CN108526860A - A kind of aircraft tail propeller fixed clamp puts together machines people - Google Patents
A kind of aircraft tail propeller fixed clamp puts together machines people Download PDFInfo
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- CN108526860A CN108526860A CN201810665299.0A CN201810665299A CN108526860A CN 108526860 A CN108526860 A CN 108526860A CN 201810665299 A CN201810665299 A CN 201810665299A CN 108526860 A CN108526860 A CN 108526860A
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- 238000009434 installation Methods 0.000 claims description 8
- 239000002245 particle Substances 0.000 claims description 8
- 239000000463 material Substances 0.000 claims description 6
- 238000010276 construction Methods 0.000 claims description 3
- 239000007787 solid Substances 0.000 claims description 3
- 238000000034 method Methods 0.000 abstract description 10
- 230000008569 process Effects 0.000 abstract description 10
- 230000009471 action Effects 0.000 description 10
- 238000004519 manufacturing process Methods 0.000 description 5
- 238000003032 molecular docking Methods 0.000 description 3
- 238000010586 diagram Methods 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 230000006872 improvement Effects 0.000 description 2
- 230000007246 mechanism Effects 0.000 description 2
- 239000002002 slurry Substances 0.000 description 2
- 229920002472 Starch Polymers 0.000 description 1
- 229910000831 Steel Inorganic materials 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 125000004122 cyclic group Chemical group 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 235000019698 starch Nutrition 0.000 description 1
- 239000008107 starch Substances 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
- B23P19/00—Machines for simply fitting together or separating metal parts or objects, or metal and non-metal parts, whether or not involving some deformation; Tools or devices therefor so far as not provided for in other classes
- B23P19/04—Machines for simply fitting together or separating metal parts or objects, or metal and non-metal parts, whether or not involving some deformation; Tools or devices therefor so far as not provided for in other classes for assembling or disassembling parts
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- Engineering & Computer Science (AREA)
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- Jigs For Machine Tools (AREA)
Abstract
It puts together machines people the present invention relates to a kind of aircraft tail propeller fixed clamp, including rotating adjustable plate, the lower end of rotation adjustable plate is uniformly disposed with clamping auxiliary device, the lower end of clamping and fixing device is uniformly disposed with clamping auxiliary device, the clamping and fixing device includes the clamping regulation motor being mounted on by motor cabinet on rotation adjustable plate, it is clamped on the output shaft of regulation motor and clamping adjustment barrel is installed, the lower end of clamping adjustment barrel is equipped with clamp standoff plate, and clamp standoff plate is in ring-shaped structure.The present invention can solve manually to need to be fixed by tools such as ropes by existing lifting equipment transporting threads paddle present in existing aircraft tail propeller assembling process, artificial fixation is not firm, there are security risks during handling, complicated for operation, labor intensity problems low with working efficiency etc. greatly, may be implemented the function that aircraft tail propeller machine grips.
Description
Technical field
The present invention relates to aircraft manufacturing mounting technology apparatus field, specifically a kind of aircraft tail propeller geometrical clamp
Hold the people that puts together machines.
Background technology
Aircraft assembly is the important link of aircraft manufacturing, is ensured between part and part, part and tooling, tooling and tooling
Coordination, and then ensure Assembly veracity aircraft manufacturing coordination mode be aircraft manufacturing important feature, aircraft assembly
The assembling between the propeller and fuselage on aircraft tail is one of most important link of aircraft manufacturing, airplane tail in the process
It manually needs to be consolidated by tools such as ropes by existing lifting equipment transporting threads slurry in wing propeller assembling process
Fixed, artificial fixation is not firm, and there are security risks during handling, complicated for operation, and labor intensity is big, and working efficiency is low.
Invention content
To solve the above-mentioned problems, it puts together machines people the present invention provides a kind of aircraft tail propeller fixed clamp, it can
To solve manually to starch needs by existing lifting equipment transporting threads present in existing aircraft tail propeller assembling process
It is fixed by tools such as ropes, artificial fixation is not firm, and there are security risk, complicated for operation, labor during handling
Fatigue resistance problems low with working efficiency etc. greatly, may be implemented the function that aircraft tail propeller machine grips, and be not necessarily to people
Work operates, and has many advantages, such as that docking is accurate, stability is good, easy to operate, labor intensity is small and work efficiency is high.
To achieve the goals above, the present invention is realized using following technical scheme：A kind of aircraft tail propeller is fixed
The people that puts together machines is clamped, including rotation adjustable plate, the lower end for rotating adjustable plate are uniformly disposed with clamping auxiliary device, are clamped
The lower end of fixing device is uniformly disposed with clamping auxiliary device, and clamping and fixing device can be according to the structure of propeller ontology
Feature is wrapped, and clamping auxiliary device can assist clamping and fixing device that operation, nothing is fixed to propeller ontology
Manual operation is needed, the labor intensity of staff is reduced, improves the efficiency of work.
The clamping and fixing device includes the clamping regulation motor being mounted on by motor cabinet on rotation adjustable plate, and clamping is adjusted
It saves and clamping adjustment barrel is installed on the output shaft of motor, the lower end that adjustment barrel is clamped is equipped with clamp standoff plate, clamp standoff plate
In ring-shaped structure, and clamp standoff plate upper edge its circumferential direction is evenly arranged with location and installation slot, clamping adjustment barrel and rotation
It is connected with clamping accessory plate between adjustable plate, and accessory plate is clamped and is mounted on rotation adjustable plate by sliding matching mode, folder
It holds adjustment barrel upper edge its circumferential direction and is evenly arranged with and grip slot；Described grip in slot is connected with folder by axis pin
Fixed plate is held, is equipped on the madial wall of gripping and fixed plate and grips block, block is gripped and is made of rubber material, and is pressed from both sides
It holds and is provided with friction particles on fixed block, clamping driver slot is provided on the lateral wall of gripping and fixed plate, is pacified on clamp standoff plate
Equipped with clamping telescopic cylinder, the top that telescopic cylinder is clamped is mounted on by flange on clamping bogie, and clamping bogie is in circle
Cyclic structure, and inner wall upper edge its circumferential direction that bogie is clamped is evenly provided with clamp standoff bar, on clamp standoff bar
Clamping driven roller is installed by bearing, clamping driven roller is connected by sliding matching mode with clamping driver slot；The clamping
Adjustment barrel is hollow-core construction, and the diameter that adjustment barrel is clamped is sequentially reduced from top to bottom.By the way that regulation motor control clamping is clamped
Adjustment barrel is rotated, and to enable clamping adjustment barrel accurately to carry out package operation to propeller ontology, the gas that stretches is clamped
Cylinder control clamping bogie carries out telescopic adjustment movement, and clamping bogie drives clamping driven roller to folder during movement
It holds fixed plate to be squeezed, gripping and fixed plate drives under the action of by external force grips block to the propeller that wraps
Ontology carries out extruding fixed operation, and frictional force between propeller ontology can be increased by gripping the friction particles on block,
So that it is guaranteed that can carry out the stable operation that grips to propeller ontology reduces staff's without human intervention
Labor intensity improves the efficiency of work.
The clamping auxiliary device includes the auxiliary swivel mount being mounted on by axis pin on clamp standoff plate, assists swivel mount
Side wall on be connected with the top of auxiliary rotary cylinder by axis pin, assist the bottom end of rotary cylinder to be mounted on by axis pin and press from both sides
It holds in support plate, assists that auxiliary telescopic cylinder is installed on swivel mount, the top of auxiliary telescopic cylinder is mounted on auxiliary by flange
It helps on expansion bracket, by bearing installation, there are two auxiliary drive rollers on auxiliary telescopic frame, and two auxiliary drive rollers are symmetrically positioned in auxiliary
Help the left and right sides of expansion bracket；By axis pin installation, there are two auxiliary to execute frame on the auxiliary swivel mount, and two auxiliary execute
Frame is symmetrically positioned in the left and right sides for assisting swivel mount, and it is in Z-shaped structure that auxiliary, which executes frame, is installed on the side wall of auxiliary execution frame
There is auxiliary to execute slot, auxiliary, which executes, to be connected between slot and auxiliary drive roller by sliding matching mode, and auxiliary executes the side wall of frame
On be provided with auxiliary mounting groove, less important work frame is equipped with by axis pin in auxiliary mounting groove, less important work frame by axis pin with
The top of less important work cylinder is connected, and the top of less important work cylinder is mounted on auxiliary by axis pin and executes on frame, less important work
Less important work plate is equipped with by less important work spring on the side wall of frame, less important work plate is made of rubber material, and assists making
It is provided with frictional groove on the outer wall of industry plate, by assisting rotary cylinder control auxiliary swivel mount to adjust to suitable operating position,
Auxiliary telescopic cylinder operation drives two auxiliary drive rollers on auxiliary telescopic frame to carry out height adjusting, and auxiliary drive roller is being transported
Mutual cooperation band dynamic auxiliary execution frame carries out angular adjustment between executing slot with auxiliary in dynamic process, it is ensured that auxiliary execution frame
The position for propeller ontology being smoothly clamped auxiliary can be moved to, less important work cylinder controls less important work frame to propeller
The lower end of ontology is squeezed, and propeller ontology can under the action of the mutual cooperation of less important work frame and auxiliary swivel mount
Ensure to shake during conveying and hoisting, improves job stability, without human intervention, reduce work
The labor intensity of personnel improves the efficiency of work.
When work：
One, clamping operation：It is rotated by the way that regulation motor control clamping adjustment barrel is clamped, to enable clamping adjustment barrel
Enough accurately to carry out package operation to propeller ontology, clamping telescopic cylinder control clamping bogie carries out telescopic adjustment movement,
Clamping bogie is driven during movement be clamped driven roller gripping and fixed plate is squeezed, gripping and fixed plate by
Drive grips block and carries out extruding fixed operation to the propeller ontology wrapped under the action of external force, grips on block
Friction particles can increase the frictional force between propeller ontology, so that it is guaranteed that can to propeller ontology carry out it is stable
Grip operation.
Two, auxiliary clamping：By assisting rotary cylinder to control the adjusting of auxiliary swivel mount to suitable operating position, auxiliary is stretched
Contracting cylinder operation drives two auxiliary drive rollers on auxiliary telescopic frame to carry out height adjusting, mistake of the auxiliary drive roller in movement
Mutual cooperation band dynamic auxiliary execution frame carries out angular adjustment between Cheng Zhongyu auxiliary executes slot, it is ensured that auxiliary execution frame can be transported
The position for propeller ontology being smoothly clamped auxiliary is moved, less important work cylinder controls less important work frame to propeller ontology
Lower end is squeezed, and propeller ontology can ensure under the action of the mutual cooperation of less important work frame and auxiliary swivel mount
It will not shake during conveying and hoisting.
Three, handling is adjusted：Electronic sliding block is adjusted in the process of work and adjusts that cooperate between telescopic cylinder can be with
The automation adjusted before and after lifter plate carries out with upper and lower two degree of freedom is driven to adjust, rotary electric machine control rotating roller is revolved
Turn, to drive rotation adjustable plate to carry out angular adjustment, adjusts driving motor control and regulation take-up roll and rotated, to logical
Crossing steel wire cable auxiliary rotating roller drives rotation adjustable plate to carry out angular adjustment, improves the stability of angular adjustment work, adjusts
Section positioning cylinder control and regulation locating piece, which moves to adjust, may insure that rotating roller is stablized in specified operating position in locating slot
Operation
Four, positioning docking：Positioning adjusts cylinder control positioning execution column and carries out telescopic adjustment, to drive positioning to execute column
On positioning operation mechanism be tightly attached on fuselage, the positioning buffer spring in positioning operation mechanism and positioning sliding bar between phase
Mutually cooperation may insure that positioning sucker disk can be tightly attached on fuselage, the external existing vacuum air pump of positioning sucker disk, existing vacuum
Positioning is executed that column is stable is fixed on fuselage outer wall by air pump by positioning sucker disk in the process of work, in propeller sheet
During body is docked with fuselage, positioning sucker disk is fixed on fuselage outer wall, the process of Locating driver motor control positioning leading screw
In by reversely operated principle, drive the present invention that propeller ontology is docked on fuselage, so that it is guaranteed that propeller ontology can
Accurately it is docked on fuselage.
The beneficial effects of the invention are as follows：
1, the present invention can solve present in existing aircraft tail propeller assembling process manually by existing lifting
Equipment conveying propeller needs are fixed by tools such as ropes, and artificial fixation is not firm, there is peace during handling
Aircraft tail propeller machineization folder may be implemented in full hidden danger, complicated for operation, labor intensity problems low with working efficiency etc. greatly
Fixed function is held, without human intervention, and accurate, stability is good, easy to operate, labor intensity is small and works with docking
The advantages that efficient.
2, the present invention devises clamping and fixing device, and clamping telescopic cylinder drives clamping driven roller to carry out gripping and fixed plate
It squeezes, gripping and fixed plate drives under the action of by external force to be gripped block and squeeze the propeller ontology wrapped
Fixed operation, frictional force between propeller ontology can be increased by gripping the friction particles on block, so that it is guaranteed that can
Propeller ontology is carried out stable to grip operation.
3, the present invention devises clamping auxiliary device, and less important work cylinder controls less important work frame under propeller ontology
End is squeezed, and propeller ontology can ensure under the action of the mutual cooperation of less important work frame and auxiliary swivel mount defeated
It will not shake during sending handling, improve job stability.
Description of the drawings
Present invention will be further explained below with reference to the attached drawings and examples.
Fig. 1 is the structural schematic diagram of the present invention；
Fig. 2 is the sectional view between present invention rotation adjustable plate and clamping and fixing device；
Fig. 3 is the structural schematic diagram between clamp standoff plate of the present invention and clamping auxiliary device.
Specific implementation mode
In order to make the technical means, the creative features, the aims and the efficiencies achieved by the present invention be easy to understand, tie below
Conjunction is specifically illustrating, and the present invention is further explained.
As shown in Fig. 1 to Fig. 3, a kind of aircraft tail propeller fixed clamp puts together machines people, including rotation adjustable plate 28,
The lower end of rotation adjustable plate 28 is equipped with clamping and fixing device 3, and it is auxiliary that the lower end of clamping and fixing device 3 is uniformly disposed with clamping
It helps device 4, clamping and fixing device 3 that can be wrapped according to the structure feature of propeller ontology 7, auxiliary device 4 is clamped
It can assist clamping and fixing device 3 that operation is fixed to propeller ontology 7, without human intervention, reduce staff's
Labor intensity improves the efficiency of work.
The clamping and fixing device 3 includes the clamping regulation motor 31 being mounted on by motor cabinet on rotation adjustable plate 28,
It is clamped on the output shaft of regulation motor 31 and clamping adjustment barrel 32 is installed, the lower end of clamping adjustment barrel 32 is equipped with clamp standoff
Plate 33, clamp standoff plate 33 is in ring-shaped structure, and 33 upper edge of clamp standoff plate its circumferential direction is evenly arranged with location and installation
Slot is clamped between adjustment barrel 32 and rotation adjustable plate 28 and is connected with clamping accessory plate 34, and accessory plate 34 is clamped and is matched by sliding
Conjunction mode is mounted on rotation adjustable plate 28, its circumferential direction of clamping 32 upper edge of adjustment barrel, which is evenly arranged with, grips slot；Institute
It states to grip in slot and gripping and fixed plate 35 is connected with by axis pin, clamping is installed solid on the madial wall of gripping and fixed plate 35
Determine block 36, grips block 36 and be made of rubber material, and grip and be provided with friction particles, gripping and fixed plate on block 36
It is provided with clamping driver slot 37 on 35 lateral wall, clamping telescopic cylinder 38 is installed on clamp standoff plate 33, the gas that stretches is clamped
The top of cylinder 38 is mounted on by flange on clamping bogie 39, and clamping bogie 39 is in ring-shaped structure, and bogie is clamped
Its circumferential direction of 39 inner wall upper edge is evenly provided with clamp standoff bar 310, is installed by bearing on clamp standoff bar 310
There are clamping driven roller 311, clamping driven roller 311 to be connected with clamping driver slot 37 by sliding matching mode；The clamping is adjusted
Cylinder 32 is hollow-core construction, and the diameter that adjustment barrel 32 is clamped is sequentially reduced from top to bottom.By the way that the control folder of regulation motor 31 is clamped
Adjustment barrel 32 is held to be rotated, to enable clamping adjustment barrel 32 accurately to carry out package operation to propeller ontology 7, clamping
The control clamping bogie 39 of telescopic cylinder 38 carries out telescopic adjustment movement, and clamping bogie 39 drives folder during movement
It holds driven roller 311 to squeeze gripping and fixed plate 35, gripping and fixed plate 35 drives under the action of by external force and grips
Block 36 carries out extruding fixed operation to the propeller ontology 7 wrapped, grip the friction particles on block 36 can increase with
Frictional force between propeller ontology 7, so that it is guaranteed that propeller ontology 7 can be carried out it is stable grip operation, be not necessarily to
Manual operation reduces the labor intensity of staff, improves the efficiency of work.
The clamping auxiliary device 4 includes the auxiliary swivel mount 41 being mounted on by axis pin on clamp standoff plate 33, auxiliary
It is connected with the top of auxiliary rotary cylinder 42 by axis pin on the side wall of swivel mount 41, the bottom end of auxiliary rotary cylinder 42 passes through
Axis pin is mounted on clamp standoff plate 33, assists being equipped with auxiliary telescopic cylinder 43 on swivel mount 41, auxiliary telescopic cylinder 43
Top is mounted on by flange on auxiliary telescopic frame 44, and by bearing installation, there are two auxiliary drive rollers on auxiliary telescopic frame 44
45, two auxiliary drive rollers 45 are symmetrically positioned in the left and right sides of auxiliary telescopic frame 44；Pass through axis pin on the auxiliary swivel mount 41
There are two auxiliary to execute frame 46 for installation, and two auxiliary execute the left and right sides that frame 46 is symmetrically positioned in auxiliary swivel mount 41, and auxiliary is held
Row frame 46 is in Z-shaped structure, and being equipped with auxiliary on the side wall of auxiliary execution frame 46 executes slot 47, and auxiliary executes slot 47 and auxiliary
It is connected by sliding matching mode between driven roller 45, auxiliary mounting groove, auxiliary peace is provided on the side wall of auxiliary execution frame 46
Less important work frame 48, the top that less important work frame 48 passes through axis pin and less important work cylinder 49 are equipped with by axis pin in tankage
It is connected, the top of less important work cylinder 49 is mounted on auxiliary by axis pin and executes on frame 46, leads on the side wall of less important work frame 48
It crosses less important work spring 410 and less important work plate 411 is installed, less important work plate 411 is made of rubber material, and less important work
It is provided with frictional groove on the outer wall of plate 411, by assisting the control auxiliary swivel mount 41 of rotary cylinder 42 to adjust to suitable work
Position, the work of auxiliary telescopic cylinder 43 drive two auxiliary drive rollers 45 on auxiliary telescopic frame 44 to carry out height adjusting, auxiliary
Mutual cooperation band dynamic auxiliary execution frame 46 carries out angle tune between driven roller 45 executes slot 47 during movement with auxiliary
Section, it is ensured that auxiliary, which executes frame 46, can move to the position for propeller ontology 7 being smoothly clamped auxiliary, less important work cylinder 49
Control less important work frame 48 squeezes the lower end of propeller ontology 7, and propeller ontology 7 is in less important work frame 48 and auxiliary
It can ensure shake during conveying and hoisting under the action of the mutual cooperation of swivel mount 41, improve work
Stability reduces the labor intensity of staff without human intervention, improves the efficiency of work.
When work：
One, clamping operation：It is rotated by the way that the control clamping adjustment barrel 32 of regulation motor 31 is clamped, to make clamping adjust
Cylinder 32 accurately can carry out package operation to propeller ontology 7, and the clamping control clamping bogie 39 of telescopic cylinder 38 is stretched
Contracting adjusts movement, and clamping bogie 39 drives clamping driven roller 311 to squeeze gripping and fixed plate 35 during movement
Pressure, gripping and fixed plate 35 drives under the action of by external force to be gripped block 36 and is squeezed to the propeller ontology 7 wrapped
Fixed operation is pressed, frictional force between propeller ontology 7 can be increased by gripping the friction particles on block 36, to really
Propeller ontology 7 can be carried out stable to grip operation by protecting.
Two, auxiliary clamping：Suitable operating position is arrived by assisting the control auxiliary swivel mount 41 of rotary cylinder 42 to adjust, it is auxiliary
Help the work of telescopic cylinder 43 that two auxiliary drive rollers 45 on auxiliary telescopic frame 44 is driven to carry out height adjusting, auxiliary drive roller
45 cooperate during movement between auxiliary execution slot 47 carries out angular adjustment with dynamic auxiliary execution frame 46, it is ensured that
Auxiliary executes frame 46 and can move to the position that smoothly clamping assists of propeller ontology 7, the control auxiliary of less important work cylinder 49
Operation frame 48 squeezes the lower end of propeller ontology 7, and propeller ontology 7 is in less important work frame 48 and auxiliary swivel mount 41
Mutual cooperation under the action of can ensure shake during conveying and hoisting.
The present invention realizes the function that aircraft tail propeller machine grips, and solves existing aircraft tail spiral
It manually needs to be consolidated by tools such as ropes by existing lifting equipment transporting threads slurry present in paddle assembling process
Fixed, artificial fixation is not firm, complicated for operation, labor intensity is low with working efficiency greatly there are security risk during handling
Etc. problems, reached purpose
The basic principles, main features and advantages of the invention have been shown and described above.The technical staff of the industry should
Understand, the present invention is not limited to the above embodiments, and the description in above embodiments and description only illustrates the present invention
Principle, without departing from the spirit and scope of the present invention, various changes and improvements may be made to the invention, these variation and
Improvement all fall within the protetion scope of the claimed invention.The claimed scope of the invention is by appended claims and its waits
Effect object defines.
Claims (4)
- The people 1. a kind of aircraft tail propeller fixed clamp puts together machines, including rotation adjustable plate (28), it is characterised in that：Rotation The lower end of adjustable plate (28) is equipped with clamping and fixing device (3), and it is auxiliary that the lower end of clamping and fixing device (3) is uniformly disposed with clamping Help device (4)；The clamping and fixing device (3) includes the clamping regulation motor being mounted on by motor cabinet on rotation adjustable plate (28) (31), clamping adjustment barrel (32), the lower end installation of clamping adjustment barrel (32) are installed on the output shaft of clamping regulation motor (31) There is clamp standoff plate (33), clamp standoff plate (33) is in ring-shaped structure, and its circumferential direction of clamp standoff plate (33) upper edge is equal It is even to be provided with location and installation slot, clamping accessory plate (34) is connected between clamping adjustment barrel (32) and rotation adjustable plate (28), and Accessory plate (34) is clamped to be mounted on rotation adjustable plate (28) by sliding matching mode, its circumferential direction of clamping adjustment barrel (32) upper edge Direction, which is evenly arranged with, grips slot；The clamping adjustment barrel (32) is hollow-core construction, and the diameter of adjustment barrel (32) is clamped It is sequentially reduced from top to bottom；The clamping auxiliary device (4) includes the auxiliary swivel mount (41) being mounted on by axis pin on clamp standoff plate (33), auxiliary It helps on the side wall of swivel mount (41) and is connected with the top of auxiliary rotary cylinder (42) by axis pin, the bottom of auxiliary rotary cylinder (42) End is mounted on by axis pin on clamp standoff plate (33), is assisted being equipped with auxiliary telescopic cylinder (43) on swivel mount (41), be assisted The top of telescopic cylinder (43) is mounted on by flange on auxiliary telescopic frame (44), and auxiliary telescopic frame is installed on (44) by bearing There are two auxiliary drive roller (45), two auxiliary drive rollers (45) are symmetrically positioned in the left and right sides of auxiliary telescopic frame (44).
- The people 2. a kind of aircraft tail propeller fixed clamp according to claim 1 puts together machines, it is characterised in that：It is described It grips in slot and gripping and fixed plate (35) is connected with by axis pin, clamping is installed solid on the madial wall of gripping and fixed plate (35) Determine block (36), grip block (36) and be made of rubber material, and grip and be provided with friction particles on block (36), clamping is solid Clamping driver slot (37) is provided on the lateral wall of fixed board (35).
- The people 3. a kind of aircraft tail propeller fixed clamp according to claim 1 puts together machines, it is characterised in that：It is described Clamping telescopic cylinder (38) is installed, the top of clamping telescopic cylinder (38) is mounted on folder by flange on clamp standoff plate (33) It holds on bogie (39), clamping bogie (39) is in ring-shaped structure, and its circumferential direction side of inner wall upper edge of bogie (39) is clamped To clamp standoff bar (310) is evenly provided with, it is equipped with by bearing on clamp standoff bar (310) and driven roller (311) is clamped, Clamping driven roller (311) is connected by sliding matching mode with clamping driver slot (37).
- The people 4. a kind of aircraft tail propeller fixed clamp according to claim 1 puts together machines, it is characterised in that：It is described It assists installing there are two auxiliary execution frame (46) by axis pin on swivel mount (41), two auxiliary execution framves (46) are symmetrically positioned in auxiliary The left and right sides of swivel mount (41) is helped, it is in Z-shaped structure that auxiliary, which executes frame (46), is equipped on the side wall of auxiliary execution frame (46) Auxiliary executes slot (47), and auxiliary, which executes, to be connected between slot (47) and auxiliary drive roller (45) by sliding matching mode, and auxiliary is held Auxiliary mounting groove is provided on the side wall of row frame (46), auxiliary mounting groove is interior to be equipped with less important work frame (48) by axis pin, auxiliary Operation frame (48) is helped to be connected with the top of less important work cylinder (49) by axis pin, the top of less important work cylinder (49) passes through pin Axis is mounted on auxiliary and executes on frame (46), is equipped with by less important work spring (410) on the side wall of less important work frame (48) auxiliary It helps operation plate (411), less important work plate (411) to be made of rubber material, and is provided with and rubs on the outer wall of less important work plate (411) Wipe slot.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810665299.0A CN108526860B (en) | 2018-06-26 | 2018-06-26 | Frock clamp is used in equipment of aircraft fin screw |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810665299.0A CN108526860B (en) | 2018-06-26 | 2018-06-26 | Frock clamp is used in equipment of aircraft fin screw |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN108526860A true CN108526860A (en) | 2018-09-14 |
| CN108526860B CN108526860B (en) | 2020-04-28 |
Family
ID=63486958
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810665299.0A Active CN108526860B (en) | 2018-06-26 | 2018-06-26 | Frock clamp is used in equipment of aircraft fin screw |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108526860B (en) |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH07227679A (en) * | 1994-02-18 | 1995-08-29 | Kanto Auto Works Ltd | Automatic spot welding equipment |
| JP2002361535A (en) * | 2001-06-08 | 2002-12-18 | Yanmar Co Ltd | Method and device for clamping thin-walled cylinder |
| DE10310421A1 (en) * | 2003-03-11 | 2004-09-23 | Eckhard Petersmann | Clamping claw to hold workpiece in position during machining has piston rod of variable diameter guided through piston bearing and bulkhead inside cylinder filled with compressible medium |
| CN104647023A (en) * | 2015-02-11 | 2015-05-27 | 无锡惠发特精密机械有限公司 | Hydraulic self-centering clamp |
| CN206680054U (en) * | 2017-04-11 | 2017-11-28 | 广和基业(天津)有限公司 | A kind of Automatic hook block for pipe pile die lifting |
| CN108792970A (en) * | 2018-06-26 | 2018-11-13 | 周昀锴 | A kind of aircraft assembly hoisting aids machinery |
-
2018
- 2018-06-26 CN CN201810665299.0A patent/CN108526860B/en active Active
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH07227679A (en) * | 1994-02-18 | 1995-08-29 | Kanto Auto Works Ltd | Automatic spot welding equipment |
| JP2002361535A (en) * | 2001-06-08 | 2002-12-18 | Yanmar Co Ltd | Method and device for clamping thin-walled cylinder |
| DE10310421A1 (en) * | 2003-03-11 | 2004-09-23 | Eckhard Petersmann | Clamping claw to hold workpiece in position during machining has piston rod of variable diameter guided through piston bearing and bulkhead inside cylinder filled with compressible medium |
| CN104647023A (en) * | 2015-02-11 | 2015-05-27 | 无锡惠发特精密机械有限公司 | Hydraulic self-centering clamp |
| CN206680054U (en) * | 2017-04-11 | 2017-11-28 | 广和基业(天津)有限公司 | A kind of Automatic hook block for pipe pile die lifting |
| CN108792970A (en) * | 2018-06-26 | 2018-11-13 | 周昀锴 | A kind of aircraft assembly hoisting aids machinery |
Also Published As
| Publication number | Publication date |
|---|---|
| CN108526860B (en) | 2020-04-28 |
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