CN210256011U - Angle bar installation aircraft nose - Google Patents

Angle bar installation aircraft nose Download PDF

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Publication number
CN210256011U
CN210256011U CN201921130246.5U CN201921130246U CN210256011U CN 210256011 U CN210256011 U CN 210256011U CN 201921130246 U CN201921130246 U CN 201921130246U CN 210256011 U CN210256011 U CN 210256011U
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cylinder
base
plate
quick
telescopic link
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CN201921130246.5U
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Chinese (zh)
Inventor
张静
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Hefei Yuanchi Technology Co Ltd
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Hefei Yuanchi Technology Co Ltd
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Abstract

The utility model provides an angle bar installation aircraft nose, the on-line screen storage device comprises a base, two quick-witted casees are installed to the symmetry on the base, be equipped with slide mechanism between base and two quick-witted casees, the inside of machine case all is equipped with solenoid valve assembly, two first cylinders and two strikes cylinders, the telescopic link of first cylinder is all connected in the mechanism of punching, the top of machine case all is equipped with the stand board, the equal vertical second cylinder that is equipped with in one side of stand board, the telescopic link of second cylinder all is connected in installation mechanism, the lateral wall on a long limit of base is equipped with the removal subassembly. The utility model discloses the cooperation that utilizes solenoid valve subassembly and a plurality of cylinders is used, reaches the control to gaseous speed in the cylinder to and the horizontal migration of having realized the aircraft nose body, and installation mechanism and the vertical removal of mechanism of punching, finally realized punching of aircraft nose and the automated control of installation, need not to take the manpower again to carry out the operation, the operating efficiency improves.

Description

Angle bar installation aircraft nose
Technical Field
The utility model relates to an angle bar installation technical field especially relates to an angle bar installation aircraft nose.
Background
When a pipeline is installed on the roof surface or the side wall of a beam in a building room, a hanging bracket made of angle iron is often needed to be installed, and when the angle iron is installed, a master generally uses an electric hammer to perform punching operation indoors, then installs an expansion bolt, and then places the angle iron for fixing.
In the process of installing the angle iron, limited to the actual structure of the angle iron, a master needs to find corresponding punching positions at the installation position by contrasting four holes at four corners of the angle iron, then the holes are punched one by one, if the master is operated manually, the error of the punching positions is large, the holes may need to be re-drilled during the subsequent angle iron installation, the operation efficiency is influenced, and time and labor are wasted; current lead screw installation aircraft nose, only 1 electric hammer can punch one by one, if to the angle bar, an angle bar corresponds a set of hole, will punch repeatedly many times, leads to the operating efficiency low, and lead screw installation aircraft nose does not have the mechanism that is used for the angle bar installation, still needs the manpower during last step installation angle bar, leads to the operating efficiency low equally.
SUMMERY OF THE UTILITY MODEL
The utility model aims at providing an overcome above-mentioned problem or solve an angle bar installation aircraft nose of above-mentioned problem at least partially to solve traditional manpower and punch the installation and current lead screw installation aircraft nose and can not effectively lead to the problem that the operating efficiency is low to the installation that punches of angle bar.
In order to achieve the above object, the technical solution of the present invention is specifically realized as follows: the base is included, two quick-witted cases are installed to the symmetry on the base, and the lateral wall on a long limit of base is equipped with the removal subassembly, it is connected with connecting screw to remove the subassembly, connecting screw passes the connecting hole in the middle of the bottom of locating every quick-witted case, the both sides of connecting hole all are equipped with fastening nut, be equipped with slide mechanism between base and two quick-witted cases, all be equipped with the stand board in the middle of the top of every quick-witted case, the both sides of stand board are equipped with first cylinder respectively and strike the cylinder, and the second cylinder is installed to the inboard of the relative direction of two stand boards, the telescopic link of first cylinder all is connected in the mechanism of punching, the telescopic link of second cylinder all is connected in.
Preferably, every the inside of quick-witted case all is equipped with solenoid valve assembly, two first cylinders and two and strikes the cylinder, the telescopic link of first cylinder and the telescopic link of striking the cylinder are all vertical to pass the top of quick-witted case, and first cylinder is located two quick-witted case opposite direction's inboard, strikes the cylinder and is located two quick-witted case opposite direction's the outside.
Preferably, slide mechanism includes slider and guide rail, be equipped with two guide rails along its long limit direction symmetry on the base, the bottom of machine case all is equipped with the multiunit slider, the slider sets up with the guide rail cooperation.
Preferably, the cross section of the guide rail has a straight arch shape with a central portion depressed inward.
Preferably, the punching mechanism comprises an electric hammer, the electric hammer is fixed on the mounting plate, and the telescopic rod of the first cylinder is connected to the mounting plate.
Preferably, the drilling end circumference of electric hammer is equipped with and connects the ash box, and the top of quick-witted case, mounting panel and the bottom that connects the ash box vertically pass the guide arm in proper order, and the guide arm is fixed in the column plate.
Preferably, installation mechanism includes that cavity sleeve, wind criticize, gear box and rotatory die clamping cylinder, the one end of gear box sets up with the output cooperation that wind was criticized, the other end of gear box runs through and is equipped with the cavity sleeve, the output circumference that wind was criticized is equipped with the fixed plate, rotatory die clamping cylinder is fixed in the fixed plate, rotatory die clamping cylinder is located one side of gear box, the telescopic link of second cylinder is fixed in the shell of fixed plate and gear box in proper order, strike the telescopic link accessible of cylinder the inner chamber of cavity sleeve, four position between the cavity sleeve is corresponding to four mounting holes of angle bar.
Preferably, the movable assembly comprises a third cylinder and a fourth cylinder, the telescopic plates of the third cylinder and the fourth cylinder are oppositely arranged and are all arranged outwards, the third cylinder is horizontally fixed on the side wall of one long edge of the base, a cylinder fixing plate is fixedly arranged on the telescopic plate of the third cylinder, the cylinder fixing plate is fixed on the cylinder body of the fourth cylinder, and the telescopic plate of the fourth cylinder is connected with the connecting screw rod through an L-shaped rod.
The utility model provides an angle bar installation aircraft nose, beneficial effect lies in:
1. the utility model discloses utilize the cooperation of solenoid valve subassembly and a plurality of cylinders to use, reach the control to the gaseous speed in the cylinder to and realized the horizontal migration of aircraft nose body, and the vertical removal of installation mechanism and punching mechanism, finally realized punching of aircraft nose and the automated control of installation, need not to take the manpower again to carry out the operation, the operating efficiency improves;
2. the utility model discloses further improve on the aircraft nose of original lead screw mounting plate, add electric hammer, gear box and the quantity of wind criticizing, and integrate them on two quick-witted casees in proper order, the aircraft nose only needs to do the action of two sets of punches can accomplish the installation of an angle bar when the during operation, need not to punch repeatedly at this moment many times, has promoted the operating efficiency;
3. the utility model discloses utilize fastening nut to adjust the distance between two quick-witted casees, and arrange the telescopic position of cavity on the gear box into corresponding with the mounting hole of angle bar, so the angle bar can the overlap joint on the cavity sleeve, accomplishes the installation, has also avoided the error of the position of punching simultaneously, has further promoted the operating efficiency.
Drawings
In order to more clearly illustrate the technical solutions of the embodiments of the present invention, the drawings used in the description of the embodiments will be briefly described below, and it is obvious that the drawings in the description below are only some embodiments of the present invention, and it is obvious for those skilled in the art that other drawings can be obtained according to these drawings without creative efforts.
FIG. 1 is a perspective view of the angle iron mounting head of the present invention;
FIG. 2 is a front view of the angle iron mounting head of the present invention;
FIG. 3 is a side view of the angle iron mounting head of the present invention with one of the housings broken away;
FIG. 4 is a right side view of the angle iron mounting head of the present invention;
FIG. 5 is a perspective view of the angle iron mounting head of the present invention from the bottom;
fig. 6 is a partially enlarged view of a portion a in fig. 5 according to the present invention.
In the figure: the device comprises a base 1, a case 2, a column plate 3, an electric hammer 4, an ash receiving box 5, a hollow sleeve 6, a pneumatic screwdriver 7, a rotary clamping cylinder 8, a second cylinder 9, a guide rod 10, a first cylinder 11, a cylinder fixing plate 12, a third cylinder 13, a fourth cylinder 14, an L-shaped rod 15, a connecting hole 16, a sliding block 17, a striking cylinder 18, a gear box 19, an electromagnetic valve assembly 20, a guide rail 21, a connecting screw rod 22, a mounting plate 23 and a fixing plate 24.
Detailed Description
Exemplary embodiments of the present disclosure will be described in more detail below with reference to the accompanying drawings. While exemplary embodiments of the present disclosure are shown in the drawings, it should be understood that the present disclosure may be embodied in various forms and should not be limited to the embodiments set forth herein. Rather, these embodiments are provided so that this disclosure will be thorough and complete, and will fully convey the scope of the disclosure to those skilled in the art.
Fig. 1-6 show angle bar installation aircraft nose that the embodiment of the utility model provides, including base 1, two quick-witted casees 2 are installed to the symmetry on base 1, and the lateral wall on a long limit of base 1 is equipped with the removal subassembly, and the removal subassembly is connected with connecting screw 22, and connecting screw 22 passes connecting hole 16 in the middle of locating the bottom of every quick-witted case 2, and the both sides of connecting hole 16 all are equipped with fastening nut, revolve wrong fastening nut, change the relative position of two connecting holes 16, finally are used for adjusting the distance between two quick-witted cases 2.
Be equipped with slide mechanism between base 1 and two quick-witted casees 2, all be equipped with stand board 3 in the middle of the top of every quick-witted case 2, the both sides of stand board 3 are equipped with first cylinder 11 respectively and hit cylinder 18, and second cylinder 9 is installed to the inboard of two stand board 3 relative directions, and the telescopic link of first cylinder 11 all is connected in the mechanism of punching, and the telescopic link of second cylinder 9 all is connected in installation mechanism. Every quick-witted case 2's inside all is equipped with solenoid valve assembly 20, two first cylinders 11 and two striking cylinders 18, and the telescopic link of first cylinder 11 and the telescopic link of striking cylinder 18 are all vertical passes the top of quick-witted case 2, and first cylinder 11 is located the inboard of two quick-witted case 2 relative directions, strikes cylinder 18 and is located the outside of two quick-witted case 2 relative directions. The utility model discloses utilize the cooperation of solenoid valve subassembly 20 and a plurality of cylinders to use, reach the control to gaseous speed in the cylinder to and realized the horizontal migration of aircraft nose body, and installation mechanism and the vertical removal of mechanism of punching, finally realized punching of aircraft nose and the automated control of installation, need not to take the manpower again to carry out the operation, the operating efficiency improves.
Referring to fig. 1, the sliding mechanism includes a sliding block 17 and a guide rail 21, two guide rails 21 are symmetrically arranged on the base 1 along the long side direction of the base, a plurality of groups of sliding blocks 17 are arranged at the bottom of the case 2, and the sliding blocks 17 are arranged in cooperation with the guide rails 21. Preferably, the cross section of the guide rail 21 presents a straight arch shape with a central portion recessed inwards, and the shape of the inner edge of the sliding block 17 matches the shape of the cross section of the guide rail 21, so that the chassis 2 can slide on the guide rail 21 more stably.
The punching mechanism comprises an electric hammer 4, the electric hammer 4 is fixed on a mounting plate 23, and the telescopic rod of the first air cylinder 11 is connected to the mounting plate 23. The drilling end circumference of electric hammer 4 is equipped with connects ash box 5, and the top of quick-witted case 2, mounting panel 23 and the bottom that connects ash box 5 vertically pass guide arm 10 in proper order, and guide arm 10 is fixed in stand board 3. The telescopic link action of first cylinder 11 lifts mounting panel 23, and then drives electric hammer 4 and lifts to the plane of punching, starts electric hammer 4's power, and electric hammer 4 drills, has bored the hole after, and the telescopic link of first cylinder 11 returns rapidly. The ash falls into and connects ash box 5 in, waits for further processing, and its position is also comparatively firm when mounting panel 23 has guaranteed that electric hammer 4 moves, and when mounting panel 23 lifted or descended, guide arm 10 played the effect of spacing direction, has also played certain firm effect simultaneously.
Installation mechanism includes hollow sleeve 6, wind batch 7, gear box 19 and rotatory die clamping cylinder 8, the one end of gear box 19 sets up with the output cooperation of wind batch 7, the other end of gear box 19 runs through and is equipped with hollow sleeve 6, the output circumference of wind batch 7 is equipped with fixed plate 24, rotatory die clamping cylinder 8 is fixed in fixed plate 24, rotatory die clamping cylinder 8 is located one side of gear box 19, the telescopic link of second cylinder 9 is fixed in the shell of fixed plate 24 and gear box 19 in proper order, strike the inner chamber of the telescopic link accessible hollow sleeve 6 of cylinder 18, the position between four hollow sleeve 6 is corresponding to four mounting holes of angle bar. The rotary clamping cylinder 8 can play a role in clamping and fastening angle irons and prevent the angle irons from falling off from the hollow sleeve 6.
Referring to fig. 2, the moving assembly includes a third cylinder 13 and a fourth cylinder 14, the direction of the expansion plate of the third cylinder 13 is opposite to that of the expansion plate of the fourth cylinder 14, the expansion plates of the third cylinder 13 and the fourth cylinder 14 are both disposed outward, the third cylinder 13 is horizontally fixed on the side wall of one long side of the base 1, the expansion plate of the third cylinder 13 is fixedly provided with a cylinder fixing plate 12, the cylinder fixing plate 12 is fixed on the cylinder body of the fourth cylinder 14, and the expansion plate of the fourth cylinder 14 is connected to the connecting screw 22 through an L-shaped rod 15.
It should be noted that the first cylinder 11, the second cylinder 9, the third cylinder 13, the fourth cylinder 14 and the striking cylinder 18 are all electrically connected to the solenoid valve assembly 20 and the external control module.
Referring to fig. 6, the connecting screw rod 22 passes through the connecting hole 16 to connect the two cases 2, and the distance between the two cases 2 and the distance between the two rows of hollow sleeves 6 can be adjusted by adjusting the fastening nuts on both sides of the connecting hole 22 until the positions of the hollow sleeves are arranged to correspond to the mounting holes of the angle iron, so that the angle iron can be lapped on the hollow sleeves to wait for mounting. Meanwhile, after the distance is fixed, the two housings 2 are integrally fixed to the connecting screw 22.
In order to clearly explain the working principle of the angle iron mounting machine head of the present invention, the machine case 2 is divided into a left machine case and a right machine case with reference to the attached drawing 2:
the angle iron is correspondingly lapped on the hollow sleeves 6 in advance, an expansion bolt is placed in each hollow sleeve 6, as mentioned above, after the electric hammer 4 on the left case drills and returns, the telescopic plate of the third cylinder 13 moves leftwards, the cylinder fixing plate 12 also moves leftwards, and then the fourth cylinder 14 and the connecting screw rod 22 are driven to integrally move leftwards, so that the case 2 integrally slides leftwards, the sliding distance is the stroke of the telescopic plate of the third cylinder 13, the stroke is set through the stroke switch, and the stroke is set to be the distance between the hollow sleeve 6 and the drilling end of the electric hammer;
after the case 2 slides leftwards, the hollow sleeve 6 on the left case is just positioned at the position of a punched hole, at the moment, the telescopic rod of the second air cylinder 9 acts to lift the gear box 19, so that the hollow sleeve 6 is driven to lift to the punching plane, at the moment, the telescopic rod of the striking air cylinder 18 penetrates through the inner cavity of the hollow sleeve 6, an expansion bolt is driven into the punched hole, the air screwdriver 7 is started, the hollow sleeve 6 starts to rotate, the nut on the air screwdriver gradually fastens the angle iron on the punching plane to complete the installation of one end of the angle iron, then, the telescopic rod of the striking air cylinder 18 and the telescopic rod of the second air cylinder 9 return rapidly, the air screwdriver 7 stops acting, and the telescopic plate of the third air cylinder also returns rapidly;
as mentioned above, after the installation of one end of the angle iron is completed, the principle of punching and installation of the other end is the same as above, and will not be described herein again. It should be noted that the rightward sliding and returning of the casing 2 is directly performed by the rightward movement or returning of the telescopic plate of the fourth cylinder 14.
In the description of the present invention, it should be noted that the terms "vertical", "left", "right", "horizontal" and the like indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, and are only for convenience of description and simplification of the description, but do not indicate or imply that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation, and thus should not be construed as limiting the present invention. Furthermore, "first," "second," and "third" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance.
The above are merely examples of the present application and are not intended to limit the present application. Various modifications and changes may occur to those skilled in the art. Any modification, equivalent replacement, improvement, etc. made within the spirit and principle of the present application should be included in the scope of the claims of the present application.

Claims (8)

1. An angle bar installation aircraft nose, its characterized in that: comprises a base (1), two cases (2) are symmetrically arranged on the base (1), a moving component is arranged on the side wall of one long edge of the base (1), the moving component is connected with a connecting screw rod (22), the connecting screw rod (22) passes through a connecting hole (16) arranged in the middle of the bottom of each case (2), fastening nuts are arranged on two sides of the connecting hole (16), a sliding mechanism is arranged between the base (1) and the two cases (2), a column plate (3) is arranged in the middle of the top of each case (2), a first cylinder (11) and a striking cylinder (18) are respectively arranged on two sides of the upright column plate (3), a second cylinder (9) is arranged on the inner side of the two upright column plates (3) in the opposite direction, the telescopic link of first cylinder (11) all connects in the mechanism of punching, the telescopic link of second cylinder (9) all connects in installation mechanism.
2. The angle iron mounting head as claimed in claim 1, wherein: every the inside of quick-witted case (2) all is equipped with solenoid valve subassembly (20), two first cylinders (11) and two striking cylinders (18), the top of quick-witted case (2) is all vertically passed to the telescopic link of first cylinder (11) and the telescopic link of striking cylinder (18), and first cylinder (11) are located the inboard of two quick-witted case (2) relative directions, strikes cylinder (18) and is located the outside of two quick-witted case (2) relative directions.
3. The angle iron mounting head as claimed in claim 1, wherein: slide mechanism includes slider (17) and guide rail (21), be equipped with two guide rail (21) along its long limit direction symmetry on base (1), the bottom of machine case (2) all is equipped with multiunit slider (17), slider (17) and guide rail (21) cooperation setting.
4. The angle iron mounting head as claimed in claim 3, wherein: the cross section of the guide rail (21) presents a straight arch shape with a central part depressed inwards.
5. The angle iron mounting head as claimed in claim 1, wherein: the punching mechanism comprises an electric hammer (4), the electric hammer (4) is fixed on the mounting plate (23), and the telescopic rod of the first air cylinder (11) is connected to the mounting plate (23).
6. The angle iron mounting head as claimed in claim 5, wherein: the drilling end circumference of electric hammer (4) is equipped with connects ash box (5), and guide arm (10) are vertically passed in proper order in the top of quick-witted case (2), mounting panel (23) and the bottom of connecting ash box (5), and guide arm (10) are fixed in column plate (3).
7. The angle iron mounting head as claimed in claim 1, wherein: installation mechanism includes that cavity sleeve (6), wind criticize (7), gear box (19) and rotatory die clamping cylinder (8), the one end of gear box (19) sets up with the output cooperation of wind criticizing (7), the other end of gear box (19) runs through and is equipped with cavity sleeve (6), the output circumference of wind criticizing (7) is equipped with fixed plate (24), rotatory die clamping cylinder (8) are fixed in fixed plate (24), rotatory die clamping cylinder (8) are located one side of gear box (19), the telescopic link of second cylinder (9) is fixed in the shell of fixed plate (24) and gear box (19) in proper order, strike the telescopic link accessible of cylinder (18) the inner chamber of cavity sleeve (6), four position between cavity sleeve (6) is corresponding to four mounting holes of angle bar.
8. The angle iron mounting head as claimed in claim 1, wherein: the movable assembly comprises a third cylinder (13) and a fourth cylinder (14), the expansion plate of the third cylinder (13) and the expansion plate of the fourth cylinder (14) are oppositely arranged and are arranged outwards, the third cylinder (13) is horizontally fixed on the side wall of one long edge of the base (1), a cylinder fixing plate (12) is fixedly arranged on the expansion plate of the third cylinder (13), the cylinder fixing plate (12) is fixed on the cylinder body of the fourth cylinder (14), and the expansion plate of the fourth cylinder (14) is connected with the connecting screw rod (22) through an L-shaped rod (15).
CN201921130246.5U 2019-07-18 2019-07-18 Angle bar installation aircraft nose Active CN210256011U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201921130246.5U CN210256011U (en) 2019-07-18 2019-07-18 Angle bar installation aircraft nose

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201921130246.5U CN210256011U (en) 2019-07-18 2019-07-18 Angle bar installation aircraft nose

Publications (1)

Publication Number Publication Date
CN210256011U true CN210256011U (en) 2020-04-07

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Family Applications (1)

Application Number Title Priority Date Filing Date
CN201921130246.5U Active CN210256011U (en) 2019-07-18 2019-07-18 Angle bar installation aircraft nose

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CN (1) CN210256011U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112873566A (en) * 2021-02-05 2021-06-01 保利长大海外工程有限公司 Automatic punching equipment and automatic fastener installation equipment

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112873566A (en) * 2021-02-05 2021-06-01 保利长大海外工程有限公司 Automatic punching equipment and automatic fastener installation equipment

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