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JPH01237068A - Internal chilling type marine propeller - Google Patents

Internal chilling type marine propeller

Info

Publication number
JPH01237068A
JPH01237068A JP6522788A JP6522788A JPH01237068A JP H01237068 A JPH01237068 A JP H01237068A JP 6522788 A JP6522788 A JP 6522788A JP 6522788 A JP6522788 A JP 6522788A JP H01237068 A JPH01237068 A JP H01237068A
Authority
JP
Japan
Prior art keywords
boss
mold
blade
marine propeller
core
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
JP6522788A
Other languages
Japanese (ja)
Inventor
Shigeyoshi Hirayama
平山 重善
Tomonori Furukawa
友紀 古川
Toshiichi Furuse
古瀬 敏一
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 JP6522788A priority Critical patent/JPH01237068A/en
Publication of JPH01237068A publication Critical patent/JPH01237068A/en
Pending legal-status Critical Current

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  • Molds, Cores, And Manufacturing Methods Thereof (AREA)

Abstract

PURPOSE:To manufacture a large-sized propeller of high accuracy in the casting factory whose melting capacity is small scaled by fixing the blades made of individual bodies in advance by positioning them to the lower die of the mold for a boss, making the mold of a boss by fitting a core and an upper die and pouring a molten metal therein. CONSTITUTION:The blade 11 on which the projecting part 13 of a blade root part 12 is formed is manufactured. The plural blades 11 are fixed at their positions centering around the lower die 7 of the mold for boss in a complete state, a core 6 and the upper die 8 of the mold for boss are fitted with a print matrix 9 and the mold of a boss 1 provided with a flow-off 10 in advance is completed. A molten metal 3 is poured into this mold through a sprue 4 and runner 5 and each blade 11 is integrally fixed to the boss 1 by solidifying it. The build-up part 15 by welding with the blade root part 12 and boundary part 15 of the boss 1 is smoothly formed after its forming. The machining of a blade fitting face, etc., and the assembly work by fastening bolt, etc., can thus be abolished and the propeller having less dislocation of the tip position of each blade after the combined assembly can be manufactured.

Description

【発明の詳細な説明】 〔産業上の利用分野〕 本発明は大型舶用プロペラの鋳造に、航空機用プロペラ
、送風機用ファン等で軸部と軸部とが同または異材質の
一体化製造方法に適用される鋳包式舶用プロペラに関す
る。
[Detailed Description of the Invention] [Field of Industrial Application] The present invention is applicable to the casting of large marine propellers, aircraft propellers, blower fans, etc., in which the shaft portions are made of the same or different materials. Regarding applicable cast-in type marine propellers.

〔従来の技術〕[Conventional technology]

従来の組立式舶用プロペラの構造及び取付状態の詳細を
第3.4図に示す。
Figure 3.4 shows details of the structure and mounting state of a conventional assembled marine propeller.

大物鋳造品、例ば溶解能力など設備能力が不足している
鋳物工場での舶用大型プロペラの製造方法において、ボ
スB+と翼Yl とは別々に鋳造し、ボスB+は翼取付
面B2及び締付ねじ穴B3を機械加工する。
In the manufacturing method of large propellers for ships in foundries that lack equipment capacity such as large castings, such as melting capacity, the boss B+ and the blade Yl are cast separately, and the boss B+ is attached to the blade mounting surface B2 and the tightening Machine the screw hole B3.

同様に、翼YIは翼根部Y2の取付面Y3と締付穴Y4
を機械加工する。
Similarly, the blade YI is connected to the mounting surface Y3 of the blade root Y2 and the tightening hole Y4.
machined.

更に、ボスB1と翼Y+とを締付ボルトYSにより結合
、組立てる。
Furthermore, the boss B1 and the wing Y+ are connected and assembled using a tightening bolt YS.

その後にボスB+及び翼根部Y2の全凹部B4はセメン
ト、または合成樹脂等で埋め、成形し裏作する。
After that, the boss B+ and the entire concave portion B4 of the blade root Y2 are filled with cement or synthetic resin, and then molded and made.

〔発明が解決しようとする課題〕[Problem to be solved by the invention]

前述した組立式舶用プロペラでは、ボスB+の翼取付面
B2及び締付ねじ穴B3の機械加工、同様に、各翼Y1
の翼根部Y2の取付面Y3と締付穴Y4の機械加工、更
には、それらの組立作業が必要であることや、締付ポル
トY5等の部品製作が必要である。また、ボスB+及び
翼根部Y2の外周に凹部B4が発生するため、セメント
または合成樹脂による埋め、成形作業が必要である。
In the prefabricated marine propeller described above, the blade mounting surface B2 and the tightening screw hole B3 of the boss B+ are machined, and each blade Y1 is similarly machined.
It is necessary to machine the mounting surface Y3 of the blade root Y2 and the tightening hole Y4, as well as to assemble them, and to manufacture parts such as the tightening port Y5. Further, since a recess B4 is generated on the outer periphery of the boss B+ and the blade root Y2, it is necessary to fill it with cement or synthetic resin and mold it.

更に、ボスB+の翼取付面B2、翼Y+の取付面Y3の
機械加工誤差(特に角度誤差)が結合組立後の各翼端位
置やピッチを大きく狂わせることがあるなどの問題を呈
した。
Furthermore, machining errors (particularly angular errors) on the blade attachment surface B2 of the boss B+ and the attachment surface Y3 of the blade Y+ sometimes caused a large deviation in the position and pitch of each blade tip after assembly.

〔課朗を解決するための手段〕[Means to solve the problem]

本発明は上記課題を解決するために、予め単体で製作さ
れた翼をボス用鋳型の下型に完成状態で位置決め固定し
、中子、同上型を取付けてボスの鋳型としてから溶解湯
を前記鋳型に注入して前記ボスと翼を一体化した舶用プ
ロペラである。すなわち、予め設置されたボス用鋳型の
下型に、翼根部が凸部を有した複数枚の翼を完成状態で
位置決め固定してから中子、同上型を取付けてできたボ
スの鋳型に溶解湯を鋳込むことを特徴とする鋳包式舶用
プロペラな役秩4ゐ。
In order to solve the above-mentioned problems, the present invention positions and fixes a blade that has been manufactured as a single unit in the completed state to the lower mold of a boss mold, attaches a core and the same mold as the boss mold, and then pours molten metal into the boss mold. This is a marine propeller in which the boss and blades are integrated by injection into a mold. In other words, multiple blades with convex blade roots are positioned and fixed in the completed state to the lower mold of the boss mold that has been installed in advance, and then the core and the same mold are attached and melted into the created boss mold. Yakuchichi 4i is a casting-type marine propeller that is characterized by the ability to cast hot water.

〔作 用〕[For production]

本発明の鋳包式舶用プロペラは上記のように製造される
舶用プロペラとなるので各部分ごとに分割鋳造となるこ
とから溶解能力が小規模な鋳物工場での大型プロペラの
製作が可能となり、また機械加工不用のための工作機械
設備、及び関連作業等を排除して加工精度の向上を図っ
た舶用プロペラである。
Since the cast-in type marine propeller of the present invention is manufactured as described above, each part is separately cast, making it possible to manufacture a large propeller in a foundry with a small melting capacity. This is a marine propeller that aims to improve machining accuracy by eliminating machine tool equipment and related work that does not require machining.

〔実施例〕〔Example〕

以下、本発明を図面に示す実施例に基づいて具体的に説
明する。第1図は本発明の一実施例に係る鋳包式舶用プ
ロペラの部分切欠き断面を示す斜視図。第2図は本実施
例に係る組込み鋳造態様を示す鋳型の縦断面図である。
Hereinafter, the present invention will be specifically described based on embodiments shown in the drawings. FIG. 1 is a perspective view showing a partially cutaway cross section of a cast-in type marine propeller according to an embodiment of the present invention. FIG. 2 is a longitudinal cross-sectional view of a mold showing an integrated casting mode according to this embodiment.

以下にその詳細を記す。The details are described below.

第1.2図において、1はボス、2は治具、3は溶解湯
、4は湯口、5は湯道、6は中子、7は下型、8は上型
、9は幅木、1oは上がり、11は翼、12は翼根部、
13は凸部、15は境界部である。
In Figure 1.2, 1 is a boss, 2 is a jig, 3 is a melting metal, 4 is a sprue, 5 is a runner, 6 is a core, 7 is a lower mold, 8 is an upper mold, 9 is a baseboard, 1o is up, 11 is the wing, 12 is the wing root,
13 is a convex portion, and 15 is a boundary portion.

第1図は予め単体で製作された複数の翼11を完成状態
に図示しないボス用鋳型の下型を中心にして位置を固定
し、図示しない中子、上型を取付けた後に溶解湯を注入
し、ボス1と翼11を一体化凝固させる。更にボス1と
!@11との境界部15は溶接により肉盛り(15) 
してから滑らかに成形した翼潤色式の舶用プロペラであ
る。次いで第1図の詳細構造並びに工程を$2図で説明
すると、翼11には図示しない従来の翼鋳型の翼根部1
2に同図のように凸部13が形成されることがら鋳込部
には凹部を設けて鋳造することとなる。また、ボスエは
ボス用鋳型の下型7中心正1こ予め完成された6翼11
を同図に示す治具2及び前記下型7上に第1図で示すよ
うに等ピッチ放射状に位に決めされて固定される。次い
で中子6及びボス用鋳型の上型8を幅木9を添えて 4
取付け、前もって上がり10を設けたボス1の鋳型を完
成し、完成したボス用鋳型に溶解湯3を湯口4、湯道5
を通じて注入し凝固させることにより6翼11をボス1
に一体的に固定される。
Figure 1 shows a plurality of blades 11 that have been manufactured individually in advance, fixed in position around the lower mold of a boss mold (not shown) in a completed state, and molten metal poured after attaching a core and an upper mold (not shown). Then, the boss 1 and the blade 11 are solidified into one piece. Plus boss 1! The boundary part 15 with @11 is built up by welding (15)
This is a marine propeller with colored blades that have been molded smoothly. Next, the detailed structure and process of FIG. 1 will be explained with reference to FIG.
Since the convex part 13 is formed in the casting part 2 as shown in the figure, the casting part is cast with a concave part provided therein. In addition, the bosse is made of 6 wings 11 completed in advance with 7 centers of the lower mold of the boss mold.
are fixed on the jig 2 shown in the figure and the lower die 7 at equal pitches radially as shown in FIG. Next, attach the core 6 and the upper mold 8 of the boss mold with the baseboard 9 4
After installation, complete the boss 1 mold with the riser 10 provided in advance, and pour the molten metal 3 into the completed boss mold through the sprue 4 and runner 5.
The 6 wings 11 are made into the boss 1 by injecting and solidifying them through the
is integrally fixed to.

上記のとおりボス1と6翼11の一体化された舶用プロ
ペラは翼根部12とボス1の境界部において溶接による
肉盛り部15を形成してから滑らかに成形されることに
より製作され、必要に応じてボス1の上下端を機械加工
で完成する舶用プロペラである。
As mentioned above, a marine propeller with integrated boss 1 and six blades 11 is manufactured by forming a built-up part 15 by welding at the boundary between the blade root 12 and boss 1, and then smoothly molding it. This is a marine propeller in which the upper and lower ends of the boss 1 are completed by machining.

〔発明の効果〕〔Effect of the invention〕

以上、具体的に説明したように本発明における鋳包式舶
用プロペラは溶解能力等の小規模の鋳物工場での大型プ
ロペラ製造が可能となり、翼取付面等の機械加工及び締
付ポルト等による組立作業が廃止可能となって結合組立
後の各ス先端位置の狂いが少ない舶用プロペラを製作で
きるものである。
As specifically explained above, the cast-in type marine propeller of the present invention enables manufacturing of large propellers in a small-scale foundry with melting capacity, etc., and assembly by machining of the blade mounting surface, etc., and tightening ports, etc. It is possible to manufacture a marine propeller in which the work can be abolished and the position of the tip of each shaft after assembly is less likely to be misaligned.

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

第1図は本発明の一実施例に係る鋳包式舶用プロペラの
部分切欠き断面を示す斜視図、第2図は本実施例に係る
組込み鋳造態様を示す鋳型の縦断面図、第3図は従来の
組立式舶用プロペラの部分切欠き断面を示す斜視図、第
4図は従米のボス及び翼の取付は状態を示す第3図■部
の拡大図である。 1・・・ボス、2・・・治具、3・・・溶解湯、4・・
・湯口、5・・・湯道、6・・・中子、7・・・下型、
8・・・上型、9・・・幅木、10・・・上がり、11
・・・翼、12・・・翼根部、13・・・凸部、15・
・・境界部。 筏埋友石用新 月4m
FIG. 1 is a perspective view showing a partially cutaway cross section of a cast-in type marine propeller according to an embodiment of the present invention, FIG. 2 is a longitudinal cross-sectional view of a mold showing an integrated casting mode according to the present embodiment, and FIG. 3 4 is a perspective view showing a partially cutaway cross-section of a conventional prefabricated marine propeller, and FIG. 4 is an enlarged view of section 3 in FIG. 3 showing how the boss and blades are attached. 1... Boss, 2... Jig, 3... Molten metal, 4...
・Spout, 5... Runway, 6... Core, 7... Lower mold,
8... Upper mold, 9... Skirting board, 10... Up, 11
... Wing, 12... Wing root, 13... Convex portion, 15.
... Boundary area. Shingetsu 4m for raft buried tomostone

Claims (1)

【特許請求の範囲】[Claims] 予め設置されたボス用鋳型の下型に、翼根部が凸部を有
した複数枚の翼を完成状態で位置決め固定してから中子
、同上型を取付けてできたボスの鋳型に溶解湯を鋳込む
ことを特徴とする鋳包式舶用プロペラ。
After positioning and fixing multiple blades with convex blade roots in the completed state to the lower mold of the boss mold that was previously installed, the core and the same mold were attached, and molten metal was poured into the boss mold that was created. A cast-in type marine propeller that is characterized by being cast.
JP6522788A 1988-03-18 1988-03-18 Internal chilling type marine propeller Pending JPH01237068A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP6522788A JPH01237068A (en) 1988-03-18 1988-03-18 Internal chilling type marine propeller

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP6522788A JPH01237068A (en) 1988-03-18 1988-03-18 Internal chilling type marine propeller

Publications (1)

Publication Number Publication Date
JPH01237068A true JPH01237068A (en) 1989-09-21

Family

ID=13280821

Family Applications (1)

Application Number Title Priority Date Filing Date
JP6522788A Pending JPH01237068A (en) 1988-03-18 1988-03-18 Internal chilling type marine propeller

Country Status (1)

Country Link
JP (1) JPH01237068A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1726523A2 (en) 2005-05-27 2006-11-29 FB DESIGN S.r.l. Boat propeller and method for assembling the same
US9011100B2 (en) 2012-09-12 2015-04-21 Mehmet Nevres ULGEN Demountable propeller

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1726523A2 (en) 2005-05-27 2006-11-29 FB DESIGN S.r.l. Boat propeller and method for assembling the same
US9011100B2 (en) 2012-09-12 2015-04-21 Mehmet Nevres ULGEN Demountable propeller

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