JPS58101897A - Frp propeller vane with metal frame - Google Patents
Frp propeller vane with metal frameInfo
- Publication number
- JPS58101897A JPS58101897A JP20055381A JP20055381A JPS58101897A JP S58101897 A JPS58101897 A JP S58101897A JP 20055381 A JP20055381 A JP 20055381A JP 20055381 A JP20055381 A JP 20055381A JP S58101897 A JPS58101897 A JP S58101897A
- Authority
- JP
- Japan
- Prior art keywords
- frp
- vane
- center
- metal frame
- rim 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
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63H—MARINE PROPULSION OR STEERING
- B63H1/00—Propulsive elements directly acting on water
- B63H1/02—Propulsive elements directly acting on water of rotary type
- B63H1/12—Propulsive elements directly acting on water of rotary type with rotation axis substantially in propulsive direction
- B63H1/14—Propellers
Abstract
Description
【発明の詳細な説明】
衝撃強度の必要な翼縁部には金属製枠を使用して耐衝撃
性を向上すると共に、表面粗度の向上前に生物剛着回避
性の向上の要求される翼央部には積@FRP材を使用し
4それぞれの特性を活用すると共に、その境界部の接合
強度を向−ヒした複合材プロペラに関する。[Detailed Description of the Invention] A metal frame is used at the wing edge where impact strength is required to improve impact resistance, and the ability to avoid biological sticking is required before improving surface roughness. The present invention relates to a composite propeller that utilizes the characteristics of FRP materials in the center of the blade and improves the joint strength at the boundary.
耐蝕性の向上、重量低減等の目的で、FRP材を使用し
たプロペラが製作されたが、その欠点としては流木への
衝撃により翼縁部が破損すると共に、この破損状況がサ
サラ状になり、積層成形した部材が順次剥離を進行させ
る欠点があった。Propellers using FRP materials have been manufactured for the purpose of improving corrosion resistance and reducing weight, but the drawback is that the blade edges are damaged by impact with driftwood, and this damage becomes rough. There was a drawback that the laminated and molded members gradually peeled off.
黙しながらFRP材の有する軽量性及び耐蝕性は捨て帷
いものがあり、且つ省エネルギー的見地からするとプロ
ペラ重量の低減は、プロペラ軸々受部の摩擦抵抗を減少
させ、動力伝達効率の向上に有効なことが判明、してい
るので、金−とFRPの両者の特性を有効に生し、安全
にして且つ省エネルギー性にすぐれたプロペラ翼の製作
が必要となった。However, the light weight and corrosion resistance of FRP materials are worthless, and from an energy-saving perspective, reducing propeller weight reduces frictional resistance at the propeller shaft bearings and is effective in improving power transmission efficiency. As a result, it became necessary to produce a propeller blade that effectively takes advantage of the properties of both gold and FRP, and is safe and energy-saving.
本発明を図面によって詳しく説明する。The present invention will be explained in detail with reference to the drawings.
第1図はプロペラ全体図を示している。このプロペラ1
のプロペラ翼縫部1はプロペラ1と同−材料で、通常マ
ンガンブロンズ、アルミブロンズ或はステンレス鋼で製
作されている。この翼央部4は積層FRP材を張り合せ
て製作する。w12図はA−ム断面を示している。プロ
ペラ翼縁部2は中央に突起部8を備え、翼央部に嵌め込
み接合されるFRP材の脱落防止を計ると共に、両部材
の接着面積を増大することにより、金属枠とFRP材の
結合を物理的e化学的に強固にする、第8図はA−A断
面の代案であり、中央の突起部8の代りに、溝Sを設け
、この中にFRP材を入り込ませて補強結合する形、式
このようにして、本発明は船舶のプロペラ翼の翼縁部は
余興製の枠状とすると共に、この枠の翼中心側の形状を
中央が突起している形状か、又は中央が溝状に入り込ん
だ形状とし、プロペラ翼の中心部を形成する積11FR
P材を前進面及び後進面より張り合せて成形した時に、
金属枠の内側の突起又は溝によって、中心部のFRP−
が強固に把握され、流木等の衝撃に対しては翼縁部の金
属枠で防御し、中心部はFRP材を使用するξとにより
重量を低減すると共に、翼の表面粗度の向上、生物耐着
の防止並に動力伝達効率の向上を計った複合材料製プロ
ペラ翼であるので、省エネルギー効果も良好である。Figure 1 shows an overall view of the propeller. This propeller 1
The propeller blade seam 1 is made of the same material as the propeller 1, and is usually made of manganese bronze, aluminum bronze, or stainless steel. This wing center portion 4 is manufactured by laminating laminated FRP materials. Figure w12 shows the A-m cross section. The propeller blade edge 2 has a protrusion 8 in the center to prevent the FRP material that is fitted and joined to the blade center from falling off, and also to increase the bonding area between the two parts to facilitate the bonding of the metal frame and the FRP material. Fig. 8 shows an alternative plan of the A-A cross section, in which a groove S is provided in place of the central protrusion 8, and the FRP material is inserted into this to strengthen the structure for reinforcement. , Equation In this way, the present invention makes the blade edge of a propeller blade of a ship to be in the shape of a recreational frame, and the shape of the frame on the wing center side is either a shape with a protrusion in the center or a groove in the center. It has a shape that is intruded into the shape, and the product is 11FR, which forms the center part of the propeller blade.
When P material is pasted together from the forward and backward surfaces and formed,
The center FRP-
The metal frame at the wing edge protects against impact from driftwood, etc., and the center part uses FRP material to reduce weight, improve the surface roughness of the wing, and protect against biological damage. Since the propeller blades are made of composite material that prevents adhesion and improves power transmission efficiency, they also have good energy-saving effects.
i@1図はプロペラ全体図、第゛2図はムーム断面図、
188図はムーム断面図の代案を示す。
1、 プロペラ 2. プロペラ翼縁部8、突 起
4.積層FRP製翼製部央部溝
手続補正書(方式)
昭和57年5月1日
特許庁長官島田春樹殿
1、事住め表示
°昭和56年特許願第200558号
2、発明の名称
金属枠付FRPプロペラ翼
3、補正をする者
事件との関係 代表特許出願人
住所 山ロ県徳山市千代田町6番8号
4、補正の日付 昭和57年8月30日5、補正の対
象 図面
6、補正の内容 別紙の通りi@Figure 1 is an overall view of the propeller, Figure 2 is a cross-sectional view of the moom,
Figure 188 shows an alternative to the Moom sectional view. 1. Propeller 2. Propeller blade edge 8, protrusion 4. Laminated FRP wing manufacturing part central groove procedural amendment (method) May 1, 1980 Haruki Shimada, Commissioner of the Patent Office 1. Indication ° 1980 Patent Application No. 200558 2. Name of the invention With metal frame FRP propeller blade 3, Relationship with the case of the person making the amendment Representative patent applicant address: 6-8-4 Chiyoda-cho, Tokuyama City, Yamaro Prefecture, date of amendment: August 30, 1980 5, subject of amendment: Drawing 6, amendment Contents as attached
Claims (1)
、この枠の翼中心側の形状を中央が突起している形状か
又は中央が溝状に入り込んだ形状とし、プロペラ翼の中
心部を形成する積層FRP材を前進面及び後進面より!
W勢合せて成形した時に、金属棒の内側の突起又は溝に
よって、中心部のFRP層が1固に把握され、流木等の
衝撃に対しては翼縁部の金−枠で防御し、中心部はFR
P材を使用することにより重量を低減すると、共に、翼
の表面粗度の向上、生物耐着の防止盤に動力伝達効率の
向上を計った複合材料製プロペラ翼。If the edge of a ship's propeller blade is made of a metal frame, the shape of the frame on the center side of the wing should be either a protruding shape in the center or a groove-like shape in the center. Laminated FRP material forming the center from the forward and backward surfaces!
When the W is pressed together and formed, the center FRP layer is held firmly by the protrusions or grooves inside the metal rod, and the metal frame at the wing edge protects against impact from driftwood, etc., and the center The part is FR
A propeller blade made of composite material that reduces weight by using P material, improves the surface roughness of the blade, prevents biofouling, and improves power transmission efficiency.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP20055381A JPS58101897A (en) | 1981-12-11 | 1981-12-11 | Frp propeller vane with metal frame |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP20055381A JPS58101897A (en) | 1981-12-11 | 1981-12-11 | Frp propeller vane with metal frame |
Publications (1)
Publication Number | Publication Date |
---|---|
JPS58101897A true JPS58101897A (en) | 1983-06-17 |
Family
ID=16426218
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP20055381A Pending JPS58101897A (en) | 1981-12-11 | 1981-12-11 | Frp propeller vane with metal frame |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS58101897A (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2009286284A (en) * | 2008-05-29 | 2009-12-10 | Mitsubishi Heavy Ind Ltd | Blade structure of marine propeller |
JP2015199483A (en) * | 2014-04-04 | 2015-11-12 | ナカシマプロペラ株式会社 | Propeller for vessel |
JP2016084081A (en) * | 2014-10-28 | 2016-05-19 | 三菱重工業株式会社 | Marine propeller and method for manufacturing marine propeller |
JP2016193667A (en) * | 2015-03-31 | 2016-11-17 | 三菱重工業株式会社 | Marine propeller |
-
1981
- 1981-12-11 JP JP20055381A patent/JPS58101897A/en active Pending
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2009286284A (en) * | 2008-05-29 | 2009-12-10 | Mitsubishi Heavy Ind Ltd | Blade structure of marine propeller |
JP2015199483A (en) * | 2014-04-04 | 2015-11-12 | ナカシマプロペラ株式会社 | Propeller for vessel |
JP2016084081A (en) * | 2014-10-28 | 2016-05-19 | 三菱重工業株式会社 | Marine propeller and method for manufacturing marine propeller |
JP2016193667A (en) * | 2015-03-31 | 2016-11-17 | 三菱重工業株式会社 | Marine propeller |
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