the inboard fixedly connected with pivot of bearing, the board is placed to the outside fixedly connected with of pivot, the bayonet socket has been seted up on the right side of placing the board, right side four regulation section of thick bamboos of right side fixedly connected with of support column, the inboard swing joint of adjusting a section of thick bamboo has the movable block, the inboard fixedly connected with inserted bar of movable block, No. three springs have been cup jointed in the outside of inserted bar, two four gag lever posts of fixedly connected with between the support column.

Preferably, the left sides of the four adjusting cylinders penetrate through the right supporting column and extend to the left side of the right supporting column, and the four adjusting cylinders are distributed vertically and symmetrically.

Preferably, four the left end of inserted bar all runs through in proper order and adjusts a section of thick bamboo, No. three spring and right side support column and extend to the inside of bayonet socket.

Preferably, the four placing plates are equal to each other in length and distance between two supporting columns, and the two supporting columns are symmetrically distributed.

Preferably, four place the board and be front and back symmetric distribution, four the right-hand member of pivot all runs through and places the board and extend to the inboard of No. two bearings.

Preferably, the rotating plate is circular, the top end of the connecting column penetrates through the base and extends to the bottom of the rotating plate, and the four damping cylinders are symmetrically distributed.

(III) advantageous effects

Compared with the prior art, the utility model provides an aircraft spare part is part frame for maintenance possesses following beneficial effect:

the part rack for maintaining the airplane parts comprises a base, a damping cylinder, a universal wheel, a positioning column, a bearing, a supporting column and a rotating shaft, wherein the base is pushed to a proper position by the universal wheel under the supporting action of the damping cylinder, the universal wheel drives the damping block to extrude a first spring in the process, the limit of extrusion is positioned at the bottom of the limiting column, then the vibration caused by movement can be effectively buffered under the elastic recovery action of the first spring, when an inserted rod is pulled, the inserted rod drives a movable block to extrude a third spring until the inserted rod is separated from a bayonet, then a placing plate is placed, the placing plate drives the rotating shaft to rotate under the supporting action of a second bearing, the placing plate is in a horizontal state, meanwhile, the limiting rod carries out limiting support on the placing plate, the parts can be placed, the elastic pieces can extrude the second spring by pressing the elastic pieces until the elastic pieces are separated from the clamping holes, the supporting column can be rotated, and the rotating plate is driven by the supporting column, the rotor plate drives the connecting column to rotate, the connecting column drives the rotor block to rotate, and when the next card hole is moved, under the elastic force restoring effect of the second spring, the second spring drives the elastic piece to pass through the card hole to be fixed.

Drawings

FIG. 1 is a schematic structural view of the present invention;

fig. 2 is a top view of the structure of the present invention.

In the figure: the damping device comprises a base 1, a damping cylinder 2, a limiting column 3, a first spring 4, a damping block 5, a universal wheel 6, a rotary groove 7, a rotary block 8, a clamping hole 9, a transverse groove 10, a second spring 11, a spring plate 12, a connecting column 13, a rotary plate 14, a supporting column 15, a groove 16, a second bearing 17, a rotating shaft 18, a placing plate 19, a bayonet 20, an adjusting cylinder 21, a movable block 22, an inserted rod 23, a third spring 24 and a limiting rod 25.

Detailed Description

The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.

Please refer to fig. 1-2, the present invention provides a technical solution: a part rack for maintaining airplane parts comprises a base 1, wherein the bottom of the base 1 is fixedly connected with four shock-absorbing cylinders 2, the four shock-absorbing cylinders 2 are symmetrically distributed in the left and right direction, the inner top wall of each shock-absorbing cylinder 2 is fixedly connected with a limiting column 3, the outer side of each limiting column 3 is sleeved with a spring 4, the top of each spring 4 is fixedly connected with the inner top wall of each shock-absorbing cylinder 2, the height of each spring 4 in a natural state is larger than that of each shock-absorbing cylinder 2, the bottom of each spring 4 is fixedly connected with a shock-absorbing block 5, the bottom of each shock-absorbing block 5 is fixedly connected with a universal wheel 6, the outer sides of the four universal wheels 6 are respectively provided with a brake pad, the top of the base 1 is provided with a rotary groove 7, the inner part of each rotary groove 7 is rotatably connected with a rotary block 8, the left side and the right side of the base 1 are respectively provided with a clamping hole 9, the right side of each rotary block 8 is provided with a transverse groove 10, the left side wall of each transverse groove 10 is fixedly connected with a second spring 11, the length of the second spring 11 in a natural state is larger than that of the transverse groove 10, the right side of the second spring 11 is fixedly connected with an elastic sheet 12, the top of the rotating block 8 is fixedly connected with a connecting column 13, the top of the connecting column 13 is fixedly connected with a rotating plate 14, the length and the width of the base 1 are respectively larger than the diameter of the rotating plate 14, the rotating plate 14 is circular, the top end of the connecting column 13 penetrates through the base 1 and extends to the bottom of the rotating plate 14, the top of the rotating plate 14 is fixedly connected with two supporting columns 15, the two supporting columns 15 are distributed in bilateral symmetry, four grooves 16 are formed in the left side wall and the right side wall of the two supporting columns 15, a second bearing 17 is fixedly connected inside each groove 16, a rotating shaft 18 is fixedly connected between the inner sides of the two corresponding second bearings 17, a placing plate 19 is fixedly connected to the outer side of the rotating shaft 18, the right ends of the four rotating shafts 18 penetrate through the placing plate 19 and extend to the inner sides of the second bearing 17, the four placing plates 19 are symmetrically distributed in the front and back direction, the length of the four placing plates 19 is equal to the distance between the two supporting columns 15, the right side of the placing plates 19 is provided with a bayonet 20, the right side of the right supporting column 15 is fixedly connected with four adjusting cylinders 21, the left sides of the four adjusting cylinders 21 penetrate through the right supporting column 15 and extend to the left side of the right supporting column 15, the four adjusting cylinders 21 are symmetrically distributed in the vertical direction, the inner side of each adjusting cylinder 21 is movably connected with a movable block 22, the inner side of each movable block 22 is fixedly connected with an inserting rod 23, the outer side of each inserting rod 23 is sleeved with a third spring 24, the length of each third spring 24 in a natural state is larger than that of each adjusting cylinder 21, the left ends of the four inserting rods 23 sequentially penetrate through the adjusting cylinders 21, the third springs 24 and the right supporting columns 15 and extend to the insides of the bayonet 20, the four limiting rods 25 are fixedly connected between the two supporting columns 15, and the length of the limiting rods 25 is equal to that between the two supporting columns 15, through the supporting action of the damping cylinder 2, the universal wheel 6 pushes the base 1 to a proper position, the universal wheel 6 drives the damping block 5 to extrude the first spring 4 in the way, the extrusion limit is positioned at the bottom of the limiting column 3, then the vibration brought by the elastic recovery action of the first spring 4 can be effectively buffered, when the inserted rod 23 is pulled, the inserted rod 23 drives the movable block 22 to extrude the third spring 24 until the inserted rod 23 is separated from the bayonet 20, then the placing plate 19 is placed, under the supporting action of the second bearing 17, the placing plate 19 drives the rotating shaft 18 to rotate, so that the placing plate 19 is in a horizontal state, meanwhile, the limiting rod 25 carries out limiting support on the placing plate 19, parts can be placed, after the placing is finished, the second spring 11 can be extruded by pressing the elastic sheet 12 until the elastic sheet 12 is separated from the clamping hole 9, the supporting column 15 can be rotated, support column 15 drives commentaries on classics board 14 and rotates, commentaries on classics board 14 drives spliced pole 13 and rotates, spliced pole 13 drives commentaries on classics piece 8 and rotates, when moving next card hole 9, under No. two spring 11's elasticity answer effect, No. two spring 11 drive shell fragment 12 and pass card hole 9 and fix, this aircraft spare part is part frame for maintenance, the staff of can being convenient for removes, stability is improved simultaneously, and the staff of can being convenient for receive and releases, can adjust the direction simultaneously.

When the shock absorber is used, the universal wheel 6 pushes the base 1 to a proper position under the supporting action of the shock absorbing cylinder 2, the universal wheel 6 drives the shock absorbing block 5 to extrude the first spring 4 in the road, the extrusion limit is positioned at the bottom of the limiting column 3, then the shock caused by movement can be effectively buffered under the elastic force recovery action of the first spring 4, when the inserted rod 23 is pulled, the inserted rod 23 drives the movable block 22 to extrude the third spring 24 until the inserted rod 23 is separated from the bayonet 20, then the placing plate 19 is placed, under the supporting action of the second bearing 17, the placing plate 19 drives the rotating shaft 18 to rotate, so that the placing plate 19 is in a horizontal state, meanwhile, the limiting rod 25 carries out limiting support on the placing plate 19, parts can be placed, after the placing is finished, the second spring 11 can be extruded by pressing the elastic sheet 12 until the elastic sheet 12 is separated from the bayonet 9, can rotate support column 15, support column 15 drives commentaries on classics board 14 and rotates, changes board 14 and drives spliced pole 13 and rotate, and spliced pole 13 drives commentaries on classics piece 8 and rotates, and when moving next card hole 9, under No. two spring 11's elasticity answer effect, No. two spring 11 drive shell fragment 12 and pass card hole 9 and fix.

To sum up, in the part rack for aircraft part maintenance, under the supporting action of the shock-absorbing cylinder 2, the universal wheel 6 pushes the base 1 to a proper position, the universal wheel 6 drives the shock-absorbing block 5 to extrude the first spring 4 on the way, the extrusion limit is positioned at the bottom of the limiting column 3, then the shock brought by the movement can be effectively buffered under the elastic force recovery action of the first spring 4, the inserted rod 23 is pulled, the inserted rod 23 drives the movable block 22 to extrude the third spring 24 until the inserted rod 23 is separated from the bayonet 20, then the placing plate 19 is placed, under the supporting action of the second bearing 17, the placing plate 19 drives the rotating shaft 18 to rotate, so that the placing plate 19 is in a horizontal state, meanwhile, the limiting rod 25 carries out limiting support on the placing plate 19, the part can be placed, after the placing is completed, the second spring 11 can be extruded by pressing the elastic sheet 12, until shell fragment 12 and card hole 9 break away from, can rotate support column 15, support column 15 drives commentaries on classics board 14 and rotates, commentaries on classics board 14 drives spliced pole 13 and rotates, spliced pole 13 drives commentaries on classics piece 8 and rotates, when removing next card hole 9, under No. two spring 11's elasticity answer effect, No. two spring 11 drive shell fragment 12 and pass card hole 9 and fix, this part frame for aircraft parts maintenance, the staff of can being convenient for removes, simultaneously, and stability is improved, and can be convenient for the staff receive and releases, simultaneously can the direction of regulation, it uses when the part frame to have solved current aircraft parts maintenance, be not convenient for remove and the problem of regulation direction.

It is to be noted that 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.

Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.

Claims (6)

1. The utility model provides an aircraft spare part maintenance is with part frame, includes base (1), its characterized in that: the shock absorber is characterized in that four shock absorbing cylinders (2) are fixedly connected to the bottom of the base (1), a limiting column (3) is fixedly connected to the inner top wall of each shock absorbing cylinder (2), a first spring (4) is sleeved on the outer side of each limiting column (3), a shock absorbing block (5) is fixedly connected to the bottom of each first spring (4), universal wheels (6) are fixedly connected to the bottom of each shock absorbing block (5), a rotary groove (7) is formed in the top of the base (1), a rotary block (8) is rotatably connected to the inside of each rotary groove (7), clamping holes (9) are formed in the left side, the right side, the front side and the back side of the base (1), a transverse groove (10) is formed in the right side of each rotary block (8), a second spring (11) is fixedly connected to the left side wall of each transverse groove (10), an elastic sheet (12) is fixedly connected to the right side of each second spring (11), and a connecting column (13) is fixedly connected to the top of each rotary block (8), the top of the connecting column (13) is fixedly connected with a rotating plate (14), the top of the rotating plate (14) is fixedly connected with two supporting columns (15), four grooves (16) are formed in the left side wall and the right side wall of the two supporting columns (15), a second bearing (17) is fixedly connected inside the grooves (16), a rotating shaft (18) is fixedly connected between the inner sides of the two corresponding second bearings (17), a placing plate (19) is fixedly connected to the outer side of the rotating shaft (18), a bayonet (20) is formed in the right side of the placing plate (19), four adjusting cylinders (21) are fixedly connected to the right side of the supporting columns (15), a movable block (22) is movably connected to the inner side of each adjusting cylinder (21), an inserting rod (23) is fixedly connected to the inner side of each movable block (22), and a third spring (24) is sleeved on the outer side of each inserting rod (23), four limiting rods (25) are fixedly connected between the two supporting columns (15).

2. The parts rack for repairing aircraft parts according to claim 1, wherein: the left sides of the four adjusting cylinders (21) all penetrate through the right side supporting column (15) and extend to the left side of the right side supporting column (15), and the four adjusting cylinders (21) are symmetrically distributed up and down.

3. The parts rack for repairing aircraft parts according to claim 1, wherein: the left end of the four inserted rods (23) sequentially penetrates through the adjusting cylinder (21), the third spring (24) and the right side supporting column (15) and extends to the inside of the bayonet (20).

4. The parts rack for repairing aircraft parts according to claim 1, wherein: the length of four place board (19) all equals with the distance between two support columns (15), two support columns (15) are bilateral symmetry and distribute.

5. The parts rack for repairing aircraft parts according to claim 1, wherein: the four placing plates (19) are symmetrically distributed front and back, and the right ends of the four rotating shafts (18) penetrate through the placing plates (19) and extend to the inner side of the second bearing (17).

6. The parts rack for repairing aircraft parts according to claim 1, wherein: the rotating plate (14) is circular, the top end of the connecting column (13) penetrates through the base (1) and extends to the bottom of the rotating plate (14), and the four damping cylinders (2) are symmetrically distributed.

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