CN208602641U - A kind of rudder blade adjustment auxiliary mould - Google Patents

A kind of rudder blade adjustment auxiliary mould Download PDF

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Publication number
CN208602641U
CN208602641U CN201820860011.0U CN201820860011U CN208602641U CN 208602641 U CN208602641 U CN 208602641U CN 201820860011 U CN201820860011 U CN 201820860011U CN 208602641 U CN208602641 U CN 208602641U
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CN
China
Prior art keywords
rudder blade
inner plating
lamina rara
rara externa
circular
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
CN201820860011.0U
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Chinese (zh)
Inventor
王维元
陈涛
阮庆海
王振兴
李昕南
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.)
China Shipbuilding Dalian Shipyard Industry Development Co.,Ltd.
Original Assignee
Steel Structure Manufacturing Co Ltd Of Dalian Shipbuilding Industry 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.)
Filing date
Publication date
Application filed by Steel Structure Manufacturing Co Ltd Of Dalian Shipbuilding Industry Co Ltd filed Critical Steel Structure Manufacturing Co Ltd Of Dalian Shipbuilding Industry Co Ltd
Priority to CN201820860011.0U priority Critical patent/CN208602641U/en
Application granted granted Critical
Publication of CN208602641U publication Critical patent/CN208602641U/en
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Abstract

A kind of rudder blade adjustment auxiliary mould, there are rudder blade, inner plating, lamina rara externa, the outer surface of inner plating is connected with the inner surface of lamina rara externa, inner plating and outer layer board ends are upturned to form the arc panel of opening, the opening of inner plating is " V " type, the inner surface of inner plating is pasted with rubber pad, and the both ends of inner plating are additionally provided with rubber block.One end of inner plating is equipped with a circular protrusions, a circular hole is provided at the center of the round protrusion, wing bolt passes through the circular hole of the protrusion, the utility model on rudder blade without welding pull ring, rudder blade surface paint will not be destroyed, work is handled without subsequent cutting, polishing, touch-up paint after rudder blade installation, and this tooling can Reusability, this tooling is not in the case where destroying rudder blade surface paint, can still rudder blade be assisted to be installed, it improves work efficiency, reduces job costs, it is economic and environment-friendly.

Description

A kind of rudder blade adjustment auxiliary mould
Technical field
The present invention relates to shipping rudder blade fields, and in particular to a kind of auxiliary mould that auxiliary ship station rudder blade is installed.
Background technique
In shipbuilding industry, when closing up the stage and installing to rudder blade, the mode of construction directly affects product quality and applies Work efficiency rate, goes wrong, and will lead to product and reprocesses, or even scrap, construction cost is significantly increased.
Existing construction method is the welding hanging ring on rudder blade, since japanning is completed in rudder blade, will cause rudder blade paint Destruction so that the later period carry out cutting polishing and touch-up paint processing, existing form of construction work assembly time is longer, construction efficiency It is low, lead to that the production cost increases.
Summary of the invention
The unresolved above problem, the present invention provide a kind of rudder blade adjustment auxiliary mould, it is intended to reach and keep rudder blade surface oil Paint is complete, works after rudder blade installation without any subsequent processing, improves the purpose of working efficiency, used technical solution It is:
A kind of rudder blade adjusts auxiliary mould, there is an inner plating and lamina rara externa, the inner plating and the lamina rara externa be both ends to Upper tilting forms the arc panel of opening, and the inner surface welded connecting of the outer surface of the inner plating and the lamina rara externa is described interior The opening of laminate is " V " type, and the both ends of the inner plating are further fixed on rubber block, and described lamina rara externa one end is in circular arc type, another End is in wedge angle type, is provided with a circular through hole in one end of the lamina rara externa circular arc type, latches across the circular through hole.
The inner surface of the inner plating is pasted with one layer of rubber pad, and the rubber pad is in contact with the rudder blade, described interior One end of laminate is equipped with a circular protrusions, is provided with a circular hole at the center of the circular protrusions, wing bolt passes through described The circular hole of protrusion, the circular hole of the protrusion is interior to be equipped with the screw thread matched with the wing bolt.
A kind of above-mentioned rudder blade adjusts auxiliary mould, it is preferable that the protrusion is arranged on the side wall of the inner plating.
A kind of above-mentioned rudder blade adjusts auxiliary mould, it is preferable that the protrusion is arranged in the inner plating and the lamina rara externa One end that arc end is connected.
A kind of above-mentioned rudder blade adjusts auxiliary mould, it is preferable that the left and right both ends of lamina rara externa are symmetrically arranged with a strip Opening.
This tooling is inserted in the side of rudder blade, the rubber pad of inner plating inner surface is in contact with rudder blade, wing bolt is tightened, Wing bolt has a pressure to rudder blade, also, while tighten wing bolt, and inner plating and lamina rara externa have certain bullet Property, inner plating and lamina rara externa can be received inwardly under the action of wing bolt, and then clamp rudder blade, keep rudder blade tighter with inner plating Close fitting, and then stronger fix rudder blade.The rubber block of rubber pad and internal layer board ends that inner plating inner surface is pasted, It prevents tooling in use, scratches rudder blade surface paint.
It is provided with a fixed block on the ground, fixed block a part is embedded in underground, and a part exposes earth's surface, exposes earth's surface There is a circular hole in part, and wirerope sequentially passes through circular hole and lamina rara externa one end with lock, made by strainer tense wire rope Rudder blade is rotated.
Using this tooling, without welding pull ring on rudder blade, rudder blade surface paint will not be destroyed, without subsequent after rudder blade installation Cutting, polishing, touch-up paint handle work, and this tooling can Reusability, this tooling do not destroying rudder blade surface paint the case where Under, can still rudder blade be assisted to be installed, improved work efficiency, reduce job costs, it is economic and environment-friendly.
Detailed description of the invention
Fig. 1 is structural schematic diagram of the invention;
Fig. 2 is side structure schematic view of the invention;
Fig. 3 is the structural schematic diagram in use process of the present invention;
Wherein: lamina rara externa 1, rubber pad 3, wing bolt 4, circular through hole 5, rubber block 6, strainer 7, is fixed inner plating 2 Block 8, rudder blade 9, lock 10, protrusion 11.
Specific embodiment
In conjunction with attached drawing, the present invention will be further described, as shown in Figure 1-3, a kind of rudder blade adjusts auxiliary mould, there is arc Lamina rara externa 1 and arc inner plating 2, the inner surface of lamina rara externa 1 and the outer surface of inner plating 2 are welded to connect, lamina rara externa 1 and inner plating 2 both ends are upturned to form an opening, and the opening of formation is " V " type.One end of lamina rara externa 1 be circular arc type, lamina rara externa 1 it is another One end is wedge angle type, and 1 circular arc type one end of lamina rara externa is equipped with a circular through hole 5, and lock 10 passes through circular through hole 5.
The inner surface of inner plating 2 is pasted with one layer of rubber pad 3, and the both ends of inner plating 2 are equipped with rubber block 6, in inner plating 2 There are a circular protrusions 11 on side wall, raised 11 centers are equipped with opening, and wing bolt 4 passes through opening.By tooling sleeve in rudder blade 9 one The rubber pad 3 of side, inner plating 2 is in contact with rudder blade 9, tightens wing bolt 4, and tooling clamps rudder blade 9.
Application method of the invention is: by tooling sleeve in 9 side of rudder blade that needs adjust, tightening wing bolt 4, makes tooling It is fixedly connected with rudder blade 9, the fixed block 8 and lock 10 of ground is sequentially passed through with wirerope, is tensed by strainer 7 and drives rudder blade 9 rotations, adjust 9 angle position of rudder blade.
The present invention can Reusability, will not destroy rudder blade surface paint, rudder blade installation after without it is subsequent cutting, polishing, touch-up paint Work is handled, improves work efficiency, reduces job costs, it is economic and environment-friendly.
The foregoing is only a preferred embodiment of the present invention, but scope of protection of the present invention is not limited thereto, Anyone skilled in the art within the technical scope of the present disclosure, according to the technique and scheme of the present invention and its Inventive concept is subject to equivalent substitution or change, should be covered by the scope of protection of the present invention.

Claims (4)

1. a kind of rudder blade adjusts auxiliary mould, there is rudder blade, it is characterised in that: have inner plating (2) and lamina rara externa (1), the internal layer Plate (2) and the lamina rara externa (1) are that both ends are upturned to form the arc panel of opening, the outer surface of the inner plating (2) and institute The inner surface for stating lamina rara externa (1) is welded to connect, and the opening of the inner plating (2) is " V " type, and the both ends of the inner plating (2) are also It is fixed with rubber block (6), described lamina rara externa (1) one end is in circular arc type, and the other end is in wedge angle type, in the lamina rara externa circular arc type One end is provided with a circular through hole (5), and lock (10) passes through the circular through hole (5);
The inner surface of the inner plating (2) is pasted with one layer of rubber pad (3), and the rubber pad (3) connects with the rudder blade (9) One end of touching, the inner plating (2) is equipped with a circular protrusions (11), is provided with a circle at the center of round raised (11) Hole, wing bolt (4) pass through the circular hole of the protrusion, are equipped in the circular hole of the protrusion and match with the wing bolt (4) Screw thread.
2. a kind of rudder blade as described in claim 1 adjusts auxiliary mould, it is characterised in that: the protrusion (11) is arranged described On the side wall of inner plating.
3. a kind of rudder blade as claimed in claim 1 or 2 adjusts auxiliary mould, it is characterised in that: protrusion (11) setting exists One end that the inner plating (2) is connected with the lamina rara externa (1) arc end.
4. a kind of rudder blade as described in claim 1 adjusts auxiliary mould, it is characterised in that: the left and right both ends pair of lamina rara externa Title is provided with strip opening.
CN201820860011.0U 2018-06-05 2018-06-05 A kind of rudder blade adjustment auxiliary mould Active CN208602641U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201820860011.0U CN208602641U (en) 2018-06-05 2018-06-05 A kind of rudder blade adjustment auxiliary mould

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201820860011.0U CN208602641U (en) 2018-06-05 2018-06-05 A kind of rudder blade adjustment auxiliary mould

Publications (1)

Publication Number Publication Date
CN208602641U true CN208602641U (en) 2019-03-15

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Application Number Title Priority Date Filing Date
CN201820860011.0U Active CN208602641U (en) 2018-06-05 2018-06-05 A kind of rudder blade adjustment auxiliary mould

Country Status (1)

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CN (1) CN208602641U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112278222A (en) * 2020-10-29 2021-01-29 广船国际有限公司 Ship rudder blade and swing test method thereof

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112278222A (en) * 2020-10-29 2021-01-29 广船国际有限公司 Ship rudder blade and swing test method thereof

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GR01 Patent grant
GR01 Patent grant
CP03 Change of name, title or address

Address after: 116411 Wulu town Wulu village, Zhuanghe City, Dalian City, Liaoning Province

Patentee after: China Shipbuilding Dalian Shipyard Industry Development Co.,Ltd.

Address before: 116000 Wulu town Wulu village, Zhuanghe City, Dalian City, Liaoning Province

Patentee before: DALIAN SHIPBUILDING INDUSTRY STEEL STRUCTURE MANUFACTURING Co.,Ltd.

CP03 Change of name, title or address