CN112192464A - Shape-preserving positioning tool for composite material wing wallboard - Google Patents
Shape-preserving positioning tool for composite material wing wallboard Download PDFInfo
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- CN112192464A CN112192464A CN202010955367.4A CN202010955367A CN112192464A CN 112192464 A CN112192464 A CN 112192464A CN 202010955367 A CN202010955367 A CN 202010955367A CN 112192464 A CN112192464 A CN 112192464A
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- positioning tool
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- 239000002131 composite material Substances 0.000 title claims abstract description 19
- 230000007246 mechanism Effects 0.000 claims abstract description 45
- 239000000463 material Substances 0.000 claims description 2
- 238000004519 manufacturing process Methods 0.000 abstract description 4
- 238000000034 method Methods 0.000 description 10
- 230000000694 effects Effects 0.000 description 6
- 230000008569 process Effects 0.000 description 6
- 230000009471 action Effects 0.000 description 3
- 238000005096 rolling process Methods 0.000 description 3
- 238000009434 installation Methods 0.000 description 2
- 238000005086 pumping Methods 0.000 description 2
- 230000003466 anti-cipated effect Effects 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 238000001514 detection method Methods 0.000 description 1
- 238000003801 milling Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 238000003860 storage Methods 0.000 description 1
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B25—HAND TOOLS; PORTABLE POWER-DRIVEN TOOLS; MANIPULATORS
- B25B—TOOLS OR BENCH DEVICES NOT OTHERWISE PROVIDED FOR, FOR FASTENING, CONNECTING, DISENGAGING OR HOLDING
- B25B11/00—Work holders not covered by any preceding group in the subclass, e.g. magnetic work holders, vacuum work holders
- B25B11/005—Vacuum work holders
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
- B64F5/10—Manufacturing or assembling aircraft, e.g. jigs therefor
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- Manufacturing & Machinery (AREA)
- Transportation (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Conveying And Assembling Of Building Elements In Situ (AREA)
Abstract
The invention discloses a shape-preserving positioning tool for a composite material wing wallboard, which belongs to the technical field of aircraft manufacturing, and adopts the technical scheme that the shape-preserving positioning tool comprises a fixed frame, a control cabinet, a guide mechanism, a transverse moving mechanism, an adjusting mechanism and a positioning mechanism, wherein the top of the fixed frame is provided with the control cabinet; the guide mechanism comprises a connecting rail, and two transverse guide rails are fixedly connected to one side of the connecting rail through bolts; the transverse moving mechanism comprises a U-shaped frame which is matched on the transverse guide rail in a sliding mode, two groups of rollers which move along the extension direction of the transverse guide rail are arranged on the inner wall of the U-shaped frame, a first motor is fixedly installed at the bottom of the U-shaped frame, and an output shaft of the first motor penetrates through the U-shaped frame and is fixedly connected with one roller which is located below the U-shaped frame; the invention is convenient for adjusting the position of the wall plate during splicing, does not need to be fixed again after being released, reduces the working strength and has safer and more reliable operation.
Description
Technical Field
The invention relates to the technical field of aircraft manufacturing, in particular to a shape-preserving positioning tool for a composite material wing wallboard.
Background
The composite material has the advantages of high specific strength, high specific modulus, good heat resistance, small thermal expansion coefficient, good corrosion resistance and the like, so the composite material is very suitable to be used as a manufacturing material of an airplane. Composite materials are now being used in the construction of new generation aircraft and to significantly improve aircraft performance, and it is anticipated that composite materials will find wider and more important use in aircraft.
In the manufacturing process of large aircraft, need splice the wallboard, current concatenation mode adopts monolithic frock to fix it mostly, then splice the operation to it, but to each whole wallboard of constituteing the wing, there is the surplus of milling in the span direction, lead to single wallboard position adjustment usually when the location, nevertheless because its size is big, weight is big, it is comparatively difficult to cause to move single wallboard on the frock, just need to remove it fixedly this moment, then the adjustment position, fix again single wallboard, the working strength has been increased greatly, and the operation degree of difficulty is bigger.
Disclosure of Invention
1. Technical problem to be solved
Aiming at the problems in the prior art, the invention aims to provide a shape-preserving positioning tool for a composite material wing wallboard, which has the advantages that the position of the wallboard is convenient to adjust during splicing, the wallboard does not need to be fixed again after being released, the working strength is reduced, and the operation is safer and more reliable.
2. Technical scheme
In order to solve the above problems, the present invention adopts the following technical solutions.
A shape-preserving positioning tool for a composite material wing wallboard comprises a fixed frame, wherein a control cabinet is arranged at the top of the fixed frame, and the shape-preserving positioning tool also comprises a guide mechanism, a transverse moving mechanism, an adjusting mechanism and a positioning mechanism;
the guide mechanism comprises a connecting rail, and two transverse guide rails are fixedly connected to one side of the connecting rail through bolts;
the transverse moving mechanism comprises a U-shaped frame which is matched on the transverse guide rail in a sliding mode, two groups of rollers which move along the extension direction of the transverse guide rail are arranged on the inner wall of the U-shaped frame, a first motor is fixedly installed at the bottom of the U-shaped frame, and an output shaft of the first motor penetrates through the U-shaped frame and is fixedly connected with one roller which is located below the U-shaped frame;
the adjusting mechanism comprises a longitudinal adjusting mechanism fixed on the U-shaped frame, one side of the longitudinal adjusting mechanism is fixedly connected with a rotating cylinder, and one side of the rotating cylinder is fixedly connected with a fixing frame;
positioning mechanism is including the guarantor type frame, guarantor type frame one side fixed mounting is in the inboard of fixed frame, the inner wall fixedly connected with equidistance of guarantor type frame distributes the floor, the top fixed mounting of floor has the sucking disc subassembly.
Further, the mount includes the bottom plate, the stand that the up end middle part fixedly connected with equidistance of bottom plate distributes, the connection rail passes through the bolt fastening in one side of stand.
Furthermore, an air pump and a controller are arranged in the control cabinet, and an operation panel is further arranged on one side of the control cabinet.
Furthermore, the longitudinal adjusting mechanism comprises a longitudinal guide rail, the inner wall of the longitudinal guide rail is rotatably connected with a screw rod through a bearing, a second motor is fixedly mounted at the top of the longitudinal guide rail, an output shaft of the second motor penetrates through the longitudinal guide rail and is fixedly connected with the screw rod, a threaded sliding block located inside the longitudinal guide rail is in threaded connection with the surface of the screw rod, and the rotary cylinder is fixedly mounted on one side of the threaded sliding block.
Further, one side fixedly connected with U type fastener of guarantor's type frame, one side fixedly connected with retaining member of U type fastener, U type fastener passes through the retaining member card in the inside of fixed frame, and the inner wall of U type fastener is provided with and increases and hinder the cushion.
Furthermore, the retaining member is including fixing the thread bush in U type fastener one side, the inner wall threaded connection of thread bush has the screw rod, the one end fixedly connected with driving lever of screw rod, the other end of screw rod run through U type fastener and with the opposite side threaded connection of U type fastener.
Furthermore, the sucking disc subassembly includes electric putter, electric putter's one end fixedly connected with high strength sucking disc, the back of high strength sucking disc is provided with the exhaust tube joint.
Further, the air suction pipe joint is connected with an air pump through a hose.
Furthermore, a rolling distance meter is arranged at the top of the U-shaped frame and connected with one of the rollers above the rolling distance meter.
3. Advantageous effects
Compared with the prior art, the invention has the advantages that:
(1) in the splicing process, the operation of the first motor is controlled, one roller is driven to rotate by the work of the first motor, the roller moves along the transverse guide rail when rotating, so that the wall plates can be driven to transversely move through the U-shaped frame and the longitudinal adjusting mechanism, the distance between the two wall plates can be adjusted, the two wall plates can be conveniently contacted, the alignment of the wall plates is completed, the subsequent splicing can be carried out, the angle of the wall plates can be adjusted through the action of the rotary cylinder, when the angle of the wall plates deviates, the angle of the wall plates can be adjusted through the rotation of the rotary cylinder, when the position of the wing wall plate deviates in the vertical direction, the operation of the second motor can be controlled through the controller, the second motor drives the screw rod to rotate, the screw thread sliding block is driven to move up and down when the screw rod rotates, and the fixed frame is driven to move through the cooperation, thereby achieving the effect of adjusting the wall plate up and down without dismounting and fixing the wall plate again;
() When the shape-preserving frame is used for positioning the wall plate, the high-strength sucker is pushed by the electric push rod to be tightly attached to the surface of the wall plate, and then air is exhausted by the air exhaust pipe joint, so that the function of adsorbing the wall plate is achieved, the traditional clamping type fixing is realized, and the damage to the wall plate is reduced;
() According to the scheme, when the shape-preserving frame is installed, the U-shaped fastener is buckled inside the fixed frame, then the U-shaped fastener is locked by the deflector rod, and can be tightly clamped on the fixed frame in the locking process of the U-shaped fastener, so that the installation of the shape-preserving frame can be rapidly completed, and when the U-shaped fastener needs to be disassembled later, the deflector rod is rotated reversely, the locking of the U-shaped fastener is released, so that the U-shaped fastener can be rapidly taken down from the fixed frame, and the disassembly is very convenient;
() This scheme removes the in-process at U type frame, and the gyro wheel rolls along transverse guide, and the gyro wheel rotates the in-process, and the rotation number of turns of gyro wheel is recorded to the roll distancer, because the girth of gyro wheel is the definite value, consequently can be quick reachs the distance that U type frame removed, is convenient for carry out accurate adjustment to the position of wallboard.
Drawings
FIG. 1 is a schematic structural view of the present invention;
FIG. 2 is a schematic view of a shape-retaining frame according to the present invention;
FIG. 3 is a schematic structural view of the traversing mechanism according to the present invention;
FIG. 4 is a schematic structural view of the longitudinal adjustment mechanism of the present invention;
FIG. 5 is a schematic view of the locking member of the present invention;
FIG. 6 is a schematic view of the structure of the chuck assembly of the present invention;
fig. 7 is an enlarged view of the invention at a in fig. 2.
The reference numbers in the figures illustrate:
1. a fixed mount; 101. a base plate; 102. a column; 2. a control cabinet; 3. connecting rails; 4. a transverse guide rail; 5. a U-shaped frame; 6. a roller; 7. a longitudinal adjustment mechanism; 701. a longitudinal guide rail; 702. a screw rod; 703. a second motor; 8. a rotating cylinder; 9. a fixing frame; 10. a shape-preserving frame; 11. a rib plate; 12. a sucker component; 1201. an electric push rod; 1202. a high-strength suction cup; 1203. an air exhaust pipe joint; 13. a first motor; 14. a U-shaped fastener; 15. a locking member; 1501. a threaded sleeve; 1502. a screw; 1503. a deflector rod; 16. a rolling distance meter.
Detailed Description
The technical solution in the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present invention; it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all embodiments, and all other embodiments obtained by those skilled in the art without any inventive work are within the scope of the present invention.
Referring to fig. 1-7, in an embodiment of the present invention, a conformal positioning tool for a composite material wing wall plate includes a fixed frame 1, a control cabinet 2 is disposed on the top of the fixed frame 1, and further includes a guiding mechanism, a traversing mechanism, an adjusting mechanism, and a positioning mechanism; the guide mechanism comprises a connecting rail 3, and one side of the connecting rail 3 is fixedly connected with two transverse guide rails 4 through bolts; the positioning mechanism comprises a shape-preserving frame 10, one side of the shape-preserving frame 10 is fixedly arranged on the inner side of the fixed frame 9, rib plates 11 which are distributed at equal intervals are fixedly connected to the inner wall of the shape-preserving frame 10, and a sucker component 12 is fixedly arranged at the top of each rib plate 11 and used for positioning the wing wall plate; the air pumping pipe joint 1203 is connected with an air pump through a hose, and the air pump pumps air inside the high-strength suction cup 1202 through the hose and the air pumping pipe joint 1203, so that the internal pressure is reduced, and the effect of adsorbing the wing wall plate is achieved.
Referring to fig. 1, the fixing frame 1 includes a bottom plate 101, a vertical column 102 is fixedly connected to the middle of the upper end face of the bottom plate 101 and is equidistantly distributed, the connecting rail 3 is fixed to one side of the vertical column 102 through bolts, and after detection is completed, the bolts can be detached subsequently, the connecting rail 3 is detached, and subsequent transportation or storage is facilitated.
Referring to fig. 1, an air pump and a controller are arranged inside a control cabinet 2, an operation panel is further arranged on one side of the control cabinet 2, the controller is used for controlling the operation of the whole equipment, the air pump is used for providing driving force for an air cylinder and the like, and the operation panel is convenient for a worker to operate the equipment.
Referring to fig. 3, the transverse moving mechanism comprises a U-shaped frame 5 slidably fitted on the transverse guide rail 4, two sets of rollers 6 moving along the extending direction of the transverse guide rail 4 are arranged on the inner wall of the U-shaped frame 5, a first motor 13 is fixedly mounted at the bottom of the U-shaped frame 5, an output shaft of the first motor 13 penetrates through the U-shaped frame 5 and is fixedly connected with one roller 6 located below the U-shaped frame, during the splicing process, one roller 6 is driven to rotate by controlling the operation of the first motor 13, the roller 6 moves along the transverse guide rail 4 when rotating, so that the transverse moving of the wall plates can be driven by the U-shaped frame 5 and the longitudinal adjusting mechanism 7, the distance between the two wall plates can be adjusted, the two wall plates can be conveniently contacted, the alignment of the wall plates can be completed, and the subsequent splicing can be performed;
referring to fig. 3, the adjusting mechanism comprises a longitudinal adjusting mechanism 7 fixed on the U-shaped frame 5, one side of the longitudinal adjusting mechanism 7 is fixedly connected with a rotary cylinder 8, one side of the rotary cylinder 8 is fixedly connected with a fixed frame 9, the angle of the wall plate can be adjusted under the action of the rotary cylinder 8, and when the angle of the wall plate deviates, the angle of the wall plate can be adjusted through the rotation of the rotary cylinder 8 without being detached and fixed again; the top of U type frame 5 is provided with roll distancer 16, and roll distancer 16 is connected with one of them gyro wheel 6 that is located the top, removes the in-process at U type frame 5, and gyro wheel 6 rolls along transverse guide 4, and gyro wheel 6 rotates the in-process, and roll distancer 16 records the number of turns of gyro wheel 6, because the girth of gyro wheel 6 is the definite value, consequently can be quick reachs the distance that U type frame 5 removed, is convenient for carry out accurate adjustment to the position of wallboard.
Referring to fig. 3 and 4, the longitudinal adjustment mechanism 7 includes a longitudinal guide rail 701, the inner wall of the longitudinal guide rail 701 is rotatably connected with a screw rod 702 through a bearing, a second motor 703 is fixedly installed at the top of the longitudinal guide rail 701, an output shaft of the second motor 703 penetrates through the longitudinal guide rail 701 and is fixedly connected with the screw rod 702, a threaded slider 704 located inside the longitudinal guide rail 701 is connected to a surface thread of the screw rod 702, the threaded slider 704 is fixedly installed at one side of the threaded slider 704, when a deviation in the vertical direction occurs at the position of the wing panel, the second motor 703 is controlled to operate by a controller, the second motor 703 operates to drive the screw rod 702 to rotate, the screw rod 702 drives the threaded slider 704 to move up and down when rotating, and then the threaded slider 704 cooperates with the rotary cylinder 8 to drive the fixed frame 9 to move, thereby achieving the effect.
Referring to fig. 2 and 7, one side of the shape-preserving frame 10 is fixedly connected with a U-shaped fastener 14, one side of the U-shaped fastener 14 is fixedly connected with a locking member 15, the U-shaped fastener 14 is clamped inside the fixing frame 9 through the locking member 15, and the inner wall of the U-shaped fastener 14 is provided with a resistance-increasing rubber mat for increasing the friction between the U-shaped fastener 14 and the fixing frame 9, so that the fixing effect is better.
Referring to fig. 2 and 5, the locking member 15 includes a thread sleeve 1501 fixed on one side of the U-shaped fastener 14, a screw 1502 is connected to an inner wall of the thread sleeve 1501 in a threaded manner, a driving lever 1503 is fixedly connected to one end of the screw 1502, and the other end of the screw 1502 penetrates through the U-shaped fastener 14 and is in threaded connection with the other side of the U-shaped fastener 14, when the shape-preserving frame 10 is installed, the U-shaped fastener 14 is buckled inside the fixing frame 9, and then the driving lever 1503 is used for locking the U-shaped fastener 14, and the U-shaped fastener 14 is tightly clamped on the fixing frame 9 in the locking process, so that the installation of the shape-preserving frame 10 can be rapidly completed, and when the U-shaped fastener 14 needs to be disassembled, the driving lever 1503 is reversely rotated to release the locking of the U-shaped fastener 14, so that the U-.
Referring to fig. 6, the suction cup assembly 12 includes an electric push rod 1201, one end of the electric push rod 1201 is fixedly connected with a high-strength suction cup 1202, and an exhaust pipe joint 1203 is arranged on the back surface of the high-strength suction cup 1202, in the using process, the high-strength suction cup 1202 is pushed by the electric push rod 1201 to be tightly attached to the surface of the wall plate, and then air is exhausted by matching the exhaust pipe joint 1203, so that the function of adsorbing the wall plate is achieved, the traditional clamping type is fixed, and damage to the wall plate is reduced.
The working principle of the invention is as follows: in the splicing process, the operation of the first motor 13 is controlled, the first motor 13 works to drive one roller 6 to rotate, the roller 6 moves along the transverse guide rail 4 when rotating, so that the wall plates can be driven to transversely move through the U-shaped frame 5 and the longitudinal adjusting mechanism 7, the distance between the two wall plates can be adjusted, the two wall plates can be conveniently contacted to complete the alignment of the wall plates, the subsequent splicing can be carried out, the angle of the wall plates can be adjusted through the action of the rotary air cylinder 8, when the angle of the wall plates deviates, the angle of the wall plates can be adjusted through the rotation of the rotary air cylinder 8, when the position of the wing wall plate deviates in the vertical direction, the second motor 703 can be controlled to operate through the controller, the second motor 703 operates to drive the screw rod 702 to rotate, the screw thread sliding block 704 is driven to move up and down when the screw rod 702 rotates, and the screw thread sliding block 704 is matched with the rotary air cylinder, thereby reach the effect of adjustment wallboard vertical adjustment and need not to pull down it and fix again.
The above are merely preferred embodiments of the present invention; the scope of the invention is not limited thereto. Any person skilled in the art should be able to cover the technical scope of the present invention by equivalent or modified solutions and modifications within the technical scope of the present invention.
Claims (9)
1. The utility model provides a shape preserving location frock for combined material wing wallboard, includes mount (1), the top of mount (1) is provided with switch board (2), its characterized in that: the device also comprises a guide mechanism, a transverse moving mechanism, an adjusting mechanism and a positioning mechanism;
the guide mechanism comprises a connecting rail (3), and one side of the connecting rail (3) is fixedly connected with two transverse guide rails (4) through bolts;
the transverse moving mechanism comprises a U-shaped frame (5) which is matched on the transverse guide rail (4) in a sliding mode, two groups of rollers (6) which move along the extending direction of the transverse guide rail (4) are arranged on the inner wall of the U-shaped frame (5), a first motor (13) is fixedly installed at the bottom of the U-shaped frame (5), and an output shaft of the first motor (13) penetrates through the U-shaped frame (5) and is fixedly connected with one roller (6) located below the U-shaped frame;
the adjusting mechanism comprises a longitudinal adjusting mechanism (7) fixed on the U-shaped frame (5), one side of the longitudinal adjusting mechanism (7) is fixedly connected with a rotating cylinder (8), and one side of the rotating cylinder (8) is fixedly connected with a fixing frame (9);
positioning mechanism is including guarantor type frame (10), guarantor type frame (10) one side fixed mounting is in the inboard of fixed frame (9), the inner wall fixedly connected with equidistance of guarantor type frame (10) distributes floor (11), the top fixed mounting of floor (11) has sucking disc subassembly (12).
2. The conformal positioning tool for a composite material wing panel according to claim 1, wherein: the fixing frame (1) comprises a bottom plate (101), the middle of the upper end face of the bottom plate (101) is fixedly connected with upright columns (102) which are distributed at equal intervals, and the connecting rail (3) is fixed on one side of the upright columns (102) through bolts.
3. The conformal positioning tool for a composite material wing panel according to claim 1, wherein: an air pump and a controller are arranged in the control cabinet (2), and an operation panel is further arranged on one side of the control cabinet (2).
4. The conformal positioning tool for a composite material wing panel according to claim 1, wherein: the longitudinal adjusting mechanism (7) comprises a longitudinal guide rail (701), the inner wall of the longitudinal guide rail (701) is connected with a screw rod (702) in a rotating mode through a bearing, a second motor (703) is fixedly installed at the top of the longitudinal guide rail (701), an output shaft of the second motor (703) penetrates through the longitudinal guide rail (701) and is fixedly connected with the screw rod (702), a threaded sliding block (704) located inside the longitudinal guide rail (701) is connected to the surface of the screw rod (702) in a threaded mode, the threaded sliding block (704) is connected to the surface of the screw rod (702), and the rotary cylinder (8) is fixedly installed on one side of the threaded sliding block (.
5. The conformal positioning tool for a composite material wing panel according to claim 1, wherein: one side fixedly connected with U type fastener (14) of guarantor type frame (10), one side fixedly connected with retaining member (15) of U type fastener (14), U type fastener (14) are blocked in the inside of fixed frame (9) through retaining member (15), and the inner wall of U type fastener (14) is provided with and increases and hinder the cushion.
6. The conformal positioning tool for a composite material wing panel according to claim 5, wherein: retaining member (15) are including fixing thread bush (1501) in U type fastener (14) one side, the inner wall threaded connection of thread bush (1501) has screw rod (1502), the one end fixedly connected with driving lever (1503) of screw rod (1502), the other end of screw rod (1502) run through U type fastener (14) and with the opposite side threaded connection of U type fastener (14).
7. The conformal positioning tool for a composite material wing panel according to claim 1, wherein: the sucker assembly (12) comprises an electric push rod (1201), one end of the electric push rod (1201) is fixedly connected with a high-strength sucker (1202), and an air suction pipe joint (1203) is arranged on the back face of the high-strength sucker (1202).
8. The conformal positioning tool for a composite material wing panel according to claim 1, wherein: the air suction pipe joint (1203) is connected with an air pump through a hose.
9. The conformal positioning tool for a composite material wing panel according to claim 1, wherein: the top of U type frame (5) is provided with roll distancer (16), roll distancer (16) and one of them be located the top gyro wheel (6) are connected.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202010955367.4A CN112192464A (en) | 2020-09-11 | 2020-09-11 | Shape-preserving positioning tool for composite material wing wallboard |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202010955367.4A CN112192464A (en) | 2020-09-11 | 2020-09-11 | Shape-preserving positioning tool for composite material wing wallboard |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN112192464A true CN112192464A (en) | 2021-01-08 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202010955367.4A Pending CN112192464A (en) | 2020-09-11 | 2020-09-11 | Shape-preserving positioning tool for composite material wing wallboard |
Country Status (1)
| Country | Link |
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| CN (1) | CN112192464A (en) |
Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6029352A (en) * | 1997-09-25 | 2000-02-29 | The Boeing Company | Wing panel assembly |
| CN102306207A (en) * | 2011-06-16 | 2012-01-04 | 西北工业大学 | Method for assembling and positioning vertical column array type fuselage wall panel and device thereof |
| CN102941545A (en) * | 2012-11-07 | 2013-02-27 | 北京航空航天大学 | Flexible tool for assembling row-line chuck type wall board |
| CN103121194A (en) * | 2013-01-15 | 2013-05-29 | 西北工业大学 | Positioning fixture for splicing large wing wallboard and positioning method |
| CN103231534A (en) * | 2013-05-14 | 2013-08-07 | 桂林橡胶机械厂 | First-stage and secondary-stage transfer device positioning system of tire molding machine |
| CN203937867U (en) * | 2014-07-10 | 2014-11-12 | 中国航空工业集团公司北京航空制造工程研究所 | A kind of accuracy controlling device of adjusting for wing wallboard attitude |
| CN107719692A (en) * | 2017-08-28 | 2018-02-23 | 浙江大学 | A kind of conformal compression tooling of wing wallboard |
| CN208214720U (en) * | 2018-04-25 | 2018-12-11 | 西安飞机工业（集团）有限责任公司 | A kind of ultra-large type answers the automatic mounting tool of material siding |
-
2020
- 2020-09-11 CN CN202010955367.4A patent/CN112192464A/en active Pending
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6029352A (en) * | 1997-09-25 | 2000-02-29 | The Boeing Company | Wing panel assembly |
| CN102306207A (en) * | 2011-06-16 | 2012-01-04 | 西北工业大学 | Method for assembling and positioning vertical column array type fuselage wall panel and device thereof |
| CN102941545A (en) * | 2012-11-07 | 2013-02-27 | 北京航空航天大学 | Flexible tool for assembling row-line chuck type wall board |
| CN103121194A (en) * | 2013-01-15 | 2013-05-29 | 西北工业大学 | Positioning fixture for splicing large wing wallboard and positioning method |
| CN103231534A (en) * | 2013-05-14 | 2013-08-07 | 桂林橡胶机械厂 | First-stage and secondary-stage transfer device positioning system of tire molding machine |
| CN203937867U (en) * | 2014-07-10 | 2014-11-12 | 中国航空工业集团公司北京航空制造工程研究所 | A kind of accuracy controlling device of adjusting for wing wallboard attitude |
| CN107719692A (en) * | 2017-08-28 | 2018-02-23 | 浙江大学 | A kind of conformal compression tooling of wing wallboard |
| CN208214720U (en) * | 2018-04-25 | 2018-12-11 | 西安飞机工业（集团）有限责任公司 | A kind of ultra-large type answers the automatic mounting tool of material siding |
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