JPS61123436A - Production of three dimentional curved face wing - Google Patents

Production of three dimentional curved face wing

Info

Publication number
JPS61123436A
JPS61123436A JP59244663A JP24466384A JPS61123436A JP S61123436 A JPS61123436 A JP S61123436A JP 59244663 A JP59244663 A JP 59244663A JP 24466384 A JP24466384 A JP 24466384A JP S61123436 A JPS61123436 A JP S61123436A
Authority
JP
Japan
Prior art keywords
wing
plate
face
rolling
wing part
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.)
Pending
Application number
JP59244663A
Other languages
Japanese (ja)
Inventor
Tsuyoshi Kawazoe
強 川添
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.)
Mitsubishi Heavy Industries Ltd
Original Assignee
Mitsubishi Heavy Industries 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 Mitsubishi Heavy Industries Ltd filed Critical Mitsubishi Heavy Industries Ltd
Priority to JP59244663A priority Critical patent/JPS61123436A/en
Publication of JPS61123436A publication Critical patent/JPS61123436A/en
Pending legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2250/00—Geometry
    • F05B2250/70—Shape
    • F05B2250/71—Shape curved
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00—Energy generation through renewable energy sources
    • Y02E10/20—Hydro energy

Landscapes

  • Hydraulic Turbines (AREA)

Abstract

PURPOSE:To produce at low cost the three dimensional curved face wing of cavitation resistance and errosion resistance by forming a wing part with rolling a plate material and by welding the wing part to a boss part. CONSTITUTION:The blank plate 10 for wing part which is cut in the prescribed wing width and length by a gas cutting, etc. is prepared. The plate 10 shall be of the material having high tensile strength, high sea water corrosion fatigue strength, high caviation resistance and high corrosion resistance. The wing face 13 of three dimentional curved face is then produced with rolling the surface of the wing part blank plate 10 by rolling a rolling roller 12 along the wing face gage plate 11 with pinching from both parts the blank plate 10 by the wing part gage plate 11. Then the boss part made in advance by casting or welding, etc. with using inexpensive ferrous materials and the wing part 14 where the wing face 13 is produced are welded, thereafter a residual stress is removed with locally annealing by applying a panel heater, etc. to the weld part 16. The machining on the wing part 14 is performed on its rear progressing face and outline only, then. With welding the wing part 14 to the boss part 15 in the prescribed numbers a complete product is made by performing an annealing and machining uniformly.

Description

【発明の詳細な説明】 〈産業上の利用分野〉 本発明は、船用プロペラ、水車等の三次元曲面翼の製造
方法に関する。DETAILED DESCRIPTION OF THE INVENTION <Industrial Application Field> The present invention relates to a method for manufacturing three-dimensionally curved blades for marine propellers, water turbines, and the like.

〈従来の技術〉 従来の三次元曲面翼の製造方法は、第６図に示すように
、鋳物砂等で上型１と下型２を製作し、これらを組合せ
てできた鋳型３の空洞部４に金属材料の溶湯５をとりベ
ロよシ流し込み、鋳造法にて三次元曲面残部７とボス部
８を製作する。蹄造にて製作された翼部７は第７図に示
すように翼面加工機９で機械加工される。<Prior art> As shown in Fig. 6, the conventional method for manufacturing three-dimensionally curved blades is to manufacture an upper mold 1 and a lower mold 2 using molding sand, etc., and then to create a hollow part of a mold 3 made by combining these molds. In Step 4, a molten metal 5 is taken and poured into the mold, and a three-dimensional curved surface remaining portion 7 and a boss portion 8 are manufactured by a casting method. The wing section 7 manufactured by the hoofing machine is machined by a wing surface processing machine 9 as shown in FIG.

〈発明が解決しようとする問題点〉 上記従来の製造方法は下記の欠点を有している。<Problem that the invention seeks to solve> The above conventional manufacturing method has the following drawbacks.

（１）　　三次元曲面翼の鋳型を作る場合、楓と同一形
状の模型本塁が必要となる。(1) When making a mold for a three-dimensional curved wing, a model base with the same shape as a maple is required.

（２）鋳型造型に多大な工数がかかる。(2) It takes a lot of man-hours to make a mold.

（３）翼部とボス部が同時鋳造となシ、翼部とボス部が
同一材料となる（一般に翼部は強度メンバーであるため
高強度材料を必要とするが、ボス部はその必要はなく、
安価な材料でよい）。(3) The wing section and the boss section are not cast simultaneously, and the wing section and the boss section are made of the same material (generally, the wing section is a strong member and therefore requires high-strength material, but the boss section does not require this. Without,
(You can use inexpensive materials).

（４）大量の高価な金属材料を溶解するため、溶解費が
高くなる。(4) Since a large amount of expensive metal material is melted, melting costs become high.

（５）鋳造であるため、強度上重要な１部に鋳巣が発生
しやすく、強度が低下して興の折損を誘発する。(5) Since it is cast, cavities are likely to occur in parts that are important for strength, reducing strength and causing breakage of the roof.

（６）鋳造であるため、楓の表面硬度を高くするコトが
できず、キャビテーション、二ローションの損傷を受け
やすい。(6) Since it is cast, it is not possible to increase the surface hardness of the maple, and it is susceptible to cavitation and damage from lotion.

本発明は、上記点に鑑みてなされたもので、上記欠点を
解消した三次元曲面翼の製造方法を提供することを目的
とする。The present invention has been made in view of the above points, and an object of the present invention is to provide a method for manufacturing a three-dimensionally curved wing that eliminates the above drawbacks.

く問題点を解決するための手段〉 上記目的を達成するための本発明の三次元曲面楓の製造
方法は、板材を圧延して翼部を形成し、当該＋４部をボ
ス部に溶接することを特徴とする。Means for Solving the Problems> The method for manufacturing a three-dimensional curved maple of the present invention to achieve the above object includes rolling a plate material to form a wing part, and welding the +4 part to a boss part. It is characterized by

〈実施例〉 以下、本発明の一実施例を図面に基づいて説明する。ま
ず、ガスカットなどで所定の輿幅及び長さに切断された
列部素材板１０（第３図参照）を準備する。この板の材
料は引張強度、海水腐食疲労強度、耐キヤビテーシヨン
腐食性共に高い材料（例えば銅合金、ステンレス鋼等）
とする。<Example> An example of the present invention will be described below based on the drawings. First, a row material plate 10 (see FIG. 3), which is cut to a predetermined width and length by gas cutting or the like, is prepared. The material of this plate is a material with high tensile strength, seawater corrosion fatigue strength, and cavitation corrosion resistance (e.g. copper alloy, stainless steel, etc.)
shall be.

次に、上記翼部素材板１０を第４図に示すように３面ゲ
ージ板１１で両方より挟み、楓面ゲー・ジ板１１に沿っ
て圧延ローラ１２をころがし、列部素材板１０表面（ピ
ッチ面もしくは前進面）を圧延して三次元曲面の翼面１
３を創成する。Next, as shown in FIG. 4, the wing material plate 10 is sandwiched between two three-sided gauge plates 11, and the rolling roller 12 is rolled along the maple-faced gauge plate 11. A three-dimensionally curved wing surface 1 is obtained by rolling the pitch surface or forward movement surface.
Create 3.

次に、第５図に示すように、あらかじめ安価な鉄系材料
を使用して鋳造又は溶接法などで作つておいたボス部１
５と前記翼面１３を創成した翼部１４とを溶接し、溶接
後、溶接部１６にパネルヒータを当て局部焼鈍して残留
応力を除去する。Next, as shown in Fig. 5, the boss part 1 is made in advance by casting or welding using an inexpensive iron-based material.
5 and the wing portion 14 where the wing surface 13 has been created are welded, and after welding, a panel heater is applied to the welded portion 16 to locally anneal it to remove residual stress.

次に、翼部１４を機械加工し、所定の翼面に加工する。Next, the wing portion 14 is machined into a predetermined wing surface.

後進面と輪郭のみ機械加工すればよい。Only the reversing surface and contour need to be machined.

翼部１４をボス部１５に所定の数（５楓、４翼、あるい
は３Ｍ）溶接し、前記のように焼鈍機械加工を行って完
成品（第１〜２図参照）とする。A predetermined number (5, 4, or 3M) of wing parts 14 are welded to the boss part 15, and annealing and machining are performed as described above to obtain a finished product (see FIGS. 1 and 2).

〈発明の効果〉 以上説明したように、本発明くよれば、下記の効果を秦
する。<Effects of the Invention> As explained above, according to the present invention, the following effects are achieved.

（１）三次元曲面翼の鋳型を作る必要がなく、楓の木型
も不要となる。(1) There is no need to make a mold for a three-dimensionally curved wing, and there is no need for a maple tree mold.

（２）多大な工数を必要とする鋳型造型の作業を省略で
きる。(2) It is possible to omit the work of mold making, which requires a large number of man-hours.

（３）翼部とボス部は溶接にて結合するため、異種材料
とすることができる。例えば、グロペラの場合、翼部は
海水腐食疲労強度の高い鋼合金系材料を使用し、ボス部
は安価な鉄系材料を使用できる。(3) Since the wing portion and the boss portion are joined by welding, they can be made of different materials. For example, in the case of a groper, the wing portion can be made of a steel alloy material with high seawater corrosion fatigue strength, and the boss portion can be made of an inexpensive iron material.

（４）単純な形状のボス部を鋳造で製作しても大量の金
属溶解を必要どしない。(4) A large amount of metal melting is not required even if a boss portion with a simple shape is manufactured by casting.

（５）翼部は元来欠陥の少ない板材を使用し、しかも表
面はローラで圧延するため、万一欠陥があってもローラ
で押しつぶされて健全な表面に改善される。(5) The blades are made of plate material with fewer defects, and the surface is rolled with rollers, so even if there is a defect, it will be crushed by the rollers and the surface will be improved to a healthy surface.

（６）圧延によシ表面硬度が高くなり、耐キャビテーシ
ョン、二ローション性が高りなる。(6) Rolling increases the surface hardness and improves cavitation resistance and lotion resistance.

【図面の簡単な説明】[Brief explanation of the drawing]

第１〜５図は本発明の一実施例を示し、第１図は本発明
によって製造された三次元曲面部を示す側面因、第２図
は同縦断面図、第３図は翼部素材板を示す斜視図、第４
図は圧延される翼部素材板を示す斜視図、第５図は溶接
された翼部とボス部を示す斜視図、第６〜７図は従来例
を示し、第６図は鋳造作業を示す断面図、第７図は鋳造
後の機械加工作業を示す図である。 図面中、 １０は翼部素材板、１１は翼面ゲージ板、１２は圧延ロ
ーラ、１３は翼面、１４は翼部、１５はボス部、１６は
溶接部である。 特許出　願人　三菱重工業株式会社 復代理人　弁理士　　光　石　士　部（他１名）第３図
　　　　　第４図 第５図Figures 1 to 5 show an embodiment of the present invention, Figure 1 is a side view showing a three-dimensional curved part manufactured by the present invention, Figure 2 is a longitudinal sectional view of the same, and Figure 3 is a wing material. Perspective view showing the plate, No. 4
The figure is a perspective view showing the blade material plate being rolled, Figure 5 is a perspective view showing the welded blade part and boss part, Figures 6 and 7 show the conventional example, and Figure 6 shows the casting operation. The sectional view, FIG. 7, is a diagram showing the machining operation after casting. In the drawings, 10 is a blade material plate, 11 is a blade gauge plate, 12 is a rolling roller, 13 is a blade surface, 14 is a blade part, 15 is a boss part, and 16 is a welded part. Patent Applicant: Mitsubishi Heavy Industries, Ltd. Sub-Agent Patent Attorney: Mitsubishi Shibu (and 1 other person) Figure 3 Figure 4 Figure 5

Claims (1)

【特許請求の範囲】[Claims] 板材を圧延して翼部を形成し、当該翼部をボス部に溶接
することを特徴とする三次元曲面翼の製造方法。A method for manufacturing a three-dimensional curved wing, comprising rolling a plate material to form a wing section, and welding the wing section to a boss section.
JP59244663A 1984-11-21 1984-11-21 Production of three dimentional curved face wing Pending JPS61123436A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP59244663A JPS61123436A (en) 1984-11-21 1984-11-21 Production of three dimentional curved face wing

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP59244663A JPS61123436A (en) 1984-11-21 1984-11-21 Production of three dimentional curved face wing

Publications (1)

Publication Number Publication Date
JPS61123436A true JPS61123436A (en) 1986-06-11

Family

ID=17122099

Family Applications (1)

Application Number Title Priority Date Filing Date
JP59244663A Pending JPS61123436A (en) 1984-11-21 1984-11-21 Production of three dimentional curved face wing

Country Status (1)

Country Link
JP (1) JPS61123436A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR20210087218A (en) * 2020-01-02 2021-07-12 주식회사 에이치티씨 Manufacturing method of high pressure vessel for direction control

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR20210087218A (en) * 2020-01-02 2021-07-12 주식회사 에이치티씨 Manufacturing method of high pressure vessel for direction control

Similar Documents

Publication Publication Date Title
FR2569136A1 (en) DEVICE FOR MANUFACTURING A DRAFT BY A SUPERIMPOSED WELDING PROCESS
US3889512A (en) Steering knuckles and method of forming the same
US4164061A (en) Method of making rotor blades of radial-axial hydraulic machines
CN204867195U (en) Chill arbor bender
CN100556564C (en) The manufacture method of composite strip steel for wood blade
AU2002317208B2 (en) Method for the production of metal profiles
JPS61123436A (en) Production of three dimentional curved face wing
CN215271038U (en) Hollow comb
US2640737A (en) One-piece forged steel railway journal box
US3635070A (en) Method of working cellular material
US2275585A (en) Method of making composite metal
JPS60221143A (en) Manufacture of rack shaft of rack and pinion steering gear
JPH01107972A (en) Manufacture of titanium made propeller
Weflen et al. Wire Arc Additive Manufacturing of Low Carbon Steel for Casting Applications
US4459880A (en) Method of making dies
JPH10252217A (en) Transformed shape steel
JPS6099449A (en) Die forging method of blank materials for nippers prior to assembly
JPS63180594A (en) Rudder forming method
US2306861A (en) Method for stamping sheet metal
JPS5817704B2 (en) Osmanthus Cylinder No. Seizouhouhou
JPS62140723A (en) Manufacture of trimming mold
JP2547805B2 (en) Mold manufacturing method
CA1083794A (en) Method of making rotor blades of radial-axial hydraulic machines
IT202100014393A1 (en) METHOD OF FORGING ITEMS
RU2041042C1 (en) Cutting tool manufacture method