JPH01161899U - - Google Patents

Info

Publication number
JPH01161899U
JPH01161899U JP5607088U JP5607088U JPH01161899U JP H01161899 U JPH01161899 U JP H01161899U JP 5607088 U JP5607088 U JP 5607088U JP 5607088 U JP5607088 U JP 5607088U JP H01161899 U JPH01161899 U JP H01161899U
Authority
JP
Japan
Prior art keywords
blade
hole
propeller
back surface
leading edge
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
JP5607088U
Other languages
Japanese (ja)
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 filed Critical
Priority to JP5607088U priority Critical patent/JPH01161899U/ja
Publication of JPH01161899U publication Critical patent/JPH01161899U/ja
Pending legal-status Critical Current

Links

Landscapes

  • Structures Of Non-Positive Displacement Pumps (AREA)

Description

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

第1図は本考案の一実施例の説明図、第2図は
第1図のA―A矢視図の拡大図、第3図は翼背面
に生ずる圧力分布の説明図、第4図は従来例の説
明図、第5図は第4図のB―B矢視図である。 図中1はプロペラ、2は翼、3は前縁、4は前
面、5は背面、6は翼根部、10は貫通孔を示す
Fig. 1 is an explanatory diagram of one embodiment of the present invention, Fig. 2 is an enlarged view of the A-A arrow view in Fig. 1, Fig. 3 is an explanatory diagram of the pressure distribution occurring on the back surface of the blade, and Fig. 4 is An explanatory diagram of the conventional example, FIG. 5 is a view taken along the line BB in FIG. 4. In the figure, 1 is a propeller, 2 is a blade, 3 is a leading edge, 4 is a front surface, 5 is a back surface, 6 is a blade root, and 10 is a through hole.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] プロペラの翼の翼根部に、前記翼の前縁を含む
前面から前記翼の背面の翼幅ほぼ中央に通ずる貫
通孔を穿設したことを特徴とするプロペラ翼構造
1. A propeller blade structure, characterized in that a through hole is formed in a blade root portion of a propeller blade, the through hole communicating from the front surface including the leading edge of the blade to approximately the center of the blade span of the back surface of the blade.
JP5607088U 1988-04-26 1988-04-26 Pending JPH01161899U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP5607088U JPH01161899U (en) 1988-04-26 1988-04-26

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP5607088U JPH01161899U (en) 1988-04-26 1988-04-26

Publications (1)

Publication Number Publication Date
JPH01161899U true JPH01161899U (en) 1989-11-10

Family

ID=31281956

Family Applications (1)

Application Number Title Priority Date Filing Date
JP5607088U Pending JPH01161899U (en) 1988-04-26 1988-04-26

Country Status (1)

Country Link
JP (1) JPH01161899U (en)

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