CN102009322A - Method for manufacturing connecting type rudder arm flow guide device - Google Patents
Method for manufacturing connecting type rudder arm flow guide device Download PDFInfo
- Publication number
- CN102009322A CN102009322A CN 201010192958 CN201010192958A CN102009322A CN 102009322 A CN102009322 A CN 102009322A CN 201010192958 CN201010192958 CN 201010192958 CN 201010192958 A CN201010192958 A CN 201010192958A CN 102009322 A CN102009322 A CN 102009322A
- Authority
- CN
- China
- Prior art keywords
- flitch
- curvature
- circular arc
- line
- guiding device
- 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.)
- Granted
Links
Images
Abstract
The invention relates to a method for manufacturing a connecting type rudder arm flow guide device, which comprises the following steps of: designing the linear profile of a flow guide device and setting a fan-shaped plate seam line; blanking and marking; transversely extruding, bending and deforming by utilizing an oil press; baking by utilizing water and fire to achieve longitudinal and curve disadvantage bending deformation; and checking and processing allowance. The method of the invention can ensure the linear accuracy of the flow guide device, shorten the production period, reduce the production cost and ensure that the production design can be matched with the processing manufacture method of a production department and the connection of the moulded rudder arm of the flow guide device and a ship body has integrity.
Description
Technical field
The present invention relates to shipbuilding, particularly relate to the manufacture method of rudder horn interconnection system guiding device on the boats and ships.
Background technology
In shipbuilding, the effect of naval vessel rudder horn guiding device is: obtain uniform wake field, resistance is converted into power, thereby improve the speed of a ship or plane of boats and ships.Certain type ship rudder horn interconnection system guiding device is to run into first in the shipbuilding of my company, this type ship adopts deflector to carry out closed the connection between hull bottom and rudder horn, because being connected with rudder horn dripping water type line style, the line style in hull bottom zone has bigger irregular in length and breadth curvature surface, the deflector plate seam setting of producing in the design has certain technical requirements and difficulty with expansion, needs to consider multiple factor.Particularly be provided with, promptly will consider the reasonability of deflector part plate seam, consider how to reduce the operability and the adaptability of degree of curvature and process and assemble in length and breadth again on plate suture road.
According to traditional handicraft in the past, general have a processing method that should adopt mould compression moulding than the sheet material of macrobending degree to irregular in length and breadth.But certain type ship is not that serial ship (just useless after the ship model tool use) is just big as the production cost of employing Mould Machining mode, and the time of making mould is longer, from the Mold Making of publishing picture, strikes the making of sample upper die and lower die and generally wants a wheat harvesting period.Certain type ship rudder horn guiding device has only short one month time from the design process and assemble of publishing picture, and adopts the Mould Machining mode not allow in time as making guiding device, and financial cost is high again.
Summary of the invention
The objective of the invention is in order to overcome above-mentioned the deficiencies in the prior art, a kind of manufacture method of new rudder horn interconnection system guiding device is provided.Method of the present invention is not to the manufacturing first of the guiding device of leading ship newtype, does not have the globality of making under the ready-made mould situation to guarantee that rudder horn is connected with hull after the guiding device moulding.
In order to reach the foregoing invention purpose, technical scheme provided by the invention is as follows:
Unite tackling key problem by design department and segmentation manufacturing department, adopt flame forming plate to implement the processing of this deflector in conjunction with oil pump roof pressure cooked mode.By the actual line style of design department according to stern zone hull and rudder horn joining place, the concrete line style section and the plate suture road of making guiding device are implemented the part setting-out again and are launched, and sample case, sample certificate are provided earlier.Undertaken by firer group of job shop of segmentation manufacturing department that flame forming plate " ride sign indicating number " baking is burnt, oil pump roof pressure molding mode is processed.
The manufacture method of above-mentioned interconnection system rudder horn guiding device specifically comprises the steps:
1. design the line style section of guiding device, make and be connected between stern zone hull bottom curvature line style and the dripping water type rudder horn, according to arc transition between hull bottom curvature surface and the rudder horn, select suitable circular arc section data point, to guarantee to be connected the correctness of line style;
2. design fanning strip suture road, it is that benchmark is located to the both sides fan out with dripping water type rudder horn center of arc's point all that plate suture road is arranged on bow stern two ends, make the equilibrium of deflector part housing longitudinal curvature gesture stress point, implement fan-shaped location breaking joint line to reduce the vertical and horizontal curvature gesture of deflector, design the sample case in order to the check line style according to design result;
3. from the steel plate loading and unloading, the size of institute's blanking plate is two adjacent deflector part dimensions, and on this flitch, reserve panel shrinkage and allowance, in the workshop, roll out the unidirectional circular arc in cross section of deflector part, be transported to the hot work place then to carry out the processing of multidirectional curvature gesture;
4. in the hot work place, earlier by the flame forming plate workmen fiery processing line of on flitch, striking, above-mentioned flitch utilization " is ridden sign indicating number " to be fixed on the processing platform, and on flitch, apply downward pressure, implement thermal-flame and water-cooling method then simultaneously flitch is dried by the fire the burning roof pressure, hocket, make the horizontal slowly distortion of flitch to meet sample case size until the horizontal circular arc of flitch and vertical curvature through multi-pass operation;
5. the sample case is placed in the flitch, checks whether the amplitude circular arc line that needs vertically with transverse curvature meets the actual center of arc of line style and whether the edge is docile with the sample case, as if not meeting then repeating step 4. with the sample case;
6. allowance down will be cut out on the flitch, and it is stand-by separately to obtain two adjacent deflector parts.
In the present invention, the 1. middle guiding device line style section locator value acquiring method of described step is: is the datum mark fan out at rudder horn rudder bearer bow stern two ends with the rudder bearer center line, branch sections such as equilibrium are asked its locator value, make section and make jointing line simultaneously, R value at stern end location circular arc section is 150mm, the bow end is 250mm, branch circular arcs such as the overlapping equilibrium of circular arc section are adjusted S shape offset, offset fills a vacancy, emit the smooth curve of fairing, the difference that reduces circular arc housing curvature surface changes, and makes the stress point equilibrium of each part, increases housing streamline line style simultaneously.
In the present invention, the 4. middle flame forming plate of described step adds divides the regional line of extreme misery baking burning man-hour earlier, and the extreme misery comb hair is apart from being controlled at 40～50mm, and the intensity of a fire time of staying was controlled at 2～3 minutes, to reduce the distortion of material wave inception.
Further, the big part of the crooked camber of commentaries on classics circle deflector to bow stern two ends increases the breaking joint line again in the middle of circular arc, the width allowance for shrinkage places and changes 30mm into, and the length direction allowance for shrinkage places and changes 300mm into, and the method that combines with the oil pump roof pressure in flame forming plate is brought up to the sample rate.
Based on technique scheme, the manufacture method of interconnection system rudder horn guiding device of the present invention has been brought following technique effect than prior art:
The present invention unites effort to substitute the method for Mould Machining by design department and segmentation fabrication portion, and the specialized designs mould is processed again, has saved the time that mould manufactures and designs, and also can reduce manufacturing cost simultaneously.In addition, this method can be guaranteed the correctness of guiding device line style, can shorten the production cycle, reduces production costs, produce design can with the machining manufacture coupling of production division, can guarantee that rudder horn after the guiding device moulding is connected with hull and has globality.
Description of drawings
Fig. 1 is guiding device among the present invention, hull bottom line style and the figure that is connected of diversion shell line style.
Fig. 2 is to be the fan out section jointing line method to set up of center line with the rudder horn among the present invention.
Fig. 3 is that guiding device among the present invention, the setting-out of line style section launch view.
The specific embodiment
Below we come the manufacture method of interconnection system rudder horn guiding device of the present invention done further with specific embodiment in conjunction with the accompanying drawings and elaborate, but can not limit protection scope of the present invention with this.
The design of line style section and the fanning strip suture road of guiding device are provided with:
Say the line style section of design guiding device earlier, make and be connected between stern zone hull bottom curvature line style and the dripping water type rudder horn, according to arc transition between hull bottom curvature surface and the rudder horn, select suitable circular arc section data point, to guarantee to be connected the correctness of line style.
Above-mentioned guiding device line style section locator value acquiring method is: is the datum mark fan out at rudder horn rudder bearer bow stern two ends with the rudder bearer center line, and branch sections such as equilibrium are asked its locator value, make section and make jointing line simultaneously.The R value of stern end location circular arc section is 150mm, the bow end is 250mm, branch circular arcs such as the overlapping equilibrium of circular arc section are adjusted S shape offset, offset fills a vacancy, emit the smooth curve of fairing, the difference that has promptly reduced circular arc housing curvature surface changes, and makes the stress point equilibrium of each part, has increased housing streamline line style simultaneously again.
In the design phase of guiding device drawing, the circular arc value that at first will make the commentaries on classics circle guiding device shell plates at bow stern two ends is R150mm-250mm, and as benchmark, sets the anchor point of each section of circular arc, obtains each circular arc section on anchor point.Because it is different with the height and the width value that the hull bottom curve connects to change circle deflector part, other changes the circle section and is irregular ellipse.For this reason, in the setting-out process of sectional line style,, make different curvilinear plane coordinate figures the overlapping circular arc five equilibrium that carries out of all directions section.Refuting with batten on the basis of getting each branch offset, replenishing its damaged some offset according to the actual joint number difference situation of minute circular arc, establishing new line style data point with extending tangent rule, control changes and the progression difference with the curvature of each line segment of the fan out face of adjustment.Make line style progressively smooth transition to optimal light along point, and set up smoothly that the three-dimensional curved surface changes the circular arc line style, by the reasonability of customized section sample case Direct Test line style, see Fig. 3 simultaneously.
The line style design that is connected in guiding device and ship stern bottom its objective is and designs the sample case that cooperates deflector to make, and provide foundation for ruling on the deflector part.
Design fanning strip suture road, it is that benchmark is located to the both sides fan out with dripping water type rudder horn center of arc's point all that plate suture road is arranged on bow stern two ends, make the equilibrium of deflector part housing longitudinal curvature gesture stress point, implement fan-shaped location breaking joint line to reduce the vertical and horizontal curvature gesture of deflector, design the sample case in order to the check line style according to design result.Because the curvature surface of shipform itself, making changes circular deflector in length and breadth to all having degree of curvature.Be provided with at the plate seam for this reason and must consider actual degree of curvature factor.According to experience of practical, it is to reduce the effective method that changes round sheet material degree of curvature that fan out intercepting section is provided with jointing line.We are producing the design phase for this reason, finish at guiding device on the basis of line style design and have taked the fan-shaped method that jointing line is set at bow stern end, see Fig. 2.
The actual production construction stage of rudder horn guiding device:
At first, from the loading and unloading of monoblock steel plate, the size of institute's blanking plate is two adjacent deflector part dimensions, and reserves panel shrinkage and allowance on this flitch.Utilize lathe to roll out the unidirectional circular arc in cross section of deflector part then in the workshop, the making of multidirectional curvature gesture then needs to be transported to the hot work place and processes.
Secondly, after the deflector part is transported to the hot work place, earlier by the flame forming plate workmen fiery processing line of on flitch, striking, again above-mentioned flitch utilization " being ridden sign indicating number " is fixed on the processing platform, and on flitch, utilize oil pump to apply downward pressure, and implement thermal-flame and water-cooling method simultaneously flitch is dried by the fire the burning roof pressure, hocket, make and the horizontal slowly distortion of flitch meet sample case size until the horizontal circular arc of flitch and vertical curvature through multi-pass operation.Above-mentioned " riding sign indicating number " be a rod iron or steel pipe bending is certain angle from the middle part, the size of bending angle is carried out as required, needs " riding sign indicating number " of standby different bendings during construction.Then be provided with a plurality of circular holes on processing platform, this circular hole is that the end for " ride sign indicating number " inserts and designs.Can successfully the deflector part of difformity and bending degree be fixed by " riding sign indicating number " and processing platform.
Once more, the sample case that to make the design phase is placed into through in the flitch after the extreme misery processing, checking needs the amplitude circular arc line of vertical and transverse curvature whether to meet the actual center of arc of line style, and whether the edge of checking flitch is docile with the sample case, then do not repeat the constructing operation that above-mentioned thermal-flame and water cooling are dried by the fire the burning roof pressure if meet with the sample case, fit tightly until flitch and sample case, the flexibility of surperficial flitch and curvature gesture meet the requirements;
At last, cut out into allowance down on the flitch of stipulating flexibility and curvature gesture, and it is stand-by separately to obtain two adjacent deflector parts make.
In the flame forming plate process, to the material thickness of steel, temperature control, the time of the intensity of a fire and the control of distance, water spray control all has strict requirement.With the thick deflector of certain type ship 12mm is example, because its thickness of slab is thinner, according to shipbuilding material characteristic, we innovate on technology, require to accomplish low temperature, low coverage, fast, closely follow, taked following steps, for reducing temperature, comb hair distance is controlled between the 40-50mm (conventional be 100mm) intensity of a fire time of staying and is controlled at 2-3 minute (conventional be 6-8 minute, the water spray comb hair is immediately following the intensity of a fire) and has reduced the distortion of material wave inception, has guaranteed the fineness of material.
Processing method of the present invention can substitute traditional die processing method, can guarantee the correctness of guiding device sectional line style, reduces the degree of curvature in length and breadth of deflector, makes the diversion shell stress point equilibrium that is connected with boat bottom, strengthens casing rigidity.Flame forming plate " is ridden sign indicating number ", and the oil pump roof pressure organically combines, and relies on " riding sign indicating number " to dry by the fire the flame forming plate processing technology of burning, and can solve the curvature gesture of part deflector, and the oil pump roof pressure has strengthened the crooked dynamics of its key position, makes deflector to process gradually and puts in place.Because the deflector after the machine-shaping is still keeping firer's allowance for shrinkage, each part keeps vertically front and back 600mm of wide 250mm-, according to the sample case, can guarantee the appearance and size of deflector part, cutting accuracy makes and launches part line style radian and actual sample case coupling.
Claims (4)
1. the manufacture method of an interconnection system rudder horn guiding device is characterized in that, this manufacture method comprises the steps:
1. design the line style section of guiding device, make and be connected between stern zone hull bottom curvature line style and the dripping water type rudder horn, according to arc transition between hull bottom curvature surface and the rudder horn, select suitable circular arc section data point, to guarantee to be connected the correctness of line style;
2. design fanning strip suture road, it is that benchmark is located to the both sides fan out with dripping water type rudder horn center of arc's point all that plate suture road is arranged on bow stern two ends, make the equilibrium of deflector part housing longitudinal curvature gesture stress point, implement fan-shaped location breaking joint line to reduce the vertical and horizontal curvature gesture of deflector, design the sample case in order to the check line style according to design result;
3. from the steel plate loading and unloading, the size of institute's blanking plate is two adjacent deflector part dimensions, and on this flitch, reserve panel shrinkage and allowance, in the workshop, roll out the unidirectional circular arc in cross section of deflector part, be transported to the hot work place then to carry out the processing of multidirectional curvature gesture;
4. in the hot work place, earlier by the flame forming plate workmen fiery processing line of on flitch, striking, above-mentioned flitch utilization " is ridden sign indicating number " to be fixed on the processing platform, and on flitch, apply downward pressure, implement thermal-flame and water-cooling method then simultaneously flitch is dried by the fire the burning roof pressure, hocket, make the horizontal slowly distortion of flitch to meet sample case size until the horizontal circular arc of flitch and vertical curvature through multi-pass operation;
5. the sample case is placed in the flitch, checks whether the amplitude circular arc line that needs vertically with transverse curvature meets the actual center of arc of line style and whether the edge is docile with the sample case, as if not meeting then repeating step 4. with the sample case;
6. will cut out allowance down on the flitch, it is stand-by to obtain two adjacent deflector parts.
2. the manufacture method of a kind of interconnection system rudder horn guiding device according to claim 1, it is characterized in that, the 1. middle guiding device line style section locator value acquiring method of described step is: is the datum mark fan out at rudder horn rudder bearer bow stern two ends with the rudder bearer center line, branch sections such as equilibrium are asked its locator value, make section and make jointing line simultaneously, R value at stern end location circular arc section is 150mm, the bow end is 250mm, branch circular arcs such as the overlapping equilibrium of circular arc section are adjusted S shape offset, the offset that fills a vacancy is emitted the smooth curve of fairing, and the difference that reduces circular arc housing curvature surface changes, make the stress point equilibrium of each part, increase housing streamline line style simultaneously.
3. the manufacture method of a kind of interconnection system rudder horn guiding device according to claim 1, it is characterized in that, the 4. middle flame forming plate of described step adds divides the regional line of extreme misery baking burning man-hour earlier, and the extreme misery comb hair is apart from being controlled at 40～50mm, and the intensity of a fire time of staying was controlled at 2～3 minutes.
4. the manufacture method of a kind of interconnection system rudder horn guiding device according to claim 3, it is characterized in that, the big part of the crooked camber of commentaries on classics circle deflector to bow stern two ends increases the breaking joint line again in the middle of circular arc, the width allowance for shrinkage places and changes 30mm into, the length direction allowance for shrinkage places and changes 300mm into, combines to bring up to the sample rate with the oil pump roof pressure in flame forming plate.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2010101929587A CN102009322B (en) | 2010-06-04 | 2010-06-04 | Method for manufacturing connecting type rudder arm flow guide device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2010101929587A CN102009322B (en) | 2010-06-04 | 2010-06-04 | Method for manufacturing connecting type rudder arm flow guide device |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN102009322A true CN102009322A (en) | 2011-04-13 |
| CN102009322B CN102009322B (en) | 2012-05-30 |
Family
ID=43839751
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2010101929587A Active CN102009322B (en) | 2010-06-04 | 2010-06-04 | Method for manufacturing connecting type rudder arm flow guide device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN102009322B (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102380756A (en) * | 2011-06-01 | 2012-03-21 | 扬帆集团股份有限公司 | Allowance-free molding method for wrapper sheet of propeller shaft |
| CN104625447A (en) * | 2014-12-19 | 2015-05-20 | 华泰重工(南通)有限公司 | Technology for mounting fan-shaped guide tube |
| CN105783639A (en) * | 2016-04-15 | 2016-07-20 | 广州文冲船厂有限责任公司 | Rudder horn and rudder blade matching detection device, and manufacturing method of rudder horn and rudder blade |
| CN106270064A (en) * | 2016-08-25 | 2017-01-04 | 福建东南造船有限公司 | A kind of span is to drawing Flame process |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0540868A1 (en) * | 1991-11-02 | 1993-05-12 | Herbert Prof. Dr.-Ing. Schneekluth | Flow guiding device |
| CN1076418A (en) * | 1993-02-03 | 1993-09-22 | 江西省交通科学技术研究所 | Asymmetric guiding hole rudder |
| CN1166432A (en) * | 1996-03-20 | 1997-12-03 | 布隆福斯工业有限公司 | Guiding device |
| CN2633705Y (en) * | 2002-06-20 | 2004-08-18 | 宣怀亮 | Novel three-van sedan flow guide plate |
-
2010
- 2010-06-04 CN CN2010101929587A patent/CN102009322B/en active Active
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0540868A1 (en) * | 1991-11-02 | 1993-05-12 | Herbert Prof. Dr.-Ing. Schneekluth | Flow guiding device |
| CN1076418A (en) * | 1993-02-03 | 1993-09-22 | 江西省交通科学技术研究所 | Asymmetric guiding hole rudder |
| CN1166432A (en) * | 1996-03-20 | 1997-12-03 | 布隆福斯工业有限公司 | Guiding device |
| CN2633705Y (en) * | 2002-06-20 | 2004-08-18 | 宣怀亮 | Novel three-van sedan flow guide plate |
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102380756A (en) * | 2011-06-01 | 2012-03-21 | 扬帆集团股份有限公司 | Allowance-free molding method for wrapper sheet of propeller shaft |
| CN102380756B (en) * | 2011-06-01 | 2013-04-24 | 扬帆集团股份有限公司 | Allowance-free molding method for wrapper sheet of propeller shaft |
| CN104625447A (en) * | 2014-12-19 | 2015-05-20 | 华泰重工(南通)有限公司 | Technology for mounting fan-shaped guide tube |
| CN104625447B (en) * | 2014-12-19 | 2016-08-24 | 华泰重工(南通)有限公司 | A kind of fan-shaped conduit mounting process |
| CN105783639A (en) * | 2016-04-15 | 2016-07-20 | 广州文冲船厂有限责任公司 | Rudder horn and rudder blade matching detection device, and manufacturing method of rudder horn and rudder blade |
| CN105783639B (en) * | 2016-04-15 | 2018-04-20 | 广州文冲船厂有限责任公司 | Rudder horn and rudder blade matching detection device and the production method of rudder horn and rudder blade |
| CN106270064A (en) * | 2016-08-25 | 2017-01-04 | 福建东南造船有限公司 | A kind of span is to drawing Flame process |
Also Published As
| Publication number | Publication date |
|---|---|
| CN102009322B (en) | 2012-05-30 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN102009322B (en) | Method for manufacturing connecting type rudder arm flow guide device | |
| CN102982200B (en) | A kind of aircraft sheet metal components process modeling method for designing | |
| CN102501944B (en) | Method for manufacturing and installing inclined curved side port | |
| CN104406502B (en) | A kind of gas turbine blades forging stock physical dimension control method and detection model | |
| CN109263798B (en) | Method for lofting hull line of stern column asymmetric ship | |
| CN113714748B (en) | Manufacturing method of large wind tunnel contraction section | |
| CN101181926A (en) | Sectionalized assembling method for ship bow luff part | |
| CN107160104A (en) | A kind of method that ship model is processed with 3D printing | |
| CN104139129A (en) | Multi-point forming technology-applied forming method for curved-surface ship board | |
| CN112407183A (en) | Lofting design method for hawse pipe and anchor platform | |
| CN100431793C (en) | Large-scale complicated double-curvature wing wallboard chordwise shot-peening forming technique | |
| CN102191815B (en) | Making method of multi-curvature radius twisted steel pipe | |
| CN113148054B (en) | Modeling and lofting method of ship air guide sleeve | |
| CN112775288B (en) | Flexible forming method for ship outer plate with complex curved surface | |
| CN103658940B (en) | The manufacturing process of large-scale water turbine stator | |
| CN104924678A (en) | Composite honeycomb sandwich plate | |
| CN207808546U (en) | The forming frock of unmanned plane composite wing integral panel | |
| CN108858943B (en) | The more metal insert cable hood forming methods of segmented and moulding pressing mold | |
| CN106514096B (en) | A kind of auxiliary mould and method of manufacture rudder for ship | |
| CN100429589C (en) | Laser method for fine-tuning shaped objects of body case of airplane | |
| CN202056430U (en) | Multi-curvature radius crankle steel pipe | |
| CN106182790B (en) | Slender type dovetail shaped airvane leading edge forming method and moulding pressing mould and special gauge | |
| CN113458716B (en) | Cold pressing manufacturing method for bottom of furnace shell of card Lu Jinding combustion type hot-blast stove | |
| CN105346672A (en) | Ship machining method | |
| CN206926166U (en) | A kind of integrally insulating plate |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant |