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CN107855714B - Aviation plug welding compaction device - Google Patents

Aviation plug welding compaction device Download PDF

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Publication number
CN107855714B
CN107855714B CN201711303515.9A CN201711303515A CN107855714B CN 107855714 B CN107855714 B CN 107855714B CN 201711303515 A CN201711303515 A CN 201711303515A CN 107855714 B CN107855714 B CN 107855714B
Authority
CN
China
Prior art keywords
swash plate
avigation
plate
dead lever
shaped
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
CN201711303515.9A
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Chinese (zh)
Other versions
CN107855714A (en
Inventor
杨立军
王博
邢超
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Shandong Feiyue Electronics Technology Co ltd
Original Assignee
Shandong Feiyue Electronics Technology Co ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
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Publication date
Application filed by Shandong Feiyue Electronics Technology Co ltd filed Critical Shandong Feiyue Electronics Technology Co ltd
Priority to CN201711303515.9A priority Critical patent/CN107855714B/en
Publication of CN107855714A publication Critical patent/CN107855714A/en
Application granted granted Critical
Publication of CN107855714B publication Critical patent/CN107855714B/en
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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K37/00Auxiliary devices or processes, not specially adapted to a procedure covered by only one of the preceding main groups
    • B23K37/04Auxiliary devices or processes, not specially adapted to a procedure covered by only one of the preceding main groups for holding or positioning work
    • B23K37/0426Fixtures for other work
    • B23K37/0435Clamps
    • B23K37/0443Jigs

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  • Physics & Mathematics (AREA)
  • Optics & Photonics (AREA)
  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Butt Welding And Welding Of Specific Article (AREA)
  • On-Site Construction Work That Accompanies The Preparation And Application Of Concrete (AREA)

Abstract

An aeronautical insert welding compaction device comprising: the bottom plate, vertical setting up riser on the bottom plate, slope set up in the swash plate of riser upper end, the level sets up the U-shaped fluting on the swash plate, the level sets up in the dead lever at swash plate rear and the dead lever sliding mechanism of drive dead lever relative swash plate upper and lower gliding, U-shaped grooved width is greater than the external diameter of aviation plug, aviation plug inserts in the U-shaped grooved, and its lower extreme contacts with U-shaped grooved bottom, and its upper end contacts with the lower terminal surface of dead lever. Through inserting the avigation in the U-shaped fluting and utilizing the dead lever to compress tightly fixedly with the avigation to realized compressing tightly of avigation, owing to the avigation is fixed on the swash plate, the swash plate is the slope setting relative bed plate, consequently can make things convenient for operating personnel to the avigation in the U-shaped fluting on the swash plate to insert the welding operation that moves, improved welding efficiency, need not manual handheld avigation and insert the welding operation that moves, saved the manpower, ensure operation safety.

Description

Aviation plug welding compaction device
Technical Field
The invention relates to the field of welding tools, in particular to an aviation plug welding compacting device.
Background
At present, the welding navigation plug is completely welded manually, the navigation plug is placed on a workbench, and the navigation plug is held by hand for welding. This is a serious effort and time consuming process.
Disclosure of Invention
In order to overcome the defects of the technology, the invention provides the aviation plug welding compacting device for effectively fixing the aviation plug and improving the welding efficiency.
The technical scheme adopted for overcoming the technical problems is as follows:
an aeronautical insert welding compaction device comprising: the bottom plate, vertical setting up riser on the bottom plate, slope set up in the swash plate of riser upper end, the level sets up the U-shaped fluting on the swash plate, the level sets up in the dead lever at swash plate rear and the dead lever sliding mechanism of drive dead lever relative swash plate upper and lower gliding, U-shaped grooved width is greater than the external diameter of aviation plug, aviation plug inserts in the U-shaped grooved, and its lower extreme contacts with U-shaped grooved bottom, and its upper end contacts with the lower terminal surface of dead lever.
Further, the fixed rod sliding mechanism comprises N connecting rods vertically arranged on the fixed rod and N longitudinal sliding grooves vertically arranged on the inclined plate and corresponding to the connecting rods, N is a natural number greater than or equal to 2, and the hand-screwed bolts penetrate through the longitudinal sliding grooves and then are screwed on the connecting rods.
In order to fix the fixing rod when not in use, the device also comprises a transverse chute which is horizontally arranged at the upper end of the chute and is connected with the chute.
The beneficial effects of the invention are as follows: through inserting the avigation in the U-shaped fluting and utilizing the dead lever to compress tightly fixedly with the avigation to realized compressing tightly of avigation, owing to the avigation is fixed on the swash plate, the swash plate is the slope setting relative bed plate, consequently can make things convenient for operating personnel to the avigation in the U-shaped fluting on the swash plate to insert the welding operation that moves, improved welding efficiency, need not manual handheld avigation and insert the welding operation that moves, saved the manpower, ensure operation safety.
Drawings
FIG. 1 is a schematic diagram I of a three-dimensional structure of the invention;
FIG. 2 is a schematic perspective view II of the present invention;
in the figure, 1, a base plate 2, a vertical plate 3, a sloping plate 4.U-shaped groove 5, a fixed rod 6, an aviation plug 7, a hand-screwed bolt 8, a longitudinal chute 9, a transverse chute 10 and a connecting rod.
Detailed Description
The invention is further described with reference to fig. 1 and 2.
An aeronautical insert welding compaction device comprising: the base plate 1, vertical setting up riser 2 on the base plate 1, the slope sets up in the swash plate 3 of riser 2 upper end, the level sets up U-shaped fluting 4 on swash plate 3, the level sets up in dead lever 5 at swash plate 3 rear and the relative swash plate 3 gliding dead lever sliding mechanism from top to bottom of drive dead lever 5, the width of U-shaped fluting 4 is greater than the external diameter of aviation plug 6, aviation plug 6 inserts in the U-shaped fluting 4, its lower extreme contacts with the bottom of U-shaped fluting 4, its upper end contacts with the lower terminal surface of dead lever 5. Through inserting the avionics 6 into the U-shaped slot 4 and utilizing the dead lever 5 to compress tightly fixedly the avionics 6 to realized compressing tightly of avionics 6, because the avionics 6 is fixed on the swash plate 3, the swash plate 3 is the slope setting relative to the bed plate 1, consequently can make things convenient for operating personnel to carry out welding operation to the avionics 6 in the U-shaped slot 4 on the swash plate 3, improved welding efficiency, need not manual handheld avionics 6 and carry out welding operation, saved the manpower, ensure operation safety.
The fixed rod sliding mechanism may be a structure including N connecting rods 10 vertically arranged on the fixed rod 5 and N longitudinal sliding grooves 8 vertically arranged on the inclined plate 3 and corresponding to the connecting rods 10, N is a natural number greater than or equal to 2, and the hand-screwed bolts 7 pass through the longitudinal sliding grooves 8 and are screwed on the connecting rods 10. The hand-screwed bolt 7 can slide up and down in the longitudinal sliding groove 8 after being loosened, so that the purpose of up-down adjustment of the fixing rod 5 is achieved, and when the fixing rod 5 is adjusted in place to tightly press the aviation plug 6 in the U-shaped groove 4, the hand-screwed bolt 7 is screwed, so that the fixing of the fixing rod 5 can be achieved, and the adjustment is convenient and simple.
Further, the horizontal sliding chute 9 is horizontally arranged at the upper end of the sliding chute 8 and is connected with the sliding chute 8. When not in use, the hand-screwed bolt 7 is upwards slid along the longitudinal sliding groove 8 after the hand-screwed bolt 7 is loosened, and then horizontally slides into the transverse sliding groove 9, so that the position of the fixing rod 5 is fixed after the fixing rod 5 ascends, the fixing rod cannot fall downwards, and the position of the fixing rod 5 is fixed.

Claims (1)

1. An aeronautical insert welding compaction device, comprising: the novel multifunctional navigation device comprises a base plate (1), a vertical plate (2) vertically arranged on the base plate (1), a sloping plate (3) obliquely arranged at the upper end of the vertical plate (2), a U-shaped slot (4) horizontally arranged on the sloping plate (3), a fixing rod (5) horizontally arranged at the rear of the sloping plate (3) and a fixing rod sliding mechanism for driving the fixing rod (5) to slide up and down relative to the sloping plate (3), wherein the width of the U-shaped slot (4) is larger than the outer diameter of a navigation plug (6), the navigation plug (6) is inserted into the U-shaped slot (4), the lower end of the navigation plug (6) is contacted with the bottom of the U-shaped slot (4), and the upper end of the navigation plug is contacted with the lower end face of the fixing rod (5);
the fixed rod sliding mechanism comprises N connecting rods (10) vertically arranged on the fixed rod (5) and N longitudinal sliding grooves (8) vertically arranged on the inclined plate (3) and corresponding to the connecting rods (10), N is a natural number greater than or equal to 2, and a hand-screwed bolt (7) passes through the longitudinal sliding grooves (8) and then is screwed on the connecting rods (10);
the horizontal sliding chute (9) is horizontally arranged at the upper end of the longitudinal sliding chute (8) and is connected with the longitudinal sliding chute (8).
CN201711303515.9A 2017-12-11 2017-12-11 Aviation plug welding compaction device Active CN107855714B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201711303515.9A CN107855714B (en) 2017-12-11 2017-12-11 Aviation plug welding compaction device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201711303515.9A CN107855714B (en) 2017-12-11 2017-12-11 Aviation plug welding compaction device

Publications (2)

Publication Number Publication Date
CN107855714A CN107855714A (en) 2018-03-30
CN107855714B true CN107855714B (en) 2023-12-05

Family

ID=61705363

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201711303515.9A Active CN107855714B (en) 2017-12-11 2017-12-11 Aviation plug welding compaction device

Country Status (1)

Country Link
CN (1) CN107855714B (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108838599A (en) * 2018-05-30 2018-11-20 苏州智能制造研究院有限公司 A kind of aviation plug welding clamping device

Citations (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB206342A (en) * 1922-10-20 1923-11-08 Patrick John Breen A new or improved device for compressing tobacco and the like
CN201872027U (en) * 2010-06-19 2011-06-22 武汉基准汽车模具有限公司 End face grinding clamp for round rod
CN202050118U (en) * 2011-05-10 2011-11-23 山东超越数控电子有限公司 Novel waterproof aviation plug
KR20130120270A (en) * 2012-04-25 2013-11-04 이상학 Jig for a welding test piece
CN203779027U (en) * 2014-03-13 2014-08-20 江门市南洋船舶工程有限公司 Adjustable fixed shape-maintaining device for assembling combined profiles
CN104476278A (en) * 2014-12-10 2015-04-01 成都市翻鑫家科技有限公司 Sliding-type multi-workpiece clamping and drilling equipment
KR20150061069A (en) * 2013-11-25 2015-06-04 (주)에이딕 Rail detaching mounting apparatus for pipeorbital welding carriage
KR20150083249A (en) * 2014-01-09 2015-07-17 임선우 apparatus of slope batter board
CN104785998A (en) * 2014-11-18 2015-07-22 平高集团有限公司 Barrel locating frame and welding tool comprising same
KR101597284B1 (en) * 2014-11-19 2016-02-24 강림중공업 주식회사 A Rotary Welding Device
CN205464961U (en) * 2016-01-29 2016-08-17 厦门精鸿鑫精密五金工业有限公司 Weld special tool
CN206632946U (en) * 2017-03-29 2017-11-14 刘华 A kind of accounting voucher bookbinding auxiliary pallet
CN207695927U (en) * 2017-12-11 2018-08-07 济南飞越机电科技有限公司 A kind of air plug welding pressing device

Patent Citations (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB206342A (en) * 1922-10-20 1923-11-08 Patrick John Breen A new or improved device for compressing tobacco and the like
CN201872027U (en) * 2010-06-19 2011-06-22 武汉基准汽车模具有限公司 End face grinding clamp for round rod
CN202050118U (en) * 2011-05-10 2011-11-23 山东超越数控电子有限公司 Novel waterproof aviation plug
KR20130120270A (en) * 2012-04-25 2013-11-04 이상학 Jig for a welding test piece
KR20150061069A (en) * 2013-11-25 2015-06-04 (주)에이딕 Rail detaching mounting apparatus for pipeorbital welding carriage
KR20150083249A (en) * 2014-01-09 2015-07-17 임선우 apparatus of slope batter board
CN203779027U (en) * 2014-03-13 2014-08-20 江门市南洋船舶工程有限公司 Adjustable fixed shape-maintaining device for assembling combined profiles
CN104785998A (en) * 2014-11-18 2015-07-22 平高集团有限公司 Barrel locating frame and welding tool comprising same
KR101597284B1 (en) * 2014-11-19 2016-02-24 강림중공업 주식회사 A Rotary Welding Device
CN104476278A (en) * 2014-12-10 2015-04-01 成都市翻鑫家科技有限公司 Sliding-type multi-workpiece clamping and drilling equipment
CN205464961U (en) * 2016-01-29 2016-08-17 厦门精鸿鑫精密五金工业有限公司 Weld special tool
CN206632946U (en) * 2017-03-29 2017-11-14 刘华 A kind of accounting voucher bookbinding auxiliary pallet
CN207695927U (en) * 2017-12-11 2018-08-07 济南飞越机电科技有限公司 A kind of air plug welding pressing device

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Address after: Room B203 and B208, Standard Factory Building D for Instrument and Equipment Assembly in ICT Industrial Park, No. 26 Road, High tech Zone, Jinan City, Shandong Province, 250000

Applicant after: SHANDONG FEIYUE ELECTRONICS TECHNOLOGY Co.,Ltd.

Address before: 250101 Ji'nan four, A402 room, 4 building, Qilu Software Park, 1 Shun Hua Road, hi tech Zone, Ji'nan, Shandong.

Applicant before: JINAN FEIYUE ELECTROMECHANICAL TECHNOLOGY Co.,Ltd.

CB02 Change of applicant information
GR01 Patent grant
GR01 Patent grant
PE01 Entry into force of the registration of the contract for pledge of patent right

Denomination of invention: An aviation plug welding compression device

Granted publication date: 20231205

Pledgee: Jinan area branch of Shandong free trade zone of Qilu Bank Co.,Ltd.

Pledgor: SHANDONG FEIYUE ELECTRONICS TECHNOLOGY Co.,Ltd.

Registration number: Y2024980038772

PE01 Entry into force of the registration of the contract for pledge of patent right