CN104400687A - Triaxial movement adjustable V-shaped bracket for butt joint of cabin sections - Google Patents

Triaxial movement adjustable V-shaped bracket for butt joint of cabin sections Download PDF

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Publication number
CN104400687A
CN104400687A CN201410617666.1A CN201410617666A CN104400687A CN 104400687 A CN104400687 A CN 104400687A CN 201410617666 A CN201410617666 A CN 201410617666A CN 104400687 A CN104400687 A CN 104400687A
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CN
China
Prior art keywords
bracket
line slideway
cabin section
arrangement bracket
docking
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Granted
Application number
CN201410617666.1A
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Chinese (zh)
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CN104400687B (en
Inventor
王相理
于世超
王忠野
张晶
刘明
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Harbin Fenghua Co ltd China Aerospace Science & Industry Corp
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Harbin Fenghua Co ltd China Aerospace Science & Industry Corp
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Publication of CN104400687A publication Critical patent/CN104400687A/en
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B25HAND TOOLS; PORTABLE POWER-DRIVEN TOOLS; MANIPULATORS
    • B25BTOOLS OR BENCH DEVICES NOT OTHERWISE PROVIDED FOR, FOR FASTENING, CONNECTING, DISENGAGING OR HOLDING
    • B25B11/00Work holders not covered by any preceding group in the subclass, e.g. magnetic work holders, vacuum work holders

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Body Structure For Vehicles (AREA)

Abstract

The invention relates to a triaxial movement adjustable V-shaped bracket for the butt joint of cabin sections, belonging to the technical field of an auxiliary device for the butt joint of the cabin sections, and aiming at solving the problems that the horizontal butt joint installation of the existing large circular barrels is completed by applying special installation devices which are respectively designed according to the requirements of the sizes of the barrels and the assembly accuracy, and the special installation devices are complicated in structure, high in cost and long in manufacturing cycle. According to the triaxial movement adjustable V-shaped bracket, a lower linear guide rail is arranged in a lower support seat and is arranged along the length direction of the lower support seat; an upper support seat is matched with the lower linear guide rail and can move left and right on the lower linear guide rail; the upper support seat is internally provided with an upper linear guide rail, and the upper linear guide rail is arranged along the width direction of the upper support seat; a transverse beam mechanism is matched with the upper linear guide rail and can move front and back on the upper linear guide rail; a V-shaped bracket is arranged on the transverse beam mechanism in a locating way by a vertical guide mechanism; a screw rod is in a vertical and threaded connection with the transverse beam mechanism, and the upper end of the screw rod leans against the bottom surface of the V-shaped bracket; the bottom of a V-shaped groove of the V-shaped bracket is a plane. The triaxial movement adjustable V-shaped bracket for butt joint of cabin sections is used for horizontal butt joint assembly of I level and II level of large boosting cabin sections.

Description

Three axles for the docking of cabin section move adjustable V-arrangement bracket
Technical field
The present invention relates to a kind of large-scale boost module section I, the nonstandard process unit of the horizontal Butt Assembling of II level, particularly relate to a kind of three axles for the docking of cabin section and move adjustable V-arrangement bracket; Belong to cabin section butt joint auxiliary device technical field.
Background technology
Cabin is many to be formed by the horizontal Butt Assembling of I, II level large-scale cabin section, in assembling process, needs each cabin section horizontal positioned, and will ensure that coaxial line docks.The horizontal abutting joint of this type of large-scale circular cylinder body domestic is all the requirement designed, designed special installation apparatus separately according to cylindrical shell size and assembly precision, and Electronic control cylindrical shell rolls and rotates, but its complex structure, cost is high, and the manufacturing cycle is long.In order to avoid these unfavorable factors, urgently design the precise positioning supporting and adjusting device of the horizontal Butt Assembling of a kind of I, II level large-scale cabin section, ensure that its structure is simple, adjustment is flexible, axial location is accurate, manufacturing cycle is short, and cost is low, ensures the personnel of erecting yard and the safety of cabin section simultaneously.
Summary of the invention
The present invention in order to the horizontal abutting joint solving existing large-scale circular cylinder body be all the requirement designed, designed special installation apparatus separately according to cylindrical shell size and assembly precision, Electronic control cylindrical shell rolls and rotates, its complex structure, cost is high, the problem that manufacturing cycle is long, and then provide a kind of three axles for the docking of cabin section to move adjustable V-arrangement bracket.
The present invention in order to solve the problems of the technologies described above taked technical scheme is:
Three axles for the docking of cabin section of the present invention move adjustable V-arrangement bracket, comprise undersetting, upper bracket, upper line slideway, beam mechanism, vertical guiding mechanism, V-arrangement bracket, lower line slideway and leading screw screw rod, lower line slideway is provided with in described undersetting, lower line slideway is arranged along the length direction of undersetting, upper bracket coordinates with lower line slideway and can move left and right on lower line slideway, line slideway is provided with in described upper bracket, upper line slideway is arranged along the width of upper bracket, beam mechanism coordinates with upper line slideway and can move forward and backward on upper line slideway, V-arrangement bracket by vertical guiding mechanism location and installation on beam mechanism, leading screw screw rod is vertically threaded on beam mechanism, and the upper end of leading screw screw rod is resisted against on the bottom surface of V-arrangement bracket, moving up and down of V-arrangement bracket is realized by adjusting screw screw rod.
Preferred: described three axles for the docking of cabin section move adjustable V-arrangement bracket and also comprise the first adjustment Limit screw, the front and back sides of beam mechanism are provided with the first adjustment Limit screw, the first adjustment Limit screw is threaded with upper bracket.Setting like this, is convenient to the front and back adjustment realizing V-arrangement bracket.
Preferred: described three axles for the docking of cabin section move adjustable V-arrangement bracket and also comprise the second adjustment Limit screw, the left and right side of upper bracket are provided with the second adjustment Limit screw, the second adjustment Limit screw is threaded with undersetting.Setting like this, is convenient to the left and right adjustment realizing V-arrangement bracket.
Preferred: described beam mechanism comprises entablature and sill, vertical guiding mechanism comprises guide pin bushing and guide pillar, entablature is fixedly connected with by guide pin bushing with sill, sill coordinates with upper line slideway and can move forward and backward on upper line slideway, first adjustment Limit screw is arranged on the front and back sides of sill, the lower end of guide pillar coordinates with guide pin bushing, and the upper end of guide pillar is fixed on V-arrangement bracket, and leading screw screw rod is vertically threaded on entablature.Setting like this, structure is simple, is convenient to assembling, is convenient to adjustment.
Preferred: described three axles for the docking of cabin section move adjustable V-arrangement bracket and also comprise rotating roller, and the V-shaped groove sidewall of described V-arrangement bracket is provided with rotating roller.Setting like this, cabin section can be rolled under external force on bearing, completes angle location.
Preferred: to be plane at the bottom of the V-shaped groove of described V-arrangement bracket.
the present invention compared with prior art has following effect:
Bottom of the present invention utilizes three layers of secondary orthogonal line slideway of pedestal therebetween two, realizes left and right and the adjustable moving of front and back respectively, and corresponding pedestal is realized passing by respective adjustment limiting component and spacing respectively; V-arrangement bracket is by vertical guiding mechanism location and installation at beam mechanism, and beam mechanism is provided with the guide pin bushing that can lead, and the guide pillar of V-arrangement bracket base can move up and down along guide pin bushing; Be provided with leading screw screw rod in the middle of the entablature of beam mechanism, V-arrangement bearing can be moved up and down; Roller is equipped with in V-arrangement bearing both sides, and cabin section can be rolled under external force on bearing, completes angle location.The precise positioning that present invention achieves the horizontal Butt Assembling of I, II level large-scale cabin section supports adjustment, and structure is simple, and adjustment is flexible, and axial location is accurate, and the manufacturing cycle is short, and cost is low, ensures the personnel of erecting yard and the safety of cabin section.
Accompanying drawing explanation
Fig. 1 is the three-dimensional structure diagram that three axles for the docking of cabin section of the present invention move adjustable V-arrangement bracket;
Fig. 2 is structure and the annexation figure of V-arrangement bracket, vertically guiding mechanism, beam mechanism;
Fig. 3 is the schematic diagram that cabin section is placed on V-arrangement adjustable bracket;
In figure: 1-undersetting; 2-upper bracket; 3-first adjusts Limit screw; The upper line slideway of 4-; 5-beam mechanism; The vertical guiding mechanism of 6-; 7-rotating roller; 8-V-arrangement bracket; Line slideway under 9-; 10-leading screw screw rod; 11-second adjusts Limit screw; 51-entablature; 52-sill; 61-guide pin bushing; 62-guide pillar.
Detailed description of the invention
Detailed description of the invention: in conjunction with the accompanying drawings, three axles for the docking of cabin section of present embodiment move adjustable V-arrangement bracket, comprise undersetting 1, upper bracket 2, upper line slideway 4, beam mechanism 5, vertical guiding mechanism 6, V-arrangement bracket 8, lower line slideway 9 and leading screw screw rod 10, lower line slideway 9 is provided with in described undersetting 1, lower line slideway 9 is arranged along the length direction of undersetting 1, upper bracket 2 coordinates with lower line slideway 9 and can move left and right on lower line slideway 9, line slideway 4 is provided with in described upper bracket 2, upper line slideway 4 is arranged along the width of upper bracket 2, beam mechanism 5 coordinates with upper line slideway 4 and can move forward and backward on upper line slideway 4, V-arrangement bracket 8 by vertical guiding mechanism 6 location and installation on beam mechanism 5, leading screw screw rod 10 is vertically threaded on beam mechanism 5, and the upper end of leading screw screw rod 10 is resisted against on the bottom surface of V-arrangement bracket 8, moving up and down of V-arrangement bracket 8 is realized by adjusting screw screw rod 10.
Further: described three axles for the docking of cabin section move adjustable V-arrangement bracket and also comprise the first adjustment Limit screw 3, the front and back sides of beam mechanism 5 is provided with the first adjustment Limit screw 3, first adjustment Limit screw 3 and is threaded with upper bracket 2.
Further: described three axles for the docking of cabin section move adjustable V-arrangement bracket and also comprise the second adjustment Limit screw 11, the left and right side of upper bracket 2 is provided with the second adjustment Limit screw 11, second adjustment Limit screw 11 and is threaded with undersetting.
Further: described beam mechanism comprises entablature 51 and sill 52, vertical guiding mechanism 6 comprises guide pin bushing 61 and guide pillar 62, entablature 51 is fixedly connected with by guide pin bushing 61 with sill 52, sill 52 coordinates with upper line slideway 4 and can move forward and backward on upper line slideway 4, first adjustment Limit screw 3 is arranged on the front and back sides of sill 52, the lower end of guide pillar 62 coordinates with guide pin bushing 61, and the upper end of guide pillar 62 is fixed on V-arrangement bracket 8, and leading screw screw rod 10 is vertically threaded on entablature 51.
Further: described three axles for the docking of cabin section move adjustable V-arrangement bracket and also comprise rotating roller 7, and the V-shaped groove sidewall of described V-arrangement bracket 8 is provided with rotating roller 7.
Further: to be plane at the bottom of the V-shaped groove of described V-arrangement bracket 8.
During application, two covers need be moved adjustable V-arrangement bracket for three axles that cabin section is docked and be placed on horizontal stand, put well and first undersetting 1, upper bracket 2 are adjusted to stroke centre position afterwards, respectively three axles that two sections of cabin section liftings are placed on for the docking of cabin section are moved adjustable V-arrangement bracket, can with one of them cabin section for benchmark, adjust the bracket of another cabin section, reach the condition that can assemble.Bracket can realize all around, move up and down, and can rotary rolling cabin section.By rotating the first adjustment Limit screw, to realize cabin section movable on guide rail, rotation second adjustment Limit screw realizes cabin section and moves left and right on guide rail, leading screw screw rod 10 in rotating beam mechanism 5 realizes cabin section and moves up and down along guide pillar guide pin bushing, the rotation of cabin section is circumferentially pushed up by external force or pulls realization, and such as a thousand pieces of gold top or row are hung.By above movement and adjustment of rolling, realize the center seam docking of two-stage large-scale cabin section, complete assembling.
The exemplary illustration of present embodiment just to this patent, does not limit its protection domain, and those skilled in the art can also change, as long as no the Spirit Essence exceeding this patent, in the protection domain of this patent its local.

Claims (5)

1. three axles for the docking of cabin section move adjustable V-arrangement bracket, it is characterized in that: comprise undersetting (1), upper bracket (2), upper line slideway (4), beam mechanism (5), vertical guiding mechanism (6), V-arrangement bracket (8), lower line slideway (9) and leading screw screw rod (10), lower line slideway (9) is provided with in described undersetting (1), lower line slideway (9) is arranged along the length direction of undersetting (1), upper bracket (2) coordinates with lower line slideway (9) and can move left and right on lower line slideway (9), line slideway (4) is provided with in described upper bracket (2), upper line slideway (4) is arranged along the width of upper bracket (2), beam mechanism (5) coordinates with upper line slideway (4) and can be upper movable at upper line slideway (4), V-arrangement bracket (8) by vertical guiding mechanism (6) location and installation on beam mechanism (5), leading screw screw rod (10) is vertically threaded on beam mechanism (5), and the upper end of leading screw screw rod (10) is resisted against on the bottom surface of V-arrangement bracket (8), moving up and down of V-arrangement bracket (8) is realized by adjusting screw screw rod (10), be plane at the bottom of the V-shaped groove of described V-arrangement bracket (8).
2. three axles for the docking of cabin section according to claim 1 move adjustable V-arrangement bracket, it is characterized in that: described three axles for the docking of cabin section move adjustable V-arrangement bracket and also comprise the first adjustment Limit screw (3), the front and back sides of beam mechanism (5) is provided with the first adjustment Limit screw (3), the first adjustment Limit screw (3) is threaded with upper bracket (2).
3. three axles for the docking of cabin section according to claim 1 and 2 move adjustable V-arrangement bracket, it is characterized in that: described three axles for the docking of cabin section move adjustable V-arrangement bracket and also comprise the second adjustment Limit screw (11), the left and right side of upper bracket (2) is provided with the second adjustment Limit screw (11), the second adjustment Limit screw (11) is threaded with undersetting.
4. three axles for the docking of cabin section according to claim 3 move adjustable V-arrangement bracket, it is characterized in that: described beam mechanism comprises entablature (51) and sill (52), vertical guiding mechanism (6) comprises guide pin bushing (61) and guide pillar (62), entablature (51) is fixedly connected with by guide pin bushing (61) with sill (52), sill (52) coordinates with upper line slideway (4) and can be upper movable at upper line slideway (4), first adjustment Limit screw (3) is arranged on the front and back sides of sill (52), the lower end of guide pillar (62) coordinates with guide pin bushing (61), the upper end of guide pillar (62) is fixed on V-arrangement bracket (8), leading screw screw rod (10) is vertically threaded on entablature (51).
5. three axles for the docking of cabin section according to claim 4 move adjustable V-arrangement bracket, it is characterized in that: described three axles for the docking of cabin section move adjustable V-arrangement bracket and also comprise rotating roller (7), and the V-shaped groove sidewall of described V-arrangement bracket (8) is provided with rotating roller (7).
CN201410617666.1A 2014-11-06 2014-11-06 Three axles for the docking of cabin section move adjustable V-arrangement bracket Active CN104400687B (en)

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Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106041513A (en) * 2016-06-29 2016-10-26 中国科学院沈阳自动化研究所 Multi-degree-of-freedom cabin position and posture adjustor
CN106239419A (en) * 2016-08-31 2016-12-21 玉柴船舶动力股份有限公司 A kind of low-speed diesel engine crosshad shoe assembling detection instrument
CN106759944A (en) * 2016-12-13 2017-05-31 浙江远成精工科技有限公司 A kind of improved durable anticorrosive accurate node component
CN107167632A (en) * 2016-03-08 2017-09-15 株式会社日立大厦*** Distribution presses fixture
CN108240783A (en) * 2016-12-23 2018-07-03 中国科学院沈阳自动化研究所 A kind of bay section docks adjustment mechanism
CN108297970A (en) * 2018-03-26 2018-07-20 沈阳航天新光集团有限公司 A kind of multi cabin combined type docking transfer car(buggy)
CN109894935A (en) * 2017-12-08 2019-06-18 辽宁法库陶瓷工程技术研究中心 A kind of overlength, high-accuracy Pyrex pipe outside diameter processing technology
CN109972522A (en) * 2019-03-07 2019-07-05 中交二航局第四工程有限公司 A kind of adjustable pile equipment method of gravity type
CN110949695A (en) * 2018-12-20 2020-04-03 中国船舶重工集团应急预警与救援装备股份有限公司 Booster and core-level rocket binding butt joint vertical direction adjusting system
CN111805493A (en) * 2020-07-10 2020-10-23 中冶宝钢技术服务有限公司 Electric furnace EBT adjusting and positioning auxiliary device and installation method thereof
CN112872788A (en) * 2021-03-11 2021-06-01 北京工业大学 Feeding mechanism of thin-wall cabin section butt-joint device

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FR2697460B1 (en) * 1992-11-05 1995-01-06 Norelem Modular V-shaped support with variable orientation.
CN201580565U (en) * 2010-01-22 2010-09-15 顾祝平 Platform vehicle for assembling and disassembling tail pipe nozzle of engine
CN102001451A (en) * 2010-11-12 2011-04-06 浙江大学 Airplane component attitude adjusting and butting system based on four numeric control positioners, attitude adjusting platform and mobile bracket and corresponding method
CN201834035U (en) * 2010-07-19 2011-05-18 凯迈(洛阳)测控有限公司 Trolley for testing gliding projectile tail capsule
CN102490281A (en) * 2011-11-29 2012-06-13 河海大学常州校区 Fixture used for silicon wafer butting machine
US20130113150A1 (en) * 2011-11-09 2013-05-09 Summer Manufacturing Co., Inc. Clamp assembly
CN104118576A (en) * 2014-08-07 2014-10-29 天津航天长征火箭制造有限公司 Integrated large-angle rolling and posture adjusting rack car

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2697460B1 (en) * 1992-11-05 1995-01-06 Norelem Modular V-shaped support with variable orientation.
CN201580565U (en) * 2010-01-22 2010-09-15 顾祝平 Platform vehicle for assembling and disassembling tail pipe nozzle of engine
CN201834035U (en) * 2010-07-19 2011-05-18 凯迈(洛阳)测控有限公司 Trolley for testing gliding projectile tail capsule
CN102001451A (en) * 2010-11-12 2011-04-06 浙江大学 Airplane component attitude adjusting and butting system based on four numeric control positioners, attitude adjusting platform and mobile bracket and corresponding method
US20130113150A1 (en) * 2011-11-09 2013-05-09 Summer Manufacturing Co., Inc. Clamp assembly
CN102490281A (en) * 2011-11-29 2012-06-13 河海大学常州校区 Fixture used for silicon wafer butting machine
CN104118576A (en) * 2014-08-07 2014-10-29 天津航天长征火箭制造有限公司 Integrated large-angle rolling and posture adjusting rack car

Cited By (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107167632B (en) * 2016-03-08 2020-10-27 株式会社日立大厦*** Wiring pressing clamp
CN107167632A (en) * 2016-03-08 2017-09-15 株式会社日立大厦*** Distribution presses fixture
CN106041513B (en) * 2016-06-29 2017-11-21 中国科学院沈阳自动化研究所 Multiple degrees of freedom bay section pose adjusting means
CN106041513A (en) * 2016-06-29 2016-10-26 中国科学院沈阳自动化研究所 Multi-degree-of-freedom cabin position and posture adjustor
CN106239419A (en) * 2016-08-31 2016-12-21 玉柴船舶动力股份有限公司 A kind of low-speed diesel engine crosshad shoe assembling detection instrument
CN106239419B (en) * 2016-08-31 2018-06-19 玉柴船舶动力股份有限公司 A kind of low-speed diesel engine crosshad shoe assembles detection instrument
CN106759944A (en) * 2016-12-13 2017-05-31 浙江远成精工科技有限公司 A kind of improved durable anticorrosive accurate node component
CN108240783A (en) * 2016-12-23 2018-07-03 中国科学院沈阳自动化研究所 A kind of bay section docks adjustment mechanism
CN109894935A (en) * 2017-12-08 2019-06-18 辽宁法库陶瓷工程技术研究中心 A kind of overlength, high-accuracy Pyrex pipe outside diameter processing technology
CN108297970A (en) * 2018-03-26 2018-07-20 沈阳航天新光集团有限公司 A kind of multi cabin combined type docking transfer car(buggy)
CN110949695A (en) * 2018-12-20 2020-04-03 中国船舶重工集团应急预警与救援装备股份有限公司 Booster and core-level rocket binding butt joint vertical direction adjusting system
CN109972522A (en) * 2019-03-07 2019-07-05 中交二航局第四工程有限公司 A kind of adjustable pile equipment method of gravity type
CN111805493A (en) * 2020-07-10 2020-10-23 中冶宝钢技术服务有限公司 Electric furnace EBT adjusting and positioning auxiliary device and installation method thereof
CN112872788A (en) * 2021-03-11 2021-06-01 北京工业大学 Feeding mechanism of thin-wall cabin section butt-joint device

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