JPH0364897U - - Google Patents

Info

Publication number
JPH0364897U
JPH0364897U JP12722489U JP12722489U JPH0364897U JP H0364897 U JPH0364897 U JP H0364897U JP 12722489 U JP12722489 U JP 12722489U JP 12722489 U JP12722489 U JP 12722489U JP H0364897 U JPH0364897 U JP H0364897U
Authority
JP
Japan
Prior art keywords
propeller
blade
distance
maximum
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
JP12722489U
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 JP12722489U priority Critical patent/JPH0364897U/ja
Publication of JPH0364897U publication Critical patent/JPH0364897U/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 drawings]

第1〜5図は本考案の一実施例としてのプロペ
ラに関するもので、第1図はそのプロペラ翼の断
面図、第2図はそのプロペラ翼の翼前縁からのそ
りの最大値までの距離C′と翼弦長Cとの比C′
/Cと、プロペラ中心からの距離rとのプロペラ
半径Rとの比r/Rとの関係を示したグラフ、第
3図はそのプロペラ翼の翼前縁から翼厚の最大値
までの距離Bと翼弦長Cとの比B/Cと、プロペ
ラ中心からの距離rとプロペラ半径Rとの比r/
Rとの関係を示したグラフ、第4図はそのプロペ
ラ翼の翼前縁からそりの最大値までの距離C′と
翼弦長Cとの比C′/Cと、変動圧力との関係を
示したグラフ、第5図はそのプロペラ翼の翼負圧
面における圧力分布を示したグラフであり、第6
図は従来のプロペラ翼における翼負圧面の圧力分
布図である。 1…プロペラ翼、1a…翼前縁、1b…翼後縁
、2…翼弦線、3…骨格線、B…翼厚の最大値の
翼前縁からの距離、C…翼弦長、C′…そりの最
大値の位置の翼前縁からの距離、d…翼厚、f…
そり、R…プロペラ半径。
Figures 1 to 5 relate to a propeller as an embodiment of the present invention. Figure 1 is a sectional view of the propeller blade, and Figure 2 is the distance from the leading edge of the propeller blade to the maximum value of warpage. Ratio C' between C' and chord length C
/C and the ratio r/R of the propeller radius R to the distance r from the propeller center. Figure 3 shows the distance B from the leading edge of the propeller blade to the maximum blade thickness. and the ratio B/C of the chord length C, and the ratio r/ of the distance r from the propeller center to the propeller radius R.
Figure 4 shows the relationship between the ratio C'/C between the distance C' from the leading edge of the propeller blade to the maximum value of warpage and the chord length C, and the fluctuating pressure. The graph shown in Figure 5 is a graph showing the pressure distribution on the suction surface of the propeller blade.
The figure is a pressure distribution diagram on the suction surface of a conventional propeller blade. 1...Propeller blade, 1a...Blade leading edge, 1b...Blade trailing edge, 2...Blade chord line, 3...Skeletal line, B...Distance of maximum blade thickness from the blade leading edge, C...Blade chord length, C ′...Distance from the blade leading edge to the position of maximum warpage, d...Blade thickness, f...
Sled, R...propeller radius.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] プロペラにおいて、同プロペラのプロペラ翼が
、同プロペラ翼をそのプロペラ軸中心線を回転軸
とする円筒面で切断した断面について、そりの最
大値の位置の翼前縁からの距離C′と翼弦長Cと
の比C′/Cの上記プロペラ翼の半径方向の分布
曲線が上記プロペラの半径をRとしたとき0.6
R〜0.7Rに最大値をもつ凸型の形状となり、
翼厚の最大値の位置の上記翼前縁からの距離Bと
上記弦長Cとの比B/Cの上記プロペラ翼の半径
方向の分布曲線が上記プロペラの半径をRとした
とき0.6R〜0.7Rに最大値をもつ凸型の形
状となるよう形成されていることを特徴とする、
プロペラ。
In a propeller, the distance C' from the leading edge of the blade at the position of the maximum warp and the blade chord of the propeller blade of the same propeller are measured by the distance C' from the leading edge of the blade at the position of the maximum warpage, with respect to a cross section of the propeller blade taken along a cylindrical surface with the propeller axis center line as the rotation axis. The distribution curve of the propeller blade in the radial direction of the ratio C'/C to the length C is 0.6 when the radius of the propeller is R.
It has a convex shape with a maximum value of R ~ 0.7R,
The distribution curve in the radial direction of the propeller blade of the ratio B/C of the distance B from the leading edge of the blade at the position of the maximum blade thickness to the chord length C is 0.6R when the radius of the propeller is R It is characterized by being formed to have a convex shape with a maximum value of ~0.7R,
propeller.
JP12722489U 1989-10-31 1989-10-31 Pending JPH0364897U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP12722489U JPH0364897U (en) 1989-10-31 1989-10-31

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP12722489U JPH0364897U (en) 1989-10-31 1989-10-31

Publications (1)

Publication Number Publication Date
JPH0364897U true JPH0364897U (en) 1991-06-25

Family

ID=31674990

Family Applications (1)

Application Number Title Priority Date Filing Date
JP12722489U Pending JPH0364897U (en) 1989-10-31 1989-10-31

Country Status (1)

Country Link
JP (1) JPH0364897U (en)

Similar Documents

Publication Publication Date Title
JPS6386923U (en)
JPH0364897U (en)
JPH0364899U (en)
JPH0364898U (en)
JPH0454997U (en)
JPH0313498U (en)
JPH032895U (en)
JPH0457311U (en)
JPH0332192U (en)
JPS6193397U (en)
JPS62110598U (en)
JPS61116322U (en)
JPS61138801U (en)
JPS62178296U (en)
JPS62102894U (en)
JPS6191041U (en)
JPH0243795U (en)
JPH02107000U (en)
JPS62153005U (en)
JPS6327553U (en)
JPS62152098U (en)
JPS62132288U (en)
JPH01152096U (en)
JPH0222700U (en)
JPS648380U (en)