JP5721895B1 - Propeller gauge with fixed measuring position - Google Patents

Propeller gauge with fixed measuring position Download PDF

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JP5721895B1
JP5721895B1 JP2014224225A JP2014224225A JP5721895B1 JP 5721895 B1 JP5721895 B1 JP 5721895B1 JP 2014224225 A JP2014224225 A JP 2014224225A JP 2014224225 A JP2014224225 A JP 2014224225A JP 5721895 B1 JP5721895 B1 JP 5721895B1
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建二 金子
建二 金子
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Abstract

【課題】プロペラの羽根の翼面形状の計測や保存、修正作業を容易で確実にできる計測位置固定型のプロペラケージを提供する。【解決手段】プロペラ100のプロペラボス102の中空部に下部1bを挿入できるシャフト1と、シャフトの上部1aから径方向に延びる連結部2と、連結部2の径方向をシャフト側と先端側に分けると、先端側において下方に延び、プロペラの羽根の翼面と少なくとも線p−q(但し、pとqは線の両端)で接触可能な計測部3と、連結部のシャフト側又はシャフトの上部において下方に延び、プロペラボス102から延びる羽根101の根元領域BAで羽根の翼面と接触可能となる、回転可能な前記シャフト1を固定する固定部4とを備える計測位置固定型のプロペラゲージを提供する。【選択図】図1A propeller cage having a fixed measurement position that can easily and reliably measure, store, and correct the blade surface shape of a blade of a propeller. A shaft 1 in which a lower portion 1b can be inserted into a hollow portion of a propeller boss 102 of a propeller 100, a connecting portion 2 extending in a radial direction from the upper portion 1a of the shaft, and a radial direction of the connecting portion 2 on a shaft side and a distal end side. When divided, the measuring part 3 that extends downward on the tip side and can contact at least the line pq (where p and q are both ends of the line) with the blade surface of the blade of the propeller, the shaft side of the connecting part or the shaft A measuring position fixed type propeller gauge comprising a fixing part 4 for fixing the rotatable shaft 1, which extends downward in the upper part and can come into contact with the blade surface of the blade in a root area BA of the blade 101 extending from the propeller boss 102. I will provide a. [Selection] Figure 1

Description

本発明は、競艇用船外機のプロペラの羽根の形状を計測して保存できるプロペラゲージに関する。   The present invention relates to a propeller gauge capable of measuring and storing the shape of the propeller blades of a boat racing outboard motor.

競艇用船外機のプロペラの羽根の形状は、モーターボートのスピードに大きな影響を与える。競艇選手は、過去に好感触を得たプロペラの羽根の形状を記憶するためプロペラゲージを用い、現在の羽根を加工や修正してその羽根の形状を再現するためにプロペラゲージを用いる。また、プロペラは、ボートやモーターとの相性があり、羽根の形状を修正して試運転する調整を繰り返して最適化するものであるが、プロペラゲージを用いて修正前の形状を記憶しておくと、羽根の曲面のどの位置における変更が、プロペラ全体としてボートの推進力にどのような効果を生じるかを判断することが可能となる。   The shape of the propeller blades of a racing outboard motor greatly affects the speed of the motorboat. A boat racer uses a propeller gauge to memorize the shape of a propeller blade that has received a good feeling in the past, and uses a propeller gauge to reproduce and reshape the current blade by processing or modifying it. In addition, the propeller is compatible with boats and motors, and it is optimized by repeatedly adjusting the shape of the blade and performing trial operation, but if the shape before correction is stored using a propeller gauge It is possible to determine what effect the change in the position of the curved surface of the blade has on the propulsive force of the boat as a whole propeller.

通常用いられているプロペラゲージ110を図15に示す。プロペラゲージ110は、後述の特許文献2の図8に従来技術として記載されているものと同じであり、プロペラ100のプロペラボスの中空部に下部111bを挿入できるシャフト111と、シャフト111の上部111aから径方向に延びる連結部112と、連結部112の先端から下方に延びる計測部113を備える。プロペラゲージ110を用いてプロペラ100の翼面の形状を記憶するときは、プラスチックの計測部113をやすりで削り、プロペラ100の翼面と合致させる。プロペラ100の翼面と合致させた計測部113を有するプロペラゲージ110を用いて、記憶した翼面の形状を、調整しようとする別のプロペラに再現するときは、そのシャフト111を挿入し、プロペラの翼面と計測部113が合致するまで木槌等で翼面をたたいて調整する。   A commonly used propeller gauge 110 is shown in FIG. The propeller gauge 110 is the same as that described in the prior art in FIG. 8 of Patent Document 2 to be described later. And a measuring part 113 extending downward from the tip of the connecting part 112. When the shape of the blade surface of the propeller 100 is stored using the propeller gauge 110, the plastic measuring unit 113 is shaved with a file to match the blade surface of the propeller 100. When reproducing the memorized shape of the blade surface on another propeller to be adjusted using the propeller gauge 110 having the measuring unit 113 matched with the blade surface of the propeller 100, the shaft 111 is inserted and the propeller is inserted. The blade surface is struck with a mallet or the like until the blade surface and the measuring unit 113 are matched.

平成24年4月以前は、競艇選手はプロペラを購入して所有できたため、好みのプロペラを再利用でき、納得できる羽根の形状が得られるまで修正や試運転を繰り返してレースに出場することができた。しかし、平成24年4月以降は、競艇選手がプロペラを所有できなくなり、レース場において競艇用船外機に備え付けられたプロペラを借用するため、プロペラを自宅に持ち帰ることができなくなり、レースに出場するまでの限られた時間内でプロペラの羽根の翼面を好みの形状に修正する必要が生じた。また、提供されるプロペラは、多く場合、他の選手が以前に使用したものであり、その選手の好みや癖が反映された形状となっているため、自分の好みの形状への修正は、新品のプロペラの修正よりも困難となっている。したがって、操作が簡単で信頼できるプロペラゲージへのニーズは、一層高くなっている。   Prior to April 2012, boat racers were able to purchase and own propellers, so they could reuse their favorite propellers and participate in the race with repeated corrections and trial runs until a satisfactory blade shape was obtained. It was. However, after April 2012, boat racers can no longer own propellers, and the propellers installed on the boat's outboard motors are borrowed at the race track, so the propellers can no longer be taken home and enter the race. It was necessary to modify the blade surface of the propeller blades to a desired shape within a limited time. Also, the propellers provided are often used by other players before, and the shape reflects the player's preferences and habits. It is more difficult than correcting a new propeller. Therefore, there is a growing need for a propeller gauge that is easy to operate and reliable.

特許文献1は、競走艇の船外機のプロペラの羽根の翼面形状記録装置として、プロペラボスの中空部内に挿入される軸部と、この軸部から延びた連結部と、この連結部に固定される記録ゲージ部とから構成され、記録ゲージ部は連結部が固定される支持体と、この支持体に羽根の外端に向けて所定間隔を存して複数本配設される調整ネジとを備え、調整ネジは支持体に螺着されて羽根の翼面形状に合わせて支持体より突出する量が調整できるように上下動可能である装置を提供する。
特許文献2は、プロペラゲージとして、プロペラの中央部に形成された穴に挿入する挿入部と、挿入部と接続されるシャフト部と、シャフト部と接続され、プロペラの形状を記憶する形状記憶部とを備え、形状記憶部は、プロペラに当てるための複数の棒状部材と、複数の棒状部材を通すための穴が形成され、複数の棒状部材を、複数の棒状部材の軸方向に移動可能にするとともに、軸方向と直交する方向に移動しないように保持する保持部と、複数の棒状部材を保持部により保持した状態から軸方向と直交する方向に締め付けることにより、複数の棒状部材を軸方向に移動しないように固定する固定部とを備えるゲージを提供する。
Patent Document 1 discloses a propeller blade blade surface shape recording device for an outboard motor of a racing boat, a shaft portion inserted into a hollow portion of a propeller boss, a connecting portion extending from the shaft portion, and a connecting portion. The recording gauge unit is configured to be fixed, and the recording gauge unit includes a support body to which the coupling unit is fixed, and a plurality of adjustment screws arranged on the support body at predetermined intervals toward the outer end of the blade. The adjusting screw is screwed to the support body and is capable of moving up and down so that the amount protruding from the support body can be adjusted according to the blade surface shape of the blade.
Patent Document 2 discloses, as a propeller gauge, an insertion portion that is inserted into a hole formed in a central portion of the propeller, a shaft portion that is connected to the insertion portion, and a shape storage portion that is connected to the shaft portion and stores the shape of the propeller. The shape memory unit is formed with a plurality of rod-shaped members for contacting the propeller and holes for passing the plurality of rod-shaped members, and the plurality of rod-shaped members can be moved in the axial direction of the plurality of rod-shaped members. And holding the plurality of rod-shaped members in the axial direction by tightening in a direction perpendicular to the axial direction from a state in which the plurality of rod-shaped members are held by the holding portion so as not to move in a direction orthogonal to the axial direction. There is provided a gauge including a fixing portion that is fixed so as not to move.

特許第5073864号公報Japanese Patent No. 5073864 特開2014−16331号公報JP 2014-16331 A

本発明者は、図15に示すプロペラゲージ110を用いて、記憶した翼面の形状を対象となるプロペラに再現することが困難な理由は、翼面の形状を記憶する際に、翼面と合致するようにプラスチックの計測部113をやすりで正確に削ることの難しさではなく、翼面の形状を再現する際に、再現しようとする翼面上の位置が移動していることにあると見出した。すなわち、シャフト111を回転させて形状を再現しようとする翼面と計測部113が接触した部分でゲージが固定されるため、計測部が固定部を兼ねており、記憶した翼面のプロペラ上の位置と、再現しようとする翼面のプロペラ上の位置を同一とする位置決めの基準がなく、計測部113が接触した部分で翼面形状を再現させているにすぎないことを見出した。翼面の上下方向の突出の程度が、記憶した翼面の形状の上下方向の突出の程度と同じである位置において形状を再現しているにすぎず、プロペラ間の突出程度の違いや木槌等による修正時の当該位置の移動により無視できない誤差が生じる。例えば、翼面のプロペラ上の位置が高いと、シャフト111を回転して再現しようとすると、記憶した翼面の位置まで届かず手前で止まり、翼面の位置が低いと、シャフト111を回転して再現しようとすると、記憶した位置を過ぎてしまい、翼面上高さが異なる別の位置で形状を合わせることになる。
特許文献1の翼面形状記録装置では、軸部をプロペラボスの中空部に挿入した際の角度位置を記録するために、軸部の下部(裏面)に印しを付しているが、軸部を固定できないため、羽根の翼面形状に合わせて調整ネジの支持体からの突出量を調整する際に、軸部が回転して印しからずれる課題がある。また、調整ネジの突出量の調整は軸部の上部方向からの目視によるため、同時に印しのある軸部の下部(裏面)を目視できず、頻繁にプロペラを裏返して軸部の下部(裏面)の印しの位置を確認しなければならず、作業効率が悪くなる課題がある。
特許文献2のプロペラゲージでは、形状記憶部が、下部の中央部に、プロペラ方向に向かうように配置された棒状部材4より太い棒状部材9を備え、プロペラゲージの位置決めをする際の目印としているが、プロペラの羽根の翼面の中央に配置されるため、プロペラの修正の影響を受けて棒状部材9が配置された位置の翼面形状が例えば上下に変動し、プロペラの羽根の翼面の形状の記憶に誤差を生じる課題がある。
すなわち、特許文献1と特許文献2は、記憶した翼面の形状を対象となるプロペラに再現することが困難な理由が、翼面の形状を記憶する際に、翼面と合致するようにプラスチックの計測部113をやすりで正確に削ることの難しさにあることの発想の下で、やすりを用いないプロペラゲージを提供する。したがって、やすりで正確に削ることの難しさは克服できるが、記憶した翼面のプロペラ上の位置と、再現しようとする翼面のプロペラ上の位置を同一とする位置決めの基準が固定されておらず、翼面形状の再現に無視できない誤差を生ずる。
また、特許文献1では羽根の翼面形状を調整ネジの先端を翼面に接触させることで特定し、特許文献2では羽根の翼面形状を棒状部材4の先端を翼面に接触させることで特定し、いずれも羽根の翼面形状を点でなぞるものであるため、調整ネジや棒状部材4が多数必要となり、操作が煩雑になるだけなく、目視による誤差を生じやすい。
本発明は、プロペラの羽根の翼面形状の計測や保存、修正作業を容易で確実にできるプロペラケージを提供する。
The present inventor uses the propeller gauge 110 shown in FIG. 15 for the reason that it is difficult to reproduce the memorized blade surface shape to the target propeller. It is not difficult to precisely cut the plastic measuring unit 113 with a file so as to match, but when reproducing the shape of the blade surface, the position on the blade surface to be reproduced is moving I found it. That is, since the gauge is fixed at the portion where the measurement portion 113 is in contact with the blade surface to be reproduced by rotating the shaft 111, the measurement portion also serves as the fixed portion, and the memorized blade surface on the propeller It has been found that there is no positioning reference that makes the position and the position on the propeller of the blade surface to be reproduced the same, and that the blade surface shape is only reproduced at the portion where the measuring unit 113 is in contact. It only reproduces the shape at a position where the vertical protrusion of the blade surface is the same as the vertical protrusion of the memorized blade surface. An error that cannot be ignored occurs due to the movement of the position at the time of correction due to the above. For example, if the position of the blade surface on the propeller is high, if you attempt to rotate and reproduce the shaft 111, it will not reach the memorized blade surface position and will stop before it, and if the blade surface position is low, the shaft 111 will rotate. If you try to reproduce it, the stored position will pass, and the shape will be matched at another position with different height on the wing surface.
In the wing surface shape recording device of Patent Document 1, in order to record the angular position when the shaft portion is inserted into the hollow portion of the propeller boss, a mark is given to the lower portion (back surface) of the shaft portion. Since the portion cannot be fixed, there is a problem that the shaft portion is rotated and misaligned when the protruding amount of the adjusting screw from the support body is adjusted in accordance with the blade surface shape of the blade. In addition, since the adjustment amount of the adjustment screw is visually observed from the upper part of the shaft part, the lower part (back side) of the marked shaft part cannot be seen at the same time. ) Has to be confirmed, and there is a problem that the work efficiency is deteriorated.
In the propeller gauge of Patent Document 2, the shape memory unit includes a bar-shaped member 9 that is thicker than the bar-shaped member 4 disposed in the lower central portion so as to face the propeller direction, and serves as a mark for positioning the propeller gauge. However, since it is arranged at the center of the blade surface of the propeller blade, the blade surface shape at the position where the rod-like member 9 is placed is affected by the correction of the propeller, for example, up and down, and the blade surface of the propeller blade is changed. There is a problem that an error occurs in memory of shapes.
In other words, Patent Document 1 and Patent Document 2 describe that the reason why it is difficult to reproduce the memorized blade surface shape on the target propeller is to match the blade surface when storing the blade surface shape. A propeller gauge that does not use a file is provided based on the idea that it is difficult to accurately cut the measurement unit 113 of the file. Therefore, the difficulty of cutting with a file can be overcome, but the memorized position of the blade surface on the propeller and the position on the propeller of the blade surface to be reproduced are fixed. Therefore, a non-negligible error occurs in the reproduction of the blade surface shape.
Further, in Patent Document 1, the blade surface shape of the blade is specified by bringing the tip of the adjustment screw into contact with the blade surface, and in Patent Document 2, the blade surface shape of the blade is brought into contact with the blade surface of the blade member 4. Since both are specified and the blade surface shape of the blade is traced with a point, a large number of adjustment screws and rod-like members 4 are required, which not only complicates the operation but also tends to cause visual errors.
The present invention provides a propeller cage capable of easily and reliably measuring, storing, and correcting the blade surface shape of a propeller blade.

本発明者は、記憶した翼面のプロペラ上の位置と、再現しようとする翼面のプロペラ上の位置を同一とする位置決めの基準を、木槌等のよる羽根の修正の影響を受けにくい、他の領域よりも厚い羽根の根元領域とした計測位置固定型のプロペラケージすることにより、再現の精度が大幅に改善されることを見出し、本発明を完成した。
本発明によれば、プロペラのプロペラボスの中空部に下部を挿入できるシャフトと、前記シャフトの上部から径方向に延びる連結部と、前記連結部の径方向をシャフト側と先端側に分けると、前記先端側において下方に延び、前記プロペラの羽根の翼面と少なくとも線p−q(但し、pとqは線の両端)で接触可能な計測部と、前記連結部の前記シャフト側又は前記シャフトの上部において下方に延び、前記プロペラボスから延びる前記羽根の根元領域で前記羽根の翼面と接触可能となる、回転可能な前記シャフトを固定する固定部とを備える計測位置固定型のプロペラゲージを提供できる。
本発明の計測位置固定型のプロペラゲージの好ましい態様では、前記連結部が、前記シャフト側において不動であり、前記先端側において径方向に延びるギャップを挟んで上下可動片又は周方向の左右可動片に分岐され、前記上下可動片の少なくとも一方又は前記左右可動片の少なくとも一方に設けた調整ねじで前記ギャップの間隔を収縮又は拡張させることにより上下方向又は左右方向に動かすことができる可撓性の可動部であり、前記計測部が、前記上もしくは下可動片から、又は前記右もしくは左可動片から下方に延び、前記プロペラの羽根の翼面と少なくとも前記線p−qで接触可能であり、前記可動部の先端側を上下方向又は左右方向に動かすことにより、前記計測部が少なくとも前記線p−qの全体を前記羽根の翼面を接触させて前記羽根の翼面をなぞることができる。
前記好ましい態様の好ましい第1の形態例では、前記上可動片及び前記下可動片が、前記シャフト側に配置されたスペーサを介して前記ギャップを隔てて上可動板の板面と下可動板の板面を上下方向に重ねて構成され、(i)前記上可動板と前記下可動板のいずれか一方が上下方向に前記ギャップに向かう第1貫通ねじ穴と、前記第1貫通ねじ穴に前記ギャップに向けて挿入される第1調整ねじを備え、かつ/又は(ii)前記第1貫通ねじ穴とは前記シャフトからの距離が異なっても同じでもよい周方向の異なる位置に前記上可動板と前記下可動板のいずれか一方が上下方向に前記ギャップに向けて第2バカ穴を備えるとともに他方が前記第2バカ穴に連通する第2ねじ穴を備え、さらに前記第2バカ穴から前記ギャップに向けて挿入され前記第2ねじ穴に挿入できる第2調整ねじを備え、前記計測部が、周方向で前記上可動板もしくは前記下可動板から下方に延び、前記羽根の翼面と少なくとも前記線p−qで接触可能な計測部であり、前記第1貫通ねじ穴に前記第1調整ねじを回してねじ込むと、前記第1調整ねじの先端が他方の可動板と接触すると止まり、さらに回すと前記上可動板と前記下可動板のギャップが上下方向に拡張して、前記計測部が前記上可動板から延びるときは前記羽根の翼面から遠ざかるように作用し、前記計測部が前記下可動板から延びるときは前記羽根の翼面に近づくように作用し、前記第2バカ穴を経て前記第2ねじ穴に前記第2調整ねじを回してねじ込むと、前記第2バカ穴を通過後前記第2ねじ穴に侵入して前記第2調整ねじの頭部が前記第2バカ穴の入口で止まり、さらに回すと前記上可動板と前記下可動板のギャップが上下方向に収縮して、前記計測部が前記上可動板から延びるときは前記羽根の翼面に近づくように作用し、前記計測部が前記下可動板から延びるときは前記羽根の翼面から遠ざかるように作用し、両作用を組み合わせて少なくとも前記線p−qの全体を前記羽根の翼面を接触させて前記羽根の翼面をなぞることができる。
前記好ましい態様の好ましい第2の形態例では、前記上可動片及び前記下可動片が、前記シャフト側に配置されたスペーサを介して前記ギャップを隔てて上可動板の板面と下可動板の板面を上下方向に重ねて構成され、(i)前記上可動板と前記下可動板のいずれか一方が上下方向に前記ギャップに向かう第1貫通ねじ穴と、前記第1貫通ねじ穴に前記ギャップに向けて挿入される第1調整ねじを備え、かつ/又は(ii)前記第1貫通ねじ穴とは径方向の異なる位置に前記上可動板と前記下可動板のいずれか一方が上下方向に前記ギャップに向けて第2バカ穴を備えるとともに他方が前記第2バカ穴に連通する第2ねじ穴を備え、さらに前記第2バカ穴から前記ギャップに向けて挿入され前記第2ねじ穴に挿入できる第2調整ねじを備え、前記計測部が、径方向で前記上可動板もしくは前記下可動板から下方に延び、前記羽根の翼面と少なくとも前記線p−qで接触可能な計測部であり、前記第1貫通ねじ穴に前記第1調整ねじを回してねじ込むと、前記第1調整ねじの先端が他方の可動板と接触すると止まり、さらに回すと前記上可動板と前記下可動板のギャップが上下方向に拡張して、前記計測部が前記上可動板から延びるときは前記羽根の翼面から遠ざかるように作用し、前記計測部が前記下可動板から延びるときは前記羽根の翼面に近づくように作用し、前記第2バカ穴を経て前記第2ねじ穴に前記第2調整ねじを回してねじ込むと、前記第2バカ穴を通過後前記第2ねじ穴に侵入して前記第2調整ねじの頭部が前記第2バカ穴の入口で止まり、さらに回すと前記上可動板と前記下可動板のギャップが上下方向に収縮して、前記計測部が前記上可動板から延びるときは前記羽根の翼面に近づくように作用し、前記計測部が前記下可動板から延びるときは前記羽根の翼面から遠ざかるように作用し、両作用を組み合わせて少なくとも前記線p−qの全体を前記羽根の翼面を接触させて前記羽根の翼面をなぞることができる。
前記好ましい態様の好ましい第3の形態例では、前記可動部が、厚さ方向を周方向に配置して板面が上下方向に延びる可動板の先端側に導入された径方向の切込みにより前記ギャップを隔てて前記上可動片と前記下可動片に分けられ、(i)前記上可動片と前記下可動片のいずれか一方が上下方向に第1貫通ねじ穴と、前記第1貫通ねじ穴に前記ギャップに向けて挿入される第1調整ねじを備え、かつ/又は(ii)前記第1貫通ねじ穴とは径方向の異なる位置に前記上可動片と前記下可動片のいずれか一方が上下方向に第2バカ穴を備えるとともに他方が前記第2バカ穴に連通する第2ねじ穴を備え、さらに前記第2バカ穴から前記ギャップに向けて挿入され前記第2ねじ穴に挿入できる第2調整ねじを備え、前記計測部が、径方向で前記下可動片から下方に延び、前記羽根の翼面と少なくとも前記線p−qで接触可能な計測部であり、前記第1貫通ねじ穴に前記第1調整ねじを回してねじ込むと、前記第1調整ねじの先端が他方の可動片と接触すると止まり、さらに回すと前記上可動片と前記下可動片のギャップが上下方向に拡張し前記計測部が前記羽根の翼面に近づくように作用し、前記第2バカ穴を経て前記第2ねじ穴に前記第2調整ねじを回してねじ込むと、前記第2バカ穴を通過後前記第2ねじ穴に侵入して前記第2調整ねじの頭部が前記第2バカ穴の入口で止まり、さらに回すと前記上可動片と前記下可動片のギャップが上下方向に収縮し前記計測部が前記羽根の翼面から遠ざかるように作用し、両作用を組み合わせて少なくとも前記線p−qの全体を前記羽根の翼面を接触させて前記羽根の翼面をなぞることができる。
前記好ましい態様の好ましい第4の形態例では、前記可動部が、板面を周方向に配置した可動板の先端側に導入された径方向の切込みにより周方向に前記ギャップを隔てて前記左可動片と前記右可動片に分けられ、(i)前記左可動片と前記右可動片のいずれか一方が左右方向に第1貫通ねじ穴と、前記第1貫通ねじ穴に前記ギャップに向けて挿入される第1調整ねじを備え、かつ/又は(ii)前記第1貫通ねじ穴とは径方向の異なる位置に前記左可動片と前記右可動片のいずれか一方が左右方向に第2バカ穴を備えるとともに他方が前記第2バカ穴に連通する第2ねじ穴を備え、さらに前記第2バカ穴から前記ギャップに向けて挿入され前記第2ねじ穴に挿入できる第2調整ねじを備え、前記計測部が、径方向で前記左可動片又は前記右可動片のいずれか一方から下方に延び、前記羽根の翼面とのなす角度が垂直より5〜30度の範囲で大きい又は小さい角度で前記羽根の翼面と少なくとも前記線p−qで接触可能な計測部であり、前記第1貫通ねじ穴に前記第1調整ねじを回してねじ込むと、前記第1調整ねじの先端が他方の可動片と接触すると止まり、さらに回すと前記左可動片と前記右可動片のギャップが周方向に拡張し前記計測部が前記羽根の翼面を第1周方向に移動するように作用し、前記第2バカ穴を経て前記第2ねじ穴に前記第2調整ねじを回してねじ込むと、前記第2バカ穴を通過後前記第2ねじ穴に侵入して前記第2調整ねじの頭部が前記第2バカ穴の入口で止まり、さらに回すと前記左可動片と前記右可動片のギャップが周方向に収縮し前記計測部が前記羽根の翼面を前記第1周方向とは反対の第2周方向に移動するように作用し、両作用を組み合わせて少なくとも前記線p−qの全体を前記羽根の翼面を接触させて前記羽根の翼面をなぞることができる。
前記好ましい態様の好ましい第1の形態例では、好ましくは、前記可動部の周方向で前記シャフトからの距離が異なっても同じでもよい位置に、前記第1貫通ねじ穴と前記第1調整ねじが少なくとも2組存在し、前記第2バカ穴と前記第2ねじ穴と前記第2調整ねじが少なくとも2組存在する。前記好ましい態様の好ましい第2〜4のいずれかの形態例では、好ましくは、前記可動部の径方向で前記シャフトからの距離が異なる位置に、前記第1貫通ねじ穴と前記第1調整ねじが少なくとも2組存在し、前記第2バカ穴と前記第2ねじ穴と前記第2調整ねじが少なくとも1組存在する。
前記好ましい態様では、好ましくは、前記連結部又は前記可動部の上下方向が、前記シャフトの上下方向から前記プロぺラのピッチ角に対応させて傾いている。また、前記好ましい態様では、好ましくは、前記第1調整ねじの先端が接触する、前記他方となる前記上可動片もしくは前記下可動片又は前記左可動片もしくは前記右可動片の接触箇所に補強材を配置する。
The inventor is less affected by the correction of the blades such as a mallet, and the positioning reference that makes the memorized position of the blade surface on the propeller the same as the position on the propeller of the blade surface to be reproduced. The present invention has been completed by finding that the accuracy of reproduction is greatly improved by using a propeller cage of a fixed measurement position that is a thicker blade root region than other regions.
According to the present invention, when a shaft capable of inserting a lower portion into a hollow portion of a propeller of a propeller, a connecting portion extending in a radial direction from the upper portion of the shaft, and dividing a radial direction of the connecting portion into a shaft side and a tip side, A measuring part that extends downward on the tip side and can contact at least the line pq (where p and q are both ends of the line) with the blade surface of the blade of the propeller, the shaft side of the connecting part or the shaft A measuring position fixed type propeller gauge comprising a fixing portion for fixing the rotatable shaft, which extends downward from an upper portion of the blade and is in contact with a blade surface of the blade in a root region of the blade extending from the propeller boss. Can be provided.
In a preferred aspect of the propeller gauge of the measurement position fixed type according to the present invention, the connecting portion is immovable on the shaft side and vertically movable pieces or circumferential left and right movable pieces with a gap extending in the radial direction on the tip side. Is flexible so that it can be moved vertically or horizontally by contracting or expanding the gap with an adjusting screw provided on at least one of the vertically movable pieces or at least one of the horizontally movable pieces. A movable part, wherein the measuring part extends downward from the upper or lower movable piece or from the right or left movable piece, and can contact the blade surface of the blade of the propeller at least on the line pq. By moving the tip side of the movable part in the vertical direction or the horizontal direction, the measurement part brings at least the entire line pq into contact with the blade surface of the blade. You can trace the blade surface of the blade.
In a preferred first embodiment of the preferred aspect, the upper movable piece and the lower movable piece are separated from each other between the plate surface of the upper movable plate and the lower movable plate with the gap interposed therebetween via a spacer disposed on the shaft side. (I) a first through screw hole in which one of the upper movable plate and the lower movable plate is directed to the gap in the vertical direction, and the first through screw hole A first adjusting screw inserted toward the gap, and / or (ii) the upper movable plate at a different position in the circumferential direction that may or may not be the same distance from the shaft as the first through screw hole. And the lower movable plate have a second hole in the vertical direction toward the gap, and the other has a second screw hole communicating with the second hole, and further from the second hole. Before being inserted into the gap A second adjusting screw that can be inserted into the second screw hole is provided, and the measuring portion extends downward from the upper movable plate or the lower movable plate in the circumferential direction, and contacts with the blade surface of the blade at least at the line pq When the first adjustment screw is turned and screwed into the first through screw hole, it stops when the tip of the first adjustment screw comes into contact with the other movable plate, and when further turned, the upper movable plate and When the gap of the lower movable plate expands in the vertical direction and the measurement unit extends from the upper movable plate, it acts to move away from the blade surface of the blade, and when the measurement unit extends from the lower movable plate Acting so as to approach the blade surface of the blade, and turning the second adjusting screw into the second screw hole through the second hole, the second screw hole is passed through the second hole and then the second screw hole. The head of the second adjustment screw enters and the second bar It stops at the inlet of the hole, and when further turned, the gap between the upper movable plate and the lower movable plate contracts in the vertical direction so that when the measuring part extends from the upper movable plate, it approaches the blade surface of the blade. When the measuring unit extends from the lower movable plate, it acts to move away from the blade surface of the blade, and by combining both operations, at least the entire line pq is brought into contact with the blade surface of the blade. The blade surface of the blade can be traced.
In a preferred second embodiment of the preferred embodiment, the upper movable piece and the lower movable piece are separated from each other between the plate surface of the upper movable plate and the lower movable plate via a spacer disposed on the shaft side with the gap interposed therebetween. (I) a first through screw hole in which one of the upper movable plate and the lower movable plate is directed to the gap in the vertical direction, and the first through screw hole A first adjusting screw inserted toward the gap, and / or (ii) one of the upper movable plate and the lower movable plate in the vertical direction at a position different from the first through screw hole in the radial direction. The second screw hole is provided to the gap, and the other has a second screw hole that communicates with the second screw hole, and is inserted into the second screw hole from the second screw hole toward the gap. With a second adjustment screw that can be inserted The measurement unit is a measurement unit that extends downward in the radial direction from the upper movable plate or the lower movable plate and is capable of contacting at least the line pq with the blade surface of the blade, and the first through screw hole When the first adjusting screw is turned and screwed in, it stops when the tip of the first adjusting screw comes into contact with the other movable plate, and when further turned, the gap between the upper movable plate and the lower movable plate expands in the vertical direction, When the measurement unit extends from the upper movable plate, it acts to move away from the blade surface of the blade, and when the measurement unit extends from the lower movable plate, it acts to approach the blade surface of the blade, the second When the second adjusting screw is turned and screwed into the second screw hole through the hole, the head of the second adjusting screw enters the second screw hole after passing through the second hole. Stops at the entrance of the fool hole and turns further to move the upper movable plate When the gap of the lower movable plate contracts in the vertical direction and the measurement unit extends from the upper movable plate, it acts so as to approach the blade surface of the blade, and when the measurement unit extends from the lower movable plate By acting away from the blade surface of the blade, the blade surface of the blade can be traced by combining both operations and bringing the blade surface of the blade into contact with at least the entire line pq.
In a preferred third embodiment of the preferred embodiment, the movable portion is configured such that the gap is formed by a radial notch introduced on a distal end side of a movable plate whose circumferential direction is disposed in the thickness direction and whose plate surface extends in the vertical direction. The upper movable piece and the lower movable piece are separated from each other, and (i) one of the upper movable piece and the lower movable piece is formed into a first through screw hole and a first through screw hole in the vertical direction. A first adjusting screw that is inserted toward the gap, and / or (ii) one of the upper movable piece and the lower movable piece is vertically moved at a position different from the first through screw hole in the radial direction. A second screw hole is provided in the direction and the other has a second screw hole communicating with the second screw hole, and is inserted into the second screw hole from the second screw hole toward the gap. An adjusting screw is provided, and the measuring section is It is a measuring part that extends downward from the moving piece and can contact at least the line pq with the blade surface of the blade. When the first adjustment screw is screwed into the first through screw hole, the first adjustment is performed. When the tip of the screw comes into contact with the other movable piece, it stops, and when further turned, the gap between the upper movable piece and the lower movable piece expands in the vertical direction so that the measurement unit approaches the blade surface of the blade, When the second adjustment screw is turned and screwed into the second screw hole through the second hole, the head of the second adjustment screw is inserted into the second screw hole after passing through the second hole. Stops at the entrance of the second hole, and when it is further turned, the gap between the upper movable piece and the lower movable piece contracts in the vertical direction so that the measuring unit moves away from the blade surface of the blade. At least the entire line pq is the wing surface of the blade. The blade surface of the blade can be traced by contact.
In a fourth preferred embodiment of the preferred embodiment, the movable portion is movable to the left with the gap in the circumferential direction by a radial cut introduced on the distal end side of a movable plate having a plate surface arranged in the circumferential direction. And (i) one of the left movable piece and the right movable piece is inserted into the first through screw hole in the left-right direction and into the first through screw hole toward the gap. And / or (ii) one of the left movable piece and the right movable piece in the left-right direction at a position different from the first through screw hole in the radial direction. And the other includes a second screw hole that communicates with the second hole, and a second adjustment screw that is inserted from the second hole toward the gap and can be inserted into the second hole. The measuring part is the left movable piece or the right possible in the radial direction. Extending downward from any one of the pieces, the blade makes contact with the blade surface of the blade at least at the line pq at a large or small angle in the range of 5 to 30 degrees from the vertical. When the first adjustment screw is turned and screwed into the first through screw hole, it stops when the tip of the first adjustment screw comes into contact with the other movable piece, and when further turned, the left movable piece and the right The gap of the movable piece expands in the circumferential direction, and the measuring unit acts so as to move the blade surface of the blade in the first circumferential direction, and passes through the second burr hole to the second screw hole to the second adjustment screw. When the screw is turned and screwed in, it passes through the second hole and enters the second screw hole and the head of the second adjustment screw stops at the entrance of the second screw hole. The gap of the right movable piece contracts in the circumferential direction, and the measuring unit is the blade The blade surface of the blade is moved in the second circumferential direction opposite to the first circumferential direction, and both blades are combined to bring the blade surface of the blade into contact with at least the entire line pq. Can be traced.
In a preferred first embodiment of the preferred aspect, preferably, the first through screw hole and the first adjustment screw are located at positions where the distance from the shaft may be different or the same in the circumferential direction of the movable portion. There are at least two sets, and there are at least two sets of the second burr hole, the second screw hole, and the second adjustment screw. In any one of the second to fourth preferred embodiments of the preferred embodiment, preferably, the first through screw hole and the first adjustment screw are located at positions where the distance from the shaft is different in the radial direction of the movable portion. There are at least two sets, and there are at least one set of the second burr hole, the second screw hole, and the second adjustment screw.
In the preferable aspect, the vertical direction of the connecting portion or the movable portion is preferably inclined in correspondence with the pitch angle of the propeller from the vertical direction of the shaft. Moreover, in the preferable aspect, preferably, a reinforcing material is provided at a contact portion of the upper movable piece or the lower movable piece, the left movable piece, or the right movable piece, which is the other, with which the tip of the first adjustment screw comes into contact. Place.

本発明の計測位置固定型のプロペラケージによれば、プロペラの羽根の翼面形状の計測や保存、修正作業を容易で確実にできる。   According to the propeller cage of the measurement position fixed type of the present invention, the measurement, storage, and correction of the blade surface shape of the propeller blades can be performed easily and reliably.

本発明のプロペラゲージの好ましい態様を示す。The preferable aspect of the propeller gauge of this invention is shown. プロペラにおける羽根の根元領域を示す。The blade root area of the propeller is shown. プロペラの展開図と、プロペラが1回転したときに翼の先端が描く円の半径Rとの関係を示す。The relationship between the developed view of the propeller and the radius R of the circle drawn by the tip of the wing when the propeller makes one revolution is shown. 本発明のプロペラゲージの好ましい態様をシャフト方向から示す。The preferable aspect of the propeller gauge of this invention is shown from a shaft direction. プロペラゲージの固定部がシャフトの上部から延びるとき、(A)計測される翼面と同じ翼面に配置される固定部の例、(B)計測される翼面とは別の翼面に配置される固定部の例を示す。When the fixed part of the propeller gauge extends from the upper part of the shaft, (A) an example of the fixed part arranged on the same blade surface as the measured blade surface, (B) arranged on a blade surface different from the measured blade surface The example of the fixing | fixed part made is shown. 本発明のプロペラゲージの第1の形態例を示す。The 1st example of a form of the propeller gauge of this invention is shown. 本発明の第1の形態例のプロペラゲージをシャフト方向から示す。The propeller gauge of the 1st example of this invention is shown from a shaft direction. 本発明のプロペラゲージの第1の形態例における、第1調整ねじ、第1貫通ねじ穴、第2調整ねじ、第2バカ穴及び第2ねじ穴を示す。The 1st adjustment screw, the 1st penetration screw hole, the 2nd adjustment screw, the 2nd burr hole, and the 2nd screw hole in the 1st form example of the propeller gauge of the present invention are shown. 本発明の第1の形態例のプロペラゲージをプロペラに設置した図である。It is the figure which installed the propeller gauge of the 1st form example of this invention in the propeller. 本発明のプロペラゲージの第2の形態例を示す。The 2nd example of a propeller gauge of the present invention is shown. 本発明のプロペラゲージの第2の形態例における、第1調整ねじ、第1貫通ねじ穴、第2調整ねじ、第2バカ穴及び第2ねじ穴を示す。The 1st adjustment screw, the 1st penetration screw hole, the 2nd adjustment screw, the 2nd burr hole, and the 2nd screw hole in the 2nd example of a propeller gauge of the present invention are shown. 本発明のプロペラゲージの第3の形態例を示す。The 3rd example of a propeller gauge of this invention is shown. 本発明のプロペラゲージの第3の形態例における、第1調整ねじ、第1貫通ねじ穴、第2調整ねじ、第2バカ穴及び第2ねじ穴を示す。The 1st adjustment screw, the 1st penetration screw hole, the 2nd adjustment screw, the 2nd burr hole, and the 2nd screw hole in the 3rd example of a propeller gauge of the present invention are shown. 本発明のプロペラゲージの第4の形態例を示す。The 4th example of a propeller gauge of the present invention is shown. 従来のプロペラゲージを示す。A conventional propeller gauge is shown.

本発明の計測位置固定型のプロペラゲージを図1の具体例に基づき説明する。
プロペラ100は羽根101とプロペラボス102を備え、プロペラボスの中空部にプロペラゲージのシャフト1の下部1bを挿入できる。通常は、ボートの後方から見たときにプロペラの回転方向は左回りとなるが、ボートが前進するときに、プロペラが水を切り始める側を前縁101a、水流がプロペラから離れる側を後縁101bという。プロペラボスの中空部の2つの開口端のどちらもプロペラゲージのシャフトを挿入可能であるが、プロペラシャフトが挿入される側にはシャーピン収納溝103と段差が存在するため、プロペラシャフトが挿入されない側にシャフト1の下部1bを挿入することが好ましい。プロペラゲージのプロペラボスの中空部に挿入される部分の長さは、プロペラゲージを保持できる長さであってプロペラボスからはみ出さない長さであればよい。好ましくは、図1に示すように、シャフト1の下部1bの径をプロペラボスの中空部の径よりも小さく、シャフト1の上部1aの径をプロペラボスの中空部の径よりも大きくして下部と上部に段差を設けると、段差の位置を調整することによりプロペラボスの中空部に挿入される部分の長さを容易に調整できる。
A fixed position measuring type propeller gauge of the present invention will be described based on a specific example of FIG.
The propeller 100 includes a blade 101 and a propeller boss 102, and a lower portion 1b of the shaft 1 of the propeller gauge can be inserted into a hollow portion of the propeller boss. Normally, when viewed from the rear of the boat, the propeller rotates counterclockwise, but when the boat advances, the front edge 101a is the side where the propeller begins to drain water, and the side where the water flow is away from the propeller is the rear edge 101b. The propeller gauge shaft can be inserted into either of the two open ends of the hollow part of the propeller boss, but the side where the propeller shaft is not inserted because there is a step with the shear pin housing groove 103 on the side where the propeller shaft is inserted. It is preferable to insert the lower part 1b of the shaft 1 into the shaft. The length of the portion inserted into the hollow portion of the propeller lab of the propeller gauge may be a length that can hold the propeller gauge and does not protrude from the propeller lab. Preferably, the diameter of the lower part 1b of the shaft 1 is smaller than the diameter of the hollow part of the propeller boss, and the diameter of the upper part 1a of the shaft 1 is larger than the diameter of the hollow part of the propeller boss as shown in FIG. If a step is provided in the upper part, the length of the portion inserted into the hollow portion of the propeller boss can be easily adjusted by adjusting the position of the step.

本発明によれば、プロペラゲージは、シャフト1と、シャフトの上部1aから径方向に延びる連結部2と、連結部2の径方向をシャフト側と先端側に分けると、先端側において下方に延び、プロペラの羽根の翼面と少なくとも線p−q(但し、pとqは線の両端)で接触可能な計測部3と、連結部のシャフト側又はシャフトの上部において下方に延び、プロペラボスから延びる羽根の根元領域で羽根の翼面と接触可能となる、回転可能なシャフトを固定する固定部4とを備える計測位置固定型のプロペラゲージが提供される。   According to the present invention, the propeller gauge extends downward on the tip side when the shaft 1, the connecting portion 2 extending in the radial direction from the upper portion 1a of the shaft, and the radial direction of the connecting portion 2 are divided into the shaft side and the tip side. , The measuring unit 3 that can contact the blade surface of the propeller blade at least on the line pq (where p and q are both ends of the line), and extend downward on the shaft side of the connecting part or on the upper part of the shaft. There is provided a propeller gauge of a fixed measurement position type including a fixing portion 4 for fixing a rotatable shaft, which can come into contact with the blade surface of the blade in the root region of the extending blade.

固定部は、図2に示すように、プロペラボスから延びる羽根の根元領域BAで羽根の翼面と接触させる。根元領域BAは一定の範囲を有するため、固定部の先端は尖っている必要はなく、根元領域BA内で接触し、固定できる形状であればよい。図2は、図1に示すプロペラゲージを用いて計測する翼面と同一の翼面上にある根元領域BAを示すが、計測する翼面と同一の翼面に限定されず、計測する翼面と異なる他の翼面上にある根元領域BAに固定部を接触させてもよい。計測しようとする翼面の位置がその翼面上の根元領域BAに近い場合に、他の翼面上にある根元領域BAに固定部を接触させることにより、固定部と計測部が密集することを避けることができる長所がある。
プロペラの前縁部分(前縁101a及びその周辺)並びに後縁部分(後縁101b及びその周辺)を除くと、羽根はプロペラボスから径方向に延びて根元を過ぎると薄くなり、ほぼ一定の厚さとなるが、プロペラボスに隣接する羽根の根元領域BAでは厚い。羽根の根元領域BAの形状は、プロペラのロット違いによって変動する可能性が殆んどなく、羽根の他の形状を木槌等で修正しても、その厚さにより影響を受けにくいため、計測部の位置を特定する基準点としては最適である。他の羽根部分よりも厚く、木槌等の影響を受けない、プロペラボスに隣接する羽根の根元領域BAは、木槌等で翼面形状を修正したことのある当業者ではあれば経験的に容易に理解できるものであるが、数値化することは容易ではない。
例えば、根元領域、プロペラボスに隣接し、プロペラの前縁部分及び後縁部分を除く、羽根の翼面の表面積全体の好ましくは20%以内に当たる、耳の形状に類似する形状の領域と言うことができる。換言すれば、1つの羽根の翼面の厚さの範囲において、厚さの上位20%以内に当たる、プロペラボスに隣接する領域と言うことができる。また、プロペラが1回転したときに翼の先端が描く円の半径をRとし、翼先端を1.0R、プロペラボスの中空部の中心軸を零とすると、図3に示すプロペラの展開図に基づき、根元領域BAは、好ましくは、プロペラボスに隣接する、0.3R以内の領域であって、プロペラの前縁101aから好ましくは15mm以上内側、プロペラの後縁101bから好ましくは10mm以上内側となる領域であると言うこともできる。これは、ボートレース用プロペラとして、0.3Rの最大翼厚は5.9mm、先端から0.1mmの位置での翼厚は0.7mm以上と記載する仕様例とも整合する。
厚い根元領域BAに固定部を設けることにより、木槌等による羽根翼面の修正の影響を受けにくくなり位置決めの基準が固定され、記憶した翼面のプロペラ上の位置と、再現しようとする翼面のプロペラ上の位置を同一とすることができ、再現の精度が高められる。
As shown in FIG. 2, the fixing portion is brought into contact with the blade surface of the blade in the blade root area BA extending from the propeller boss. Since the root area BA has a certain range, the tip of the fixing portion does not need to be sharp, and may be any shape that can be contacted and fixed in the root area BA. FIG. 2 shows a root area BA on the same blade surface as the blade surface measured using the propeller gauge shown in FIG. 1, but is not limited to the same blade surface as the blade surface to be measured, and the blade surface to be measured The fixed portion may be brought into contact with the root area BA on the other blade surface different from the above. When the position of the blade surface to be measured is close to the root area BA on the blade surface, the fixed section and the measurement section are gathered by bringing the fixed section into contact with the root area BA on the other blade surface. There are advantages that can be avoided.
Except for the front edge portion of the propeller (the front edge 101a and its surroundings) and the rear edge portion (the rear edge 101b and its surroundings), the blades extend radially from the propeller boss and become thin after passing through the root, and have a substantially constant thickness. However, it is thick in the root area BA of the blade adjacent to the propeller boss. The shape of the blade root area BA is unlikely to fluctuate depending on the lot of the propeller, and even if the other shape of the blade is modified with a mallet or the like, it is less affected by the thickness, so measurement It is optimal as a reference point for specifying the position of the part. The root area BA of the blade adjacent to the propeller boss, which is thicker than the other blade portions and not affected by the mallet, is empirically used by those skilled in the art who have modified the blade surface shape using the mallet. Although it can be easily understood, it is not easy to quantify it.
For example, the root region, adjacent to the propeller boss and excluding the front and rear edge portions of the propeller, preferably a region of a shape similar to the shape of the ear that preferably falls within 20% of the total surface area of the blade surface Can do. In other words, in the range of the thickness of the blade surface of one blade, it can be said that it is a region adjacent to the propeller boss that falls within the upper 20% of the thickness. Further, assuming that the radius of the circle drawn by the tip of the blade when the propeller makes one revolution is R, the tip of the blade is 1.0R, and the central axis of the hollow portion of the propeller is zero, the development view of the propeller shown in FIG. Based on this, the root area BA is preferably an area within 0.3R adjacent to the propeller boss, preferably 15 mm or more inside from the front edge 101a of the propeller, preferably 10 mm or more inside from the rear edge 101b of the propeller. It can also be said that this is an area. This is consistent with a specification example in which a maximum blade thickness of 0.3R is 5.9 mm and a blade thickness at a position of 0.1 mm from the tip is 0.7 mm or more as a boat race propeller.
By providing a fixed portion in the thick root area BA, the influence of the blade blade surface correction by the mallet or the like is less likely to be affected, the positioning reference is fixed, and the stored blade surface position on the propeller and the blade to be reproduced The position of the surface on the propeller can be made the same, and the reproduction accuracy is improved.

本明細書において、上下方向は、図1に示すように、シャフトをプロペラボスの中空部に挿入する方向を下方向、その反対を上方向と呼ぶ。また、図1に示すように、プロペラゲージをプロペラに設置したとき、プロペラゲージの計測部をプロペラの羽根の翼面に近づける方向を下方向と呼び、その反対を上方向と呼ぶ。プロペラゲージの計測部をプロペラの羽根の翼面に接触させるため、図4に示すように、連結部の上下方向とシャフトの上下方向のなす角度θを、プロペラのピッチ角と同じとすることが好ましい。この場合には、連結部の上下方向は、シャフトの上下方向からピッチ角だけ傾いているが、本明細書ではいずれも上下方向と呼ぶ。
本明細書において、径方向と周方向は、シャフト(軸)を中心にしてプロペラゲージを回転させて所望のプロペラの羽根の翼面上に移動させることを考慮して、シャフトを中心に円を描くとみなしてその半径が延びる方向を径方向と呼び、円周を描く方向を周方向と呼ぶ。
In the present specification, as shown in FIG. 1, in the vertical direction, the direction in which the shaft is inserted into the hollow portion of the propeller boss is referred to as the downward direction, and the opposite is referred to as the upward direction. As shown in FIG. 1, when the propeller gauge is installed on the propeller, the direction in which the measuring unit of the propeller gauge is brought closer to the blade surface of the propeller blade is referred to as the downward direction, and the opposite is referred to as the upward direction. In order to bring the propeller gauge measuring section into contact with the blade surface of the propeller blade, as shown in FIG. 4, the angle θ 1 formed by the vertical direction of the connecting section and the vertical direction of the shaft should be the same as the pitch angle of the propeller. Is preferred. In this case, although the vertical direction of the connecting portion is inclined by a pitch angle from the vertical direction of the shaft, both are referred to as the vertical direction in this specification.
In this specification, the radial direction and the circumferential direction are determined by rotating the propeller gauge around the shaft (axis) and moving it on the blade surface of the blade of the desired propeller. A direction in which the radius extends is called a radial direction, and a direction in which the circumference is drawn is called a circumferential direction.

固定部は、連結部のシャフト側から下方に延び、又はシャフトの上部において下方に延び、プロペラボスから延びる羽根の根元領域で羽根の翼面と接触可能となる。図1の固定部4は、プロペラゲージの固定部が連結部のシャフト側から下方に延びる例である。図5は、プロペラゲージの固定部がシャフトの上部から延びるとき、(A)計測される翼面と同じ翼面に配置される固定部の例、(B)計測される翼面とは別の翼面に配置される固定部の例を示す。
固定部は、連結部のシャフト側と、シャフトの上部とのいずれから延びてもよいが、取り付けが容易さの点からは前者が好ましいが、連結部が短いときや、計測する翼面と異なる他の翼面上にある根元領域BAに固定部を接触させるときには後者が好ましい。
The fixing portion extends downward from the shaft side of the connecting portion, or extends downward at the upper portion of the shaft, and can come into contact with the blade surface of the blade in the root region of the blade extending from the propeller boss. The fixing portion 4 in FIG. 1 is an example in which the fixing portion of the propeller gauge extends downward from the shaft side of the connecting portion. FIG. 5 shows an example of a fixed portion arranged on the same blade surface as the measured blade surface when the fixed portion of the propeller gauge extends from the upper part of the shaft, and (B) different from the measured blade surface. The example of the fixing | fixed part arrange | positioned at a blade surface is shown.
The fixing part may extend from either the shaft side of the connecting part or the upper part of the shaft, but the former is preferable from the viewpoint of ease of attachment, but when the connecting part is short or different from the blade surface to be measured The latter is preferred when the fixed part is brought into contact with the root area BA on the other blade surface.

計測部は、連結部の先端側において下方に延び、プロペラの羽根の翼面と少なくとも線p−q(但し、pとqは線の両端)で接触できる形状であればよい。「少なくとも線p−q」は、線p−qが厚さを有し、面として翼面に接してもよいことを意味するが、厚くなると面が大きくなり、面全体を翼面に接触させることが困難になるため、計測部は、接触する部分の厚さを薄くしたものが好ましい。
プロペラゲージは、プロペラの羽根の翼面を線p−qで計測して記憶するため、1つのプロペラゲージが1つの計測部を備えるときは、プロペラゲージの個数は、プロペラの羽根の翼面の計測箇所数と同じである。プロペラの羽根の翼面の計測箇所数は、多いほど正確な形状の再現が可能となるが、煩雑になるため、好ましくは10〜20か所である。具体的な箇所は、各競艇選手がプロペラの推進力への影響が大きく、計測又は記憶する価値が高いと考える箇所を選択すればよく、個人差が生じる。
シャフトからの距離が異なり、計測方向の異なる計測部を有するプロペラゲージを使い分けることにより、プロペラの羽根の翼面を多数の線p−qで特定することができる。線p−qの長さは同じである必要はなく、計測箇所の翼面の形状に応じて長くしたり短くしたりできる。
プロペラゲージの大きさは、計測部の線p−qの長さに応じて選択することができ、計測部が短ければプロペラゲージ自体も小さくすることができ、計測部が長ければプロペラゲージ自体も大きくなる傾向がある。また、プロペラゲージは、周方向又は径方向に2つ以上の計測部を備えてもよい。
The measurement part should just be the shape which extends below in the front end side of a connection part, and can contact with the wing | blade surface of the blade | wing of a propeller at least with the line pq (however, p and q are the both ends of a line). “At least line pq” means that the line pq has a thickness and may contact the blade surface as a surface, but as the surface becomes thicker, the surface becomes larger and the entire surface is brought into contact with the blade surface. Therefore, it is preferable that the measurement unit has a reduced thickness at the contact portion.
Since the propeller gauge measures and stores the blade surface of the propeller blade with the line pq, when one propeller gauge has one measuring unit, the number of the propeller gauge is the number of the blade surface of the propeller blade. It is the same as the number of measurement points. The more the number of measurement points on the blade surface of the propeller blade, the more accurate the shape can be reproduced. However, the number of measurement points is preferably 10 to 20 because it becomes complicated. The specific location may be selected as a location where each boat racer has a great influence on the propeller propulsive force and is considered to be highly measurable or memorized, resulting in individual differences.
By properly using propeller gauges having different measurement units with different distances from the shaft, the blade surfaces of the propeller blades can be identified by a number of lines pq. The lengths of the lines p-q do not have to be the same, and can be increased or decreased according to the shape of the blade surface at the measurement location.
The size of the propeller gauge can be selected according to the length of the line pq of the measuring unit. If the measuring unit is short, the propeller gauge itself can be reduced, and if the measuring unit is long, the propeller gauge itself is also selected. There is a tendency to grow. The propeller gauge may include two or more measurement units in the circumferential direction or the radial direction.

シャフト、連結部、計測部及び固定部を備えるプロペラケージの材質は、後述するように連結部を可動部として使用する場合以外は特に限定されないが、加工の容易さ及び接着剤等を用いる接着の容易さの点において好ましくはプラスチックである。
計測部は、やすり等により削って調整できる点において好ましくはプラスチックを用いるとよく、少なくとも線p−qで接触していることの確認が容易になる点において、好ましくは透明度の高いプラスチックを用いるとよい。透明度の高いプラスチックとしては、アクリル酸エステル又はメタクリル酸エステルの重合体であるアクリル樹脂(特に好ましくはポリメチルメタクリレート(PMMA))、ポリカーボネート(PC)、ポリ塩化ビニル(PVC)、ポリエチレンテレフタレート(PET)等が挙げられる。また、プロペラケージをデータ化して3Dプリンターによりいつでも同じ形状のものを作ることも可能となる点においてABS樹脂、PLA樹脂等も挙げられる。
シャフト、連結部(可動部)、計測部及び固定部を備えるプロペラケージは、一体的に成形して得ることも可能であるが、シャフト、連結部(可動部)、計測部及び固定部のうちのいずれか又は全部を、接着剤を用いて接着しても、融着してもよい。
The material of the propeller cage including the shaft, the connecting portion, the measuring portion, and the fixing portion is not particularly limited except when the connecting portion is used as a movable portion as will be described later. In terms of ease, plastic is preferable.
The measuring unit is preferably made of plastic in that it can be cut and adjusted with a file or the like, and at least in terms of easy confirmation of contact with the line pq, it is preferable to use plastic with high transparency. Good. As a highly transparent plastic, acrylic resin (particularly preferably polymethyl methacrylate (PMMA)), polycarbonate (PC), polyvinyl chloride (PVC), polyethylene terephthalate (PET) which is a polymer of acrylic ester or methacrylic ester. Etc. Moreover, ABS resin, PLA resin, etc. are mentioned at the point which can make a propeller cage into data and can always make the same shape with a 3D printer.
A propeller cage including a shaft, a connecting part (movable part), a measuring part and a fixed part can be obtained by integrally molding, but among the shaft, connecting part (movable part), measuring part and fixed part, Any or all of these may be adhered using an adhesive or may be fused.

本発明の計測位置固定型のプロペラゲージの好ましい態様では、連結部2は、シャフト側において不動であり、先端側において径方向に延びるギャップを挟んで上下可動片又は周方向の左右可動片に分岐され、上下可動片の少なくとも一方又は左右可動片の少なくとも一方に設けた調整ねじでギャップの間隔を収縮又は拡張させることにより上下方向又は左右方向に動かすことができる可撓性の可動部2であり、計測部3は、上もしくは下可動片から、又は右もしくは左可動片から下方に延び、プロペラの羽根の翼面と少なくとも線p−qで接触可能であり、可動部2の先端側を上下方向又は左右方向に動かすことにより、計測部3が少なくとも線p−qの全体を羽根の翼面を接触させて羽根の翼面をなぞることができる。
本発明の計測位置固定型のプロペラゲージの好ましい態様には、好ましい第1〜4の形態例が挙げられる。本発明によるプロペラゲージを、まず、第1〜4の形態例を挙げて説明する。本発明はこれらの形態例に限らず、他の多くの形態を取り得ることができることは当業者に容易に理解できる。そこで、第1〜4の形態例の説明後、さらに本発明を総括的に説明する。
In a preferred aspect of the measurement position fixed type propeller gauge according to the present invention, the connecting portion 2 is stationary on the shaft side and branches into a vertically movable piece or a circumferentially movable left and right piece with a gap extending in the radial direction on the tip side. A flexible movable part 2 that can be moved in the vertical direction or the horizontal direction by contracting or expanding the gap interval with an adjustment screw provided on at least one of the vertical movable pieces or at least one of the left and right movable pieces. The measuring unit 3 extends downward from the upper or lower movable piece or from the right or left movable piece, and can contact the blade surface of the propeller blade at least on the line pq. By moving in the direction or the left-right direction, the measuring unit 3 can trace the blade surface of the blade by bringing the blade surface of the blade into contact with at least the entire line pq.
Preferred embodiments of the fixed position measuring type propeller gauge of the present invention include preferred first to fourth embodiments. First, the propeller gauge according to the present invention will be described with reference to first to fourth embodiments. It is easily understood by those skilled in the art that the present invention is not limited to these embodiments and can take many other forms. Therefore, after the description of the first to fourth embodiments, the present invention will be further explained.

本発明によるプロペラゲージの第1の形態例であるプロペラゲージ10を図6〜9に基づき説明する。
プロペラゲージ10は、プロペラのプロペラボスの中空部に下部11bを挿入できるシャフト11と、シャフト11の上部11aから径方向に延びる可撓性の連結部(可動部)12と、可動部12の径方向をシャフト側と先端側に分けると、先端側において下方に延び、プロペラの羽根の翼面と少なくとも線p−qで接触可能な計測部13と、可動部12の不動であるシャフト側又はシャフトの上部において下方に延び、プロペラボスから延びる羽根の根元領域BAで羽根の翼面と接触可能となる、シャフト11を回転しないように固定する固定部14とを備える。
可動部12の先端側は、径方向に延びるギャップGを挟んで上可動片12a及び下可動片12bに分岐される。好ましくは、図6に示すように、シャフト側に配置されたスペーサ12sを介してギャップGを隔てて上可動板12aの板面と下可動板12bの板面を上下方向に重ねて構成してもよい。
計測部13は、上可動板12aもしくは下可動板12bの先端側における周方向の一端から下方に延び、羽根の翼面と少なくとも線p−qで接触できるように好ましくは接触する部分の厚さを薄くしている。上可動片12a及び下可動片12bの少なくとも一方に設けた調整ねじでギャップGの間隔を収縮又は拡張させると、計測部13を上下方向に動かすことができ、少なくとも線p−qの全体を羽根の翼面に接触させて羽根の翼面をなぞることができる。
A propeller gauge 10 which is a first embodiment of a propeller gauge according to the present invention will be described with reference to FIGS.
The propeller gauge 10 includes a shaft 11 in which a lower portion 11b can be inserted into a hollow portion of a propeller of a propeller, a flexible connecting portion (movable portion) 12 extending in a radial direction from the upper portion 11a of the shaft 11, and a diameter of the movable portion 12. When the direction is divided into the shaft side and the tip side, the measuring unit 13 that extends downward on the tip side and can contact with the blade surface of the blade of the propeller at least by the line pq, and the shaft side or the shaft where the movable unit 12 is immovable And a fixing portion 14 for fixing the shaft 11 so as not to rotate. The fixing portion 14 extends downward from the upper portion of the blade and can come into contact with the blade surface of the blade in the blade root area BA extending from the propeller boss.
The distal end side of the movable portion 12 is branched into an upper movable piece 12a and a lower movable piece 12b with a gap G extending in the radial direction interposed therebetween. Preferably, as shown in FIG. 6, the plate surface of the upper movable plate 12a and the plate surface of the lower movable plate 12b are vertically stacked with a gap G interposed via a spacer 12s disposed on the shaft side. Also good.
The measuring part 13 extends downward from one end in the circumferential direction on the distal end side of the upper movable plate 12a or the lower movable plate 12b, and preferably has a thickness at a portion in contact with the blade surface of the blade at least on line pq. Is thinning. When the gap G is contracted or expanded with an adjusting screw provided on at least one of the upper movable piece 12a and the lower movable piece 12b, the measuring unit 13 can be moved in the vertical direction, and at least the entire line pq is moved to the blade. The blade surface of the blade can be traced in contact with the blade surface.

プロペラゲージの計測部をプロペラの羽根の翼面に接触させるため、図7に示すように、計測部の上下方向は、シャフトの上下方向からプロペラのピッチ角θだけ傾けることが好ましい。   In order to bring the propeller gauge measuring section into contact with the blade surface of the propeller blade, the vertical direction of the measuring section is preferably inclined by the propeller pitch angle θ from the vertical direction of the shaft, as shown in FIG.

図8に示すように、上可動板12aと下可動板12bのいずれか一方は、上下方向にギャップGに向かう第1貫通ねじ穴16aと、第1貫通ねじ穴16aにギャップGに向けて挿入される第1調整ねじ15aを備え、第1貫通ねじ穴16aとはシャフト11からの距離が異なっても同じでもよい周方向の異なる位置に上可動板12aと下可動板12bのいずれか一方が上下方向にギャップGに向けて第2バカ穴18aを備えるとともに他方が第2バカ穴18aに連通する第2ねじ穴19aを備え、さらに第2バカ穴18aからギャップGに向けて挿入され第2ねじ穴19aに挿入できる第2調整ねじ17aを備える。
図8は、3つの第1調整ねじ15a〜cとこれらに対応する3つの第1貫通ねじ穴16a〜cに加えて、2つの第2調整ねじ17a〜bと対応する2組の第2バカ穴18a〜bと第2ねじ穴19a〜bを示すが、第1調整ねじと第2調整ねじの数は、羽根の翼面の形状及び当該形状を記憶する精度に応じて選択できる。羽根の翼面上を多くの箇所で記憶するために、多くのプロペラゲージを用いるため、各プロペラゲージは、好ましくは、少なくとも1つの第1調整ねじ及び少なくとも1つの第2調整ねじ、これに対応する少なくとも1つの第1貫通ねじ穴及び少なくとも1組の第2バカ穴と第2ねじ穴を備えればよい。
As shown in FIG. 8, one of the upper movable plate 12a and the lower movable plate 12b is inserted into the first through screw hole 16a toward the gap G in the vertical direction and into the first through screw hole 16a toward the gap G. The first movable screw 12a and the lower movable plate 12b are located at different positions in the circumferential direction that may be the same as or different from the first through screw hole 16a. A second burr hole 18a is provided in the vertical direction toward the gap G, and the other is provided with a second screw hole 19a communicating with the second burr hole 18a. Further, the second burr hole 18a is inserted into the gap G from the second burr hole 18a. A second adjustment screw 17a that can be inserted into the screw hole 19a is provided.
FIG. 8 shows two sets of second baffles corresponding to two second adjustment screws 17a-b in addition to the three first adjustment screws 15a-c and the corresponding three first through screw holes 16a-c. Although the holes 18a-b and the second screw holes 19a-b are shown, the numbers of the first adjustment screw and the second adjustment screw can be selected according to the shape of the blade surface of the blade and the accuracy of storing the shape. Since many propeller gauges are used to memorize the blade surface on many points, each propeller gauge preferably corresponds to at least one first adjustment screw and at least one second adjustment screw. It suffices to have at least one first through screw hole and at least one set of second fool hole and second screw hole.

プロペラゲージ10を、図9に示すように、プロペラ100に設置して羽根101の翼面の形状を計測することができる。
プロペラゲージ10をプロペラ100に設置し、羽根101の翼面に固定部14の下方を接触させる。羽根101の翼面に固定部14の下方を接触させた後、計測部13の下方を羽根101の翼面に接触させ、線p−qの全体が羽根の翼面を接触するように調整ねじを用いて調整する。
第1貫通ねじ穴16a,16b,16cに第1調整ねじ15a,15b,15cを回してねじ込むと、第1調整ねじ15a,15b,15cの先端が他方の可動板と接触すると止まり、さらに回すと上可動板12aと下可動板12bのギャップGが上下方向に拡張して、計測部13が上可動板12aから延びるときは羽根の翼面から遠ざかるように作用し、計測部13が下可動板12bから延びるときは羽根の翼面に近づくように作用する。図8に示すように、第1調整ねじ15a,15b,15cの先端が接触する他方の可動板には、調整ねじとの繰り返しの接触により他方の可動板が摩耗することを防止するため、耐摩耗性の高い補強材RMを設置すると良い。
また、第2バカ穴18a,18bを経て第2ねじ穴19a,19bに第2調整ねじ17a,17bを回してねじ込むと、第2バカ穴18a,18bを通過後第2ねじ穴19a,19bに侵入して第2調整ねじ17a,17bの頭部が第2バカ穴18a,18bの入口で止まり、さらに回すと上可動板12aと下可動板12bのギャップGが上下方向に収縮し、計測部13が上可動板12aから延びるときは羽根の翼面に近づくように作用し、計測部13が下可動板12bから延びるときは羽根の翼面に遠ざかるように作用する。第2バカ穴18a,18bに連通する第2ねじ穴19a,19bは、貫通するねじ穴でも、貫通しないねじ穴でもよいが、貫通しないねじ穴を用いるときは、第2調整ねじ17a,17bが最大限に挿入された場合でも収納できる深さであることが好ましく、製造上の容易さの点において貫通するねじ穴が好ましい。また、第2バカ穴18a,18bは、第2調整ねじ17a,17bの径よりやや大きい「バカ穴」であり、バカ穴とすることにより第2調整ねじ17a,17bと第2ねじ穴19a,19bでギャップGの収縮を行うことができる。バカ穴は、ねじよりも径が大きいためねじ切りが不要であり、通常はねじのない穴である。
第1調整ねじ15a,15b,15cによる調整及び第2調整ねじ17a,17bによる調整を組み合わせることにより、少なくとも線p−qの全体を羽根の翼面を接触させて羽根の翼面をなぞることが可能となる。
As shown in FIG. 9, the propeller gauge 10 can be installed on the propeller 100 to measure the shape of the blade surface of the blade 101.
The propeller gauge 10 is installed on the propeller 100 and the lower surface of the fixed portion 14 is brought into contact with the blade surface of the blade 101. After the lower part of the fixed part 14 is brought into contact with the blade surface of the blade 101, the lower part of the measuring unit 13 is brought into contact with the blade surface of the blade 101, and the adjustment screw is brought into contact with the blade surface of the blade. Use to adjust.
When the first adjustment screw 15a, 15b, 15c is turned and screwed into the first through screw hole 16a, 16b, 16c, it stops when the tip of the first adjustment screw 15a, 15b, 15c comes into contact with the other movable plate. When the gap G between the upper movable plate 12a and the lower movable plate 12b expands in the vertical direction, and the measuring unit 13 extends from the upper movable plate 12a, the measuring unit 13 acts away from the blade surface of the blade. When extending from 12b, it acts to approach the blade surface of the blade. As shown in FIG. 8, the other movable plate with which the tips of the first adjustment screws 15a, 15b, and 15c are in contact with each other is prevented from being worn by repeated contact with the adjustment screw. A highly wearable reinforcing material RM may be installed.
Further, when the second adjusting screws 17a and 17b are screwed into the second screw holes 19a and 19b through the second hole 18a and 18b, the second screw holes 19a and 19b are passed through the second hole 18a and 18b and then passed through the second screw holes 19a and 19b. The heads of the second adjusting screws 17a and 17b stop at the entrances of the second burr holes 18a and 18b, and when further rotated, the gap G between the upper movable plate 12a and the lower movable plate 12b contracts in the vertical direction. When 13 extends from the upper movable plate 12a, it acts to approach the blade surface of the blade, and when the measuring unit 13 extends from the lower movable plate 12b, it acts to move away from the blade surface of the blade. The second screw holes 19a, 19b communicating with the second fool holes 18a, 18b may be threaded holes that do not penetrate or screw holes that do not penetrate, but when using screw holes that do not penetrate, the second adjustment screws 17a, 17b The depth is preferably such that it can be accommodated even when inserted to the maximum, and a threaded hole that penetrates is preferable in terms of ease of manufacturing. Further, the second flaw holes 18a and 18b are “buck holes” that are slightly larger than the diameters of the second adjustment screws 17a and 17b, and the second adjustment screws 17a and 17b and the second screw holes 19a and 19b are formed as fool holes. The gap G can be contracted at 19b. Since the diameter of the hole is larger than that of the screw, the screw hole is not required and is usually a hole without a screw.
By combining the adjustment by the first adjustment screws 15a, 15b, and 15c and the adjustment by the second adjustment screws 17a and 17b, at least the entire line pq can be brought into contact with the blade surface of the blade to trace the blade surface of the blade. It becomes possible.

本発明によるプロペラゲージの第2の形態例であるプロペラゲージ20を図10〜11に基づき説明する。
プロペラケージ20は、プロペラのプロペラボスの中空部に下部21bを挿入できるシャフト21と、シャフト21の上部21aから径方向に延びる可撓性の連結部(可動部)22と、可動部22の径方向をシャフト側と先端側に分けると、先端側において下方に延び、プロペラの羽根の翼面と少なくとも線p−qで接触可能な計測部23と、可動部22の不動であるシャフト側又はシャフトの上部において下方に延び、プロペラボスから延びる羽根の根元領域BAで羽根の翼面と接触可能となる、シャフト21を回転しないように固定する固定部24とを備える。
可動部22の先端側は、径方向に延びるギャップGを挟んで上可動片22a及び下可動片22bに分岐される。好ましくは、図10に示すように、シャフト側に配置されたスペーサ22sを介してギャップGを隔てて上可動板22aの板面と下可動板22bの板面を上下方向に重ねて構成してよい。
計測部23は、径方向で上可動板22aもしくは下可動板22bから下方に延び、羽根の翼面と少なくとも線p−qで接触できるように好ましくは接触する部分の厚さを薄くしている。上可動片22a及び下可動片22bの少なくとも一方に設けた調整ねじでギャップGの間隔を収縮又は拡張させると、計測部23を上下方向に動かすことができ、少なくとも線p−qの全体を羽根の翼面に接触させて羽根の翼面をなぞることができる。
A propeller gauge 20 as a second embodiment of the propeller gauge according to the present invention will be described with reference to FIGS.
The propeller cage 20 includes a shaft 21 into which a lower portion 21b can be inserted into a hollow portion of a propeller boss of the propeller, a flexible connecting portion (movable portion) 22 extending in a radial direction from the upper portion 21a of the shaft 21, and a diameter of the movable portion 22. When the direction is divided into the shaft side and the tip side, the measuring unit 23 that extends downward on the tip side and can contact at least the line pq with the blade surface of the blade of the propeller, and the shaft side or the shaft where the movable unit 22 is stationary And a fixing portion 24 for fixing the shaft 21 so as not to rotate. The fixing portion 24 can be brought into contact with the blade surface of the blade in the root region BA of the blade extending from the propeller boss.
The distal end side of the movable portion 22 is branched into an upper movable piece 22a and a lower movable piece 22b with a gap G extending in the radial direction interposed therebetween. Preferably, as shown in FIG. 10, the plate surface of the upper movable plate 22a and the plate surface of the lower movable plate 22b are vertically stacked with a gap G interposed via a spacer 22s disposed on the shaft side. Good.
The measuring unit 23 extends downward from the upper movable plate 22a or the lower movable plate 22b in the radial direction, and preferably has a reduced thickness at a portion in contact with the blade surface of the blade at least on the line pq. . When the gap G is contracted or expanded with an adjusting screw provided on at least one of the upper movable piece 22a and the lower movable piece 22b, the measuring unit 23 can be moved in the vertical direction, and at least the entire line pq is moved to the blade. The blade surface of the blade can be traced in contact with the blade surface.

計測部23を取り除いた図11に示すように、上可動板22aと下可動板22bのいずれか一方は、上下方向にギャップGに向かう第1貫通ねじ穴26aと、第1貫通ねじ穴26aにギャップGに向けて挿入される第1調整ねじ25aを備え、第1貫通ねじ穴26aとはシャフト21からの距離が異なる、径方向の異なる位置に上可動板22aと下可動板22bのいずれか一方が上下方向にギャップGに向けて第2バカ穴28を備えるとともに他方が第2バカ穴28に連通する第2ねじ穴29を備え、さらに第2バカ穴28からギャップGに向けて挿入され第2ねじ穴29に挿入できる第2調整ねじ27を備える。
図11は、2つの第1調整ねじ25a〜bとこれらに対応する2つの第1貫通ねじ穴26a〜bに加えて、1つの第2調整ねじ27と対応する1組の第2バカ穴28と第2ねじ穴29を示すが、第1調整ねじと第2調整ねじの数は、羽根の翼面の形状及び当該形状を記憶する精度に応じて選択できる。羽根の翼面上を多くの箇所で記憶するために、多くのプロペラゲージを用いるため、各プロペラゲージは、好ましくは、少なくとも1つの第1調整ねじ及び少なくとも1つの第2調整ねじ、これに対応する少なくとも1つの第1貫通ねじ穴及び少なくとも1組の第2バカ穴と第2ねじ穴を備えればよい。
As shown in FIG. 11 with the measurement unit 23 removed, one of the upper movable plate 22a and the lower movable plate 22b has a first through screw hole 26a and a first through screw hole 26a extending in the vertical direction toward the gap G. The first adjustment screw 25a inserted toward the gap G is provided, the distance from the shaft 21 is different from the first through screw hole 26a, and either the upper movable plate 22a or the lower movable plate 22b at a different radial direction. One is provided with a second burr hole 28 in the vertical direction toward the gap G and the other is provided with a second screw hole 29 communicating with the second burr hole 28, and is further inserted from the second burr hole 28 toward the gap G. A second adjustment screw 27 that can be inserted into the second screw hole 29 is provided.
FIG. 11 shows a pair of second burr holes 28 corresponding to one second adjustment screw 27 in addition to the two first adjustment screws 25a-b and the two first through screw holes 26a-b corresponding thereto. The number of the first adjustment screw and the second adjustment screw can be selected according to the shape of the blade surface of the blade and the accuracy of storing the shape. Since many propeller gauges are used to memorize the blade surface on many points, each propeller gauge preferably corresponds to at least one first adjustment screw and at least one second adjustment screw. It suffices to have at least one first through screw hole and at least one set of second fool hole and second screw hole.

プロペラゲージ20をプロペラ100に設置し、羽根101の翼面に固定部24の下方を接触させる。羽根101の翼面に固定部24の下方を接触させた後、計測部23の下方を羽根101の翼面に接触させ、線p−qの全体が羽根の翼面を接触するように調整ねじを用いて調整する。
第1貫通ねじ穴26a,26bに第1調整ねじ25a,25bを回してねじ込むと、第1調整ねじ25a,25bの先端が他方の可動板と接触すると止まり、さらに回すと上可動板22aと下可動板22bのギャップGが上下方向に拡張して、計測部23が上可動板22aから延びるときは羽根の翼面から遠ざかるように作用し、計測部23が下可動板22bから延びるときは羽根の翼面に近づくように作用する。第1調整ねじ25a,25bの先端が接触する他方の可動板には、調整ねじとの繰り返しの接触により他方の可動板が摩耗することを防止するため、耐摩耗性の高い補強材RMを設置すると良い。
また、第2バカ穴28を経て第2ねじ穴29に第2調整ねじ27を回してねじ込むと、第2バカ穴28を通過後第2ねじ穴29に侵入して第2調整ねじ27の頭部が第2バカ穴28の入口で止まり、さらに回すと上可動板22aと下可動板22bのギャップGが上下方向に収縮して、計測部23が上可動板22aから延びるときは羽根の翼面に近づくように作用し、計測部23が下可動板22bから延びるときは羽根の翼面から遠ざかるように作用する。第2バカ穴28に連通する第2ねじ穴29は、貫通するねじ穴でも、貫通しないねじ穴でもよいが、貫通しないねじ穴を用いるときは、第2調整ねじ27が最大限に挿入された場合でも収納できる深さであることが好ましく、製造上の容易さの点において貫通するねじ穴が好ましい。また、第2バカ穴28は、第2調整ねじ27の径よりやや大きい「バカ穴」であり、バカ穴とすることにより第2調整ねじ27と第2ねじ穴29でギャップGの収縮を行うことができる。
第1調整ねじ25a,25bによる調整及び第2調整ねじ27による調整を組み合わせることにより、少なくとも線p−qの全体を前記羽根の翼面を接触させて前記羽根の翼面をなぞることが可能となる。
The propeller gauge 20 is installed on the propeller 100 and the lower surface of the fixed portion 24 is brought into contact with the blade surface of the blade 101. After the lower part of the fixed part 24 is brought into contact with the blade surface of the blade 101, the lower part of the measuring unit 23 is brought into contact with the blade surface of the blade 101, and the adjustment screw is set so that the entire line pq contacts the blade surface of the blade. Use to adjust.
When the first adjustment screws 25a and 25b are turned and screwed into the first through screw holes 26a and 26b, the tip ends of the first adjustment screws 25a and 25b come into contact with the other movable plate, and when further turned, the upper movable plate 22a and the lower When the gap G of the movable plate 22b expands in the vertical direction so that the measuring unit 23 extends from the upper movable plate 22a, the movable plate 22b acts away from the blade surface of the blade, and when the measuring unit 23 extends from the lower movable plate 22b, the blade It works to get closer to the wing surface. In order to prevent the other movable plate from being worn by repeated contact with the adjustment screw, the other adjustment plate RM having high wear resistance is installed on the other movable plate where the tips of the first adjustment screws 25a and 25b come into contact. Good.
Further, when the second adjustment screw 27 is turned and screwed into the second screw hole 29 through the second burr hole 28, the second adjustment screw 27 enters the second screw hole 29 after passing through the second burr hole 28. The portion stops at the entrance of the second hole 28, and when further rotated, the gap G between the upper movable plate 22a and the lower movable plate 22b contracts in the vertical direction, and when the measuring unit 23 extends from the upper movable plate 22a, the blade blade When the measuring unit 23 extends from the lower movable plate 22b, it acts to move away from the blade surface of the blade. The second screw hole 29 communicating with the second fool hole 28 may be a screw hole that penetrates or a screw hole that does not penetrate, but when the screw hole that does not penetrate is used, the second adjustment screw 27 is inserted to the maximum extent. Even in such a case, it is preferable to have a depth that can be accommodated, and a threaded hole that penetrates in terms of ease of manufacturing is preferable. In addition, the second baffle hole 28 is a “burst hole” that is slightly larger than the diameter of the second adjustment screw 27, and the gap G is contracted by the second adjustment screw 27 and the second screw hole 29 by being a fool hole. be able to.
By combining the adjustment by the first adjustment screws 25a and 25b and the adjustment by the second adjustment screw 27, it is possible to trace the blade surface of the blade by bringing at least the entire line pq into contact with the blade surface of the blade. Become.

本発明によるプロペラゲージの第3の形態例であるプロペラゲージ30を図12〜13に基づき説明する。
プロペラゲージ30は、プロペラのプロペラボスの中空部に下部31bを挿入できるシャフト31と、シャフト31の上部31aから径方向に延びる可撓性の連結部(可動部)32と、可動部32の径方向をシャフト側と先端側に分けると、先端側において下方に延び、プロペラの羽根の翼面と少なくとも線p−qで接触可能な計測部33と、可動部32の不動であるシャフト側又はシャフトの上部において下方に延び、プロペラボスから延びる羽根の根元領域BAで羽根の翼面と接触可能となる、シャフト31を回転しないように固定する固定部34とを備える。
可動部32の先端側は、径方向に延びるギャップGを挟んで上可動片32a及び下可動片32bに分岐される。好ましくは、図12に示すように、厚さ方向を周方向に配置して板面が上下方向に延びる可動板32の先端側に導入された径方向の切込みによりギャップGを隔てて上可動片32aと下可動片32bに分岐してもよい。
計測部33は、上可動片32a及び下可動片32bのいずれか一方から下方に延び、羽根の翼面と少なくとも線p−qで接触できるように好ましくは接触する部分の厚さを薄くしている。上可動片32a及び下可動片32bの少なくとも一方に設けた調整ねじでギャップGの間隔を収縮又は拡張させると、計測部33を上下方向に動かすことができ、少なくとも線p−qの全体を羽根の翼面に接触させて羽根の翼面をなぞることができる。
A propeller gauge 30 as a third embodiment of the propeller gauge according to the present invention will be described with reference to FIGS.
The propeller gauge 30 includes a shaft 31 into which a lower portion 31b can be inserted into a hollow portion of a propeller boss of the propeller, a flexible connecting portion (movable portion) 32 extending in a radial direction from the upper portion 31a of the shaft 31, and a diameter of the movable portion 32. When the direction is divided into the shaft side and the tip side, the measuring unit 33 that extends downward on the tip side and can contact with the blade surface of the blade of the propeller at least on the line pq, and the shaft side or the shaft where the movable unit 32 is immovable And a fixing portion 34 for fixing the shaft 31 so as not to rotate. The fixing portion 34 can be brought into contact with the blade surface of the blade at a root region BA of the blade extending from the propeller boss.
The distal end side of the movable portion 32 is branched into an upper movable piece 32a and a lower movable piece 32b with a gap G extending in the radial direction interposed therebetween. Preferably, as shown in FIG. 12, the upper movable piece is separated from the gap G by a radial cut introduced on the distal end side of the movable plate 32 whose thickness direction is arranged in the circumferential direction and the plate surface extends in the vertical direction. You may branch to 32a and the lower movable piece 32b.
The measurement unit 33 extends downward from one of the upper movable piece 32a and the lower movable piece 32b, and preferably has a reduced thickness at a portion that is in contact with the blade surface of the blade at least on the line pq. Yes. When the gap G is contracted or expanded with an adjustment screw provided on at least one of the upper movable piece 32a and the lower movable piece 32b, the measuring unit 33 can be moved in the vertical direction, and at least the entire line pq is moved to the blade. The blade surface of the blade can be traced in contact with the blade surface.

図13に示すように、上可動片32aと下可動片32bのいずれか一方は、上下方向にギャップGに向かう第1貫通ねじ穴36a,36bと、第1貫通ねじ穴36a,36bにギャップGに向けて挿入される第1調整ねじ35a,35bを備え、第1貫通ねじ穴36a,36bとは径方向の異なる位置に上可動片32aと下可動片32bのいずれか一方が上下方向にギャップGに向けて第2バカ穴38を備えるとともに他方が第2バカ穴38に連通する第2ねじ穴39を備え、さらに第2バカ穴38からギャップGに向けて挿入され第2ねじ穴39に挿入できる第2調整ねじ37を備える。
図13は、2つの第1調整ねじ35a〜bとこれらに対応する2つの第1貫通ねじ穴36a〜bに加えて、1つの第2調整ねじ37と対応する1組の第2バカ穴38と第2ねじ穴39を示すが、第1調整ねじと第2調整ねじの数は、羽根の翼面の形状及び当該形状を記憶する精度に応じて選択できる。羽根の翼面上を多くの箇所で記憶するために、多くのプロペラゲージを用いるため、各プロペラゲージは、好ましくは、少なくとも1つの第1調整ねじ及び少なくとも1つの第2調整ねじ、これに対応する少なくとも1つの第1貫通ねじ穴及び少なくとも1組の第2バカ穴と第2ねじ穴を備えればよい。
As shown in FIG. 13, one of the upper movable piece 32a and the lower movable piece 32b has a gap G in the first through screw holes 36a and 36b and the first through screw holes 36a and 36b. The first adjustment screws 35a and 35b are inserted into the first through screw holes 36a and 36b, and one of the upper movable piece 32a and the lower movable piece 32b has a gap in the vertical direction. The second screw hole 39 is provided to the second screw hole 39 and the second screw hole 39 communicating with the second screw hole 38 is provided to the second screw hole 39. A second adjustment screw 37 that can be inserted is provided.
FIG. 13 shows a pair of second burr holes 38 corresponding to one second adjustment screw 37 in addition to the two first adjustment screws 35a-b and the two first through screw holes 36a-b corresponding thereto. The number of the first adjustment screw and the second adjustment screw can be selected according to the shape of the blade surface of the blade and the accuracy of storing the shape. Since many propeller gauges are used to memorize the blade surface on many points, each propeller gauge preferably corresponds to at least one first adjustment screw and at least one second adjustment screw. It suffices to have at least one first through screw hole and at least one set of second fool hole and second screw hole.

プロペラゲージ30をプロペラ100に設置し、羽根101の翼面に固定部34の下方を接触させる。羽根101の翼面に固定部34の下方を接触させた後、計測部33の下方を羽根101の翼面に接触させ、線p−qの全体が羽根の翼面を接触するように調整ねじを用いて調整する。
第1貫通ねじ穴36aに第1調整ねじ35aを回してねじ込むと、第1調整ねじ35aの先端が他方の可動片と接触すると止まり、さらに回すと上可動片32aと下可動片32bのギャップGが上下方向に拡張し計測部33が羽根の翼面に近づくように作用する。第1調整ねじ35aの先端が接触する他方の可動板には、調整ねじとの繰り返しの接触により他方の可動板が摩耗することを防止するため、耐摩耗性の高い補強材RMを設置すると良い。
また、第2バカ穴38を経て第2ねじ穴39に第2調整ねじ37を回してねじ込むと、第2バカ穴38を通過後第2ねじ穴39に侵入して第2調整ねじ37の頭部が第2バカ穴38の入口で止まり、さらに回すと上可動片32aと下可動片32bのギャップGが上下方向に収縮し計測部33が羽根の翼面から遠ざかるように作用する。第2バカ穴38に連通する第2ねじ穴39は、貫通するねじ穴でも、貫通しないねじ穴でもよいが、貫通しないねじ穴を用いるときは、第2調整ねじ37が最大限に挿入された場合でも収納できる深さであることが好ましく、製造上の容易さの点において貫通するねじ穴が好ましい。また、第2バカ穴38は、第2調整ねじ37の径よりやや大きい「バカ穴」であり、バカ穴とすることにより第2調整ねじ37と第2ねじ穴39でギャップGの収縮を行うことができる。
第1調整ねじ35a,35bによる調整及び第2調整ねじ37による調整を組み合わせることにより、少なくとも線p−qの全体を羽根の翼面を接触させて羽根の翼面をなぞることができる。
The propeller gauge 30 is installed on the propeller 100 and the lower surface of the fixed portion 34 is brought into contact with the blade surface of the blade 101. After the lower part of the fixed part 34 is brought into contact with the blade surface of the blade 101, the lower part of the measuring unit 33 is brought into contact with the blade surface of the blade 101, and the adjustment screw so that the whole line pq contacts the blade surface of the blade 101. Use to adjust.
When the first adjustment screw 35a is turned and screwed into the first through screw hole 36a, it stops when the tip of the first adjustment screw 35a comes into contact with the other movable piece, and when further turned, the gap G between the upper movable piece 32a and the lower movable piece 32b. Expands in the vertical direction and acts so that the measurement unit 33 approaches the blade surface of the blade. In order to prevent the other movable plate from being worn by repeated contact with the adjustment screw, the other movable plate with which the tip of the first adjustment screw 35a contacts is preferably provided with a reinforcing material RM having high wear resistance. .
Further, when the second adjustment screw 37 is turned and screwed into the second screw hole 39 through the second burr hole 38, the second adjustment screw 37 enters the second screw hole 39 after passing through the second burr hole 38. The part stops at the entrance of the second flaw hole 38, and when further rotated, the gap G between the upper movable piece 32a and the lower movable piece 32b contracts in the vertical direction so that the measuring part 33 acts away from the blade surface of the blade. The second screw hole 39 communicating with the second fool hole 38 may be a screw hole that penetrates or may not penetrate, but when the screw hole that does not penetrate is used, the second adjustment screw 37 is inserted to the maximum extent. Even in such a case, it is preferable to have a depth that can be accommodated, and a threaded hole that penetrates in terms of ease of manufacturing is preferable. In addition, the second burr hole 38 is a “burst hole” that is slightly larger than the diameter of the second adjustment screw 37, and the gap G is contracted by the second adjustment screw 37 and the second screw hole 39 by being a fool hole. be able to.
By combining the adjustment using the first adjustment screws 35a and 35b and the adjustment using the second adjustment screw 37, at least the entire line pq can be brought into contact with the blade surface of the blade and the blade surface of the blade can be traced.

本発明によるプロペラゲージの第4の形態例であるプロペラゲージ40を図14に基づき説明する。
プロペラゲージ40は、プロペラのプロペラボスの中空部に下部41bを挿入できるシャフト41と、シャフト41の上部41aから径方向に延びる可撓性の連結部(可動部)42と、可動部42の径方向をシャフト側と先端側に分けると、先端側において下方に延び、プロペラの羽根の翼面と少なくとも線p−qで接触可能な計測部43と、可動部42の不動であるシャフト側又はシャフトの上部において下方に延び、プロペラボスから延びる羽根の根元領域BAで羽根の翼面と接触可能となる、シャフト41を回転しないように固定する固定部44とを備える。
可動部42の先端側は、径方向に延びるギャップGを挟んで周方向に左可動片42a及び右可動片42bに分岐される。好ましくは、図14に示すように、板面を周方向に配置して、厚さ方向が上下方向に延びる可動板42の先端側に導入された径方向の切込みにより周方向にギャップGを隔てて左可動片42aと右可動片42bに分岐してもよい。なお、本明細書において、左右方向は、便宜上、シャフトの上方からシャフトの回転を見るとき、右回り(時計回り)となる方向を右方向、左回り(反時計回り)となる方向を左方向と呼ぶ。
計測部43は、左可動片42a又は右可動片42bのいずれか一方から下方に延び、羽根の翼面とのなす角度θが、垂直から左又は右方向に5〜30度傾けた角度(60°≦θ≦85°又は95°≦θ≦120°)となるようにして羽根の翼面と接触できるようにし、少なくとも線p−qで接触できるように好ましくは接触する部分の厚さを薄くしている。計測部の羽根の翼面と接触する部分と羽根の翼面とのなす角度θを、垂直より5〜30度の範囲で大きく又は小さくした角度とすることより、左可動片42a及び右可動片42bの少なくとも一方に設けた調整ねじでギャップGの間隔を収縮又は拡張させると、計測部43を周方向(左右方向)に動かすことができ、少なくとも線p−qの全体を羽根の翼面に接触させて羽根の翼面をなぞることができる。なお、角度θを垂直より5〜30度の範囲で大きく又は小さくした角度とするため、連結部の上下方向とシャフトの上下方向のなす角度θを変化させてもよい。
A propeller gauge 40 which is a fourth embodiment of the propeller gauge according to the present invention will be described with reference to FIG.
The propeller gauge 40 includes a shaft 41 into which the lower portion 41b can be inserted into the hollow portion of the propeller boss of the propeller, a flexible connecting portion (movable portion) 42 extending in the radial direction from the upper portion 41a of the shaft 41, and the diameter of the movable portion 42. When the direction is divided into the shaft side and the tip side, the measuring part 43 that extends downward on the tip side and can contact the blade surface of the blade of the propeller at least by the line pq, and the shaft side or the shaft where the movable part 42 is immovable And a fixing portion 44 for fixing the shaft 41 so as not to rotate. The fixing portion 44 extends downward from the upper portion of the blade and can come into contact with the blade surface of the blade in the blade root area BA extending from the propeller boss.
The distal end side of the movable portion 42 is branched into a left movable piece 42a and a right movable piece 42b in the circumferential direction with a gap G extending in the radial direction interposed therebetween. Preferably, as shown in FIG. 14, the plate surface is arranged in the circumferential direction, and the gap G is separated in the circumferential direction by a radial cut introduced in the distal end side of the movable plate 42 whose thickness direction extends in the vertical direction. The left movable piece 42a and the right movable piece 42b may be branched. In this specification, for the sake of convenience, when viewing the rotation of the shaft from above the shaft, the clockwise direction is the clockwise direction (clockwise) and the counterclockwise direction is the left direction. Call it.
Measurement unit 43 extends from either the left movable piece 42a or right movable piece 42b downward, the angle theta 2 between the blade surface of the blade, inclined 5-30 degrees left or right from the vertical angle ( 60 ° ≦ θ 2 ≦ 85 ° or 95 ° ≦ θ 2 ≦ 120 °), and contact with the blade surface of the blade, and preferably the thickness of the contacted portion so that contact can be made at least with the line pq The thickness is thinned. The angle theta 2 between the blade surface of the part and the blade in contact with the blade surface of the blade of the measuring part, than to a larger or smaller angular range of 5 to 30 degrees from vertical, left movable piece 42a and right movable When the gap G is contracted or expanded with an adjusting screw provided on at least one of the pieces 42b, the measuring section 43 can be moved in the circumferential direction (left-right direction), and at least the entire line pq is at least the blade surface of the blade. The blade surface of the blade can be traced by contacting the blade. In order to the angle theta 2 with larger or smaller angular range of 5 to 30 degrees from the vertical, it may be changed in the vertical direction and the vertical direction of the angle theta 1 of the shaft of the connecting portion.

図14に示すように、左可動片42aと右可動片42bのいずれか一方は、左右方向にギャップGに向かう第1貫通ねじ穴46と、第1貫通ねじ穴46にギャップGに向けて挿入される第1調整ねじ45を備え、第1貫通ねじ穴46とは径方向の異なる位置に左可動片42aと右可動片42bのいずれか一方が左右方向にギャップGに向けて第2バカ穴48を備えるとともに他方が第2バカ穴48に連通する第2ねじ穴49を備え、さらに第2バカ穴48からギャップGに向けて挿入され第2ねじ穴49に挿入できる第2調整ねじ47を備える。
図14は、1つの第1調整ねじ45とこれに対応する1つの第1貫通ねじ穴46に加えて、1つの第2調整ねじ47と対応する1組の第2バカ穴48と第2ねじ穴49を示すが、第1調整ねじと第2調整ねじの数は、羽根の翼面の形状及び当該形状を記憶する精度に応じて選択できる。羽根の翼面上を多くの箇所で記憶するために、多くのプロペラゲージを用いるため、各プロペラゲージは、好ましくは、少なくとも1つの第1調整ねじ及び少なくとも1つの第2調整ねじ、これに対応する少なくとも1つの第1貫通ねじ穴及び少なくとも1組の第2バカ穴と第2ねじ穴を備えればよい。
As shown in FIG. 14, one of the left movable piece 42 a and the right movable piece 42 b is inserted into the first through screw hole 46 toward the gap G in the left-right direction and into the first through screw hole 46 toward the gap G. The first adjusting screw 45 is provided, and either the left movable piece 42a or the right movable piece 42b is located at a position different from the first through screw hole 46 in the radial direction. 48, and the other includes a second screw hole 49 that communicates with the second burr hole 48, and a second adjustment screw 47 that is inserted from the second burr hole 48 toward the gap G and can be inserted into the second screw hole 49. Prepare.
FIG. 14 shows a pair of second burr holes 48 and second screws corresponding to one second adjustment screw 47 in addition to one first adjustment screw 45 and one corresponding first through screw hole 46. Although the hole 49 is shown, the number of the first adjustment screw and the second adjustment screw can be selected according to the shape of the blade surface of the blade and the accuracy of storing the shape. Since many propeller gauges are used to memorize the blade surface on many points, each propeller gauge preferably corresponds to at least one first adjustment screw and at least one second adjustment screw. It suffices to have at least one first through screw hole and at least one set of second fool hole and second screw hole.

プロペラゲージ40をプロペラ100に設置し、羽根101の翼面に固定部44の下方を接触させる。羽根101の翼面に固定部44の下方を接触させた後、計測部43の下方を羽根101の翼面に接触させ、線p−qの全体が羽根の翼面を接触するように調整ねじを用いて調整する。
第1貫通ねじ穴46に第1調整ねじ45を回してねじ込むと、第1調整ねじ45の先端が他方の可動片と接触すると止まり、さらに回すと左可動片42aと右可動片42bのギャップGが周方向に拡張し計測部43が羽根の翼面を第1周方向に移動するように作用する。第1調整ねじ45aの先端が接触する他方の可動板には、調整ねじとの繰り返しの接触により他方の可動板が摩耗することを防止するため、耐摩耗性の高い補強材RMを設置すると良い。
また、第2バカ穴48を経て第2ねじ穴49に第2調整ねじ47を回してねじ込むと、第2バカ穴48を通過後第2ねじ穴49に侵入して第2調整ねじ47の頭部が第2バカ穴48の入口で止まり、さらに回すと左可動片42aと右可動片42bのギャップGが周方向に収縮し計測部43が羽根の翼面を第1周方向とは反対の第2周方向に移動するように作用する。第2バカ穴48に連通する第2ねじ穴49は、貫通するねじ穴でも、貫通しないねじ穴でもよいが、貫通しないねじ穴を用いるときは、第2調整ねじ47が最大限に挿入された場合でも収納できる深さであることが好ましく、製造上の容易さの点において貫通するねじ穴が好ましい。また、第2バカ穴48は、第2調整ねじ47の径よりやや大きい「バカ穴」であり、バカ穴とすることにより第2調整ねじ47と第2ねじ穴49でギャップGの収縮を行うことができる。
第1調整ねじ45による調整及び第2調整ねじ47による調整を組み合わせることにより、少なくとも線p−qの全体を羽根の翼面を接触させて羽根の翼面をなぞることが可能となる。
The propeller gauge 40 is installed on the propeller 100 and the lower surface of the fixed portion 44 is brought into contact with the blade surface of the blade 101. After the lower part of the fixed part 44 is brought into contact with the blade surface of the blade 101, the lower part of the measuring unit 43 is brought into contact with the blade surface of the blade 101, and the adjustment screw is brought into contact with the blade surface of the blade. Use to adjust.
When the first adjustment screw 45 is turned and screwed into the first through screw hole 46, it stops when the tip of the first adjustment screw 45 comes into contact with the other movable piece, and when further turned, the gap G between the left movable piece 42a and the right movable piece 42b. Expands in the circumferential direction, and the measuring unit 43 acts to move the blade surface of the blade in the first circumferential direction. In order to prevent the other movable plate from being worn by repeated contact with the adjustment screw, the other movable plate with which the tip of the first adjustment screw 45a contacts is preferably provided with a reinforcing material RM having high wear resistance. .
Further, when the second adjustment screw 47 is turned and screwed into the second screw hole 49 through the second burr hole 48, the second adjustment screw 47 enters the second screw hole 49 after passing through the second burr hole 48. The part stops at the entrance of the second hole 48, and when further rotated, the gap G between the left movable piece 42a and the right movable piece 42b contracts in the circumferential direction, and the measuring unit 43 causes the blade surface of the blade to be opposite to the first circumferential direction. It acts to move in the second circumferential direction. The second screw hole 49 communicating with the second fool hole 48 may be a screw hole that penetrates or a screw hole that does not penetrate, but when the screw hole that does not penetrate is used, the second adjustment screw 47 is inserted to the maximum extent. Even in such a case, it is preferable to have a depth that can be accommodated, and a threaded hole that penetrates in terms of ease of manufacturing is preferable. In addition, the second baffle hole 48 is a “burst hole” that is slightly larger than the diameter of the second adjustment screw 47, and the gap G is contracted by the second adjustment screw 47 and the second screw hole 49 by being a fool hole. be able to.
By combining the adjustment by the first adjustment screw 45 and the adjustment by the second adjustment screw 47, it is possible to trace the blade surface of the blade by bringing the blade surface of the blade into contact with at least the entire line pq.

これまで4つの形態例を図面に基づき説明したが、本発明は、これらの4つの形態例に限られず、同じ技術的思想の内で多くの形態例や変形例が含まれる。4つの形態例を示す図において、図中の符号は、その一の位が同じであれば同様又は類似の機能を有するように付されている。4つの形態例の図中の符号を付して、本発明の計測位置固定型のプロペラゲージの好ましい態様を記載すると以下の通りである。
プロペラ100のプロペラボス102の中空部に下部11b、21b、31b、41bを挿入できるシャフト11、21、31、41と、
シャフトの上部11a、21a、31a、41aから径方向に延びる可撓性の可動部であって、可動部の径方向をシャフト側と先端側に分けると、シャフト側において不動であり、先端側において径方向に延びるギャップを挟んで上可動片12a、22a、32aもしくは下可動片12b、22b、32b又は周方向の左可動片42aもしくは右可動片42bに分岐され、上下可動片の少なくとも一方又は前記左右可動片の少なくとも一方に設けた調整ねじ15a〜c、17a〜b、25a〜b、27、35a〜b、37、45、47で前記ギャップの間隔を収縮又は拡張させることにより上下方向又は左右方向に動かすことができる可撓性の可動部12、22、32、42と、
可動部の先端側において、上可動片もしくは下可動片から、又は右可動片もしくは左可動片から下方に延び、プロペラの羽根の翼面と少なくとも線p−q(但し、pとqは線の両端)で接触可能な計測部13、23、33、43と、
可動部のシャフト側又はシャフトの上部において下方に延び、プロペラボスから延びる羽根の根元領域BAで羽根の翼面と接触可能となる、回転可能な前記シャフトを固定する固定部14、24、34、44とを備え、可動部の先端側を上下方向又は左右方向に動かすことにより、計測部が少なくとも線p−qの全体を羽根の翼面を接触させて羽根の翼面をなぞることができる計測位置固定型のプロペラゲージ。
Up to this point, four exemplary embodiments have been described with reference to the drawings. However, the present invention is not limited to these four exemplary embodiments, and includes many exemplary embodiments and modifications within the same technical idea. In the drawings showing the four form examples, the reference numerals in the drawings are attached so as to have the same or similar functions as long as the ones are the same. It is as follows when the code | symbol in the figure of four example forms is attached | subjected and the preferable aspect of the propeller gauge of the measurement position fixed type | mold of this invention is described.
Shafts 11, 21, 31, 41 into which the lower parts 11 b, 21 b, 31 b, 41 b can be inserted into the hollow part of the propeller labs 102 of the propeller 100,
A flexible movable part extending in the radial direction from the upper parts 11a, 21a, 31a, 41a of the shaft. When the radial direction of the movable part is divided into the shaft side and the tip side, it is immobile on the shaft side, The upper movable pieces 12a, 22a, 32a or the lower movable pieces 12b, 22b, 32b or the left movable piece 42a or the right movable piece 42b in the circumferential direction are branched across a gap extending in the radial direction, and at least one of the upper and lower movable pieces or the aforementioned By adjusting or expanding the gap interval with the adjusting screws 15a to 15c, 17a to b, 25a to b, 27, 35a to b, 37, 45, 47 provided on at least one of the left and right movable pieces, Flexible movable parts 12, 22, 32, 42 that can be moved in the direction;
At the front end side of the movable part, it extends downward from the upper movable piece or the lower movable piece, or from the right movable piece or the left movable piece, and at least the line p-q (where p and q are lines) Measuring units 13, 23, 33, 43 that can be contacted at both ends),
A fixed part 14, 24, 34 for fixing the rotatable shaft, which extends downward on the shaft side of the movable part or on the upper part of the shaft and can come into contact with the blade surface of the blade in the blade root area BA extending from the propeller boss. 44, and the measurement unit can trace the blade surface of the blade by bringing the blade surface of the blade into contact with at least the entire line pq by moving the tip side of the movable portion in the vertical direction or the horizontal direction. Propeller gauge with fixed position.

プロペラゲージの可動部は、剛性材料ではなく可撓性材料で構成される。可動部に設けられたギャップを上下方向又は左右方向(周方向)に調整ねじで調整する際に、可撓性の可動部に挟まれるギャップが若干伸縮することができ、その伸縮に応じて上下可動片のいいずれか一方又は左右可動片のいずれか一方から延びる計測部も若干移動することができ、計測部を、プロペラの羽根の翼面を上下方向又は左右方向(周方向)に移動させる微調整が可能となる。
可動部に用いる可撓性材料は、例えば、プラスチックが挙げられ、好ましくは、調整ねじの動きが容易に確認できる点において透明度の高いプラスチックであり、アクリル酸エステル又はメタクリル酸エステルの重合体であるアクリル樹脂(特に好ましくはポリメチルメタクリレート(PMMA))、ポリカーボネート(PC)、ポリ塩化ビニル(PVC)、ポリエチレンテレフタレート(PET)等が挙げられる。また、好ましくは、可動部の形状をデータ化して3Dプリンターによりいつでも同じ形状のものを作ることも可能となる点においてABS樹脂、PLA樹脂等も挙げられる。
可動部にプラスチックを用いると、加工の容易さ及び接着剤等を用いる接着の容易さの点から、シャフト、計測部及び計測部もプラスチックとすることが好ましい。特に計測部は、羽根の翼面の接触箇所が容易に確認できる点において可動部と同様な透明度の高いプラスチックが好ましく、計測部の形状をデータ化して3Dプリンターによりいつでも同じ形状のものを作ることも可能となる点においてABS樹脂、PLA樹脂等も挙げられる。計測部にプラスチックを用いると、やすり等により削ることも可能である。
プロペラゲージのシャフト、可動部、固定部及び計測部が全てプラスチックから構成される場合、各部分を接着剤による接着又は加熱による融着で接合してもよいが、一部又は全部を一体的に成形してもよい。
The movable part of the propeller gauge is made of a flexible material, not a rigid material. When adjusting the gap provided in the movable part with the adjustment screw in the vertical direction or the left-right direction (circumferential direction), the gap sandwiched between the flexible movable parts can be slightly expanded and contracted depending on the expansion and contraction. The measuring unit extending from either one of the movable pieces or the left and right movable pieces can also move slightly, and the measuring unit moves the blade surface of the propeller blade in the vertical direction or the horizontal direction (circumferential direction). Fine adjustment is possible.
The flexible material used for the movable part is, for example, plastic, and is preferably a highly transparent plastic in that the movement of the adjusting screw can be easily confirmed, and is a polymer of acrylate ester or methacrylate ester. Examples thereof include acrylic resins (particularly preferably polymethyl methacrylate (PMMA)), polycarbonate (PC), polyvinyl chloride (PVC), polyethylene terephthalate (PET), and the like. Preferably, ABS resin, PLA resin, etc. are also mentioned in that the shape of the movable part can be converted into data and the same shape can be made at any time by a 3D printer.
When plastic is used for the movable part, it is preferable that the shaft, the measurement part, and the measurement part are also plastic from the viewpoint of ease of processing and easy adhesion using an adhesive or the like. In particular, the measurement unit is preferably a highly transparent plastic like the movable unit in that the contact location of the blade surface of the blade can be easily confirmed, and the shape of the measurement unit is converted into data and the same shape is always made by a 3D printer. In addition, ABS resin, PLA resin, and the like can also be mentioned in that they can be used. When plastic is used for the measuring part, it can be cut by a file or the like.
When the propeller gauge shaft, movable part, fixed part and measuring part are all made of plastic, each part may be joined by bonding with an adhesive or by fusion by heating, but part or all of them are integrated. You may shape | mold.

プロペラゲージは、周方向又は径方向に2つ以上の計測部を備えてもよいが、ギャップを共有することになるため、計測する翼面の形状が限られ、調整ねじの密集を緩和するため、プロペラゲージは大きくなる傾向がある。   The propeller gauge may include two or more measuring units in the circumferential direction or the radial direction, but since the gap is shared, the shape of the blade surface to be measured is limited, and the adjustment screw is less dense. The propeller gauge tends to be large.

上下可動片又は周方向の左右可動片に挟まれたギャップの間隔は、調整ねじにより調整できる間隔であれば特に限定されないが、例えば、調整ねじのねじ部の長さが10〜20mmのときのギャップは、好ましくは1〜8mmが挙げられ、より好ましくは2〜5mmである。   The gap between the vertically movable pieces or the left and right movable pieces in the circumferential direction is not particularly limited as long as the gap can be adjusted by the adjusting screw. For example, when the length of the screw portion of the adjusting screw is 10 to 20 mm The gap is preferably 1 to 8 mm, and more preferably 2 to 5 mm.

調整ねじは、第1貫通ねじ穴及び第2ねじ穴等のねじ穴にねじ込めるものであれば特に限定されず、例えば、全体が金属製であるねじ、プラスチック製の頭部以外は金属製であるねじ等が挙げられるが、指で頭部を回転させるときの感触の良さの点において、好ましくは頭部がプラスチック製で頭部以外が金属製であるねじである。なお、調整ねじの頭部は、ねじ部分の径よりも大きい部分で、第1貫通ねじ穴等のねじ穴及び第2バカ穴等のバカ穴に挿入できない部分である。
上下可動片又は左右可動片の一方の可動片を貫通する第1調整ねじの先端が接触する、他方となる前記上下可動片又は前記左右可動片の接触箇所には、好ましくは補強材RMを配置する。
ねじの先端を受け止める補強材RMとしては、特に限定されず、透明でない材料であってもよく、例えば、充填材により強度を高めたプラスチック片、強度の高いプラスチックを用いたプラスチック片、又はステンレススチール等の金属片が挙げられ、ねじの先端を受け止める可動片の部分に接着剤等で接着すれば良い。
The adjustment screw is not particularly limited as long as it can be screwed into screw holes such as the first through screw hole and the second screw hole. For example, the adjustment screw is made of metal except for a screw made entirely of metal and a plastic head. A certain screw or the like can be mentioned. From the viewpoint of good feeling when the head is rotated with a finger, the screw is preferably a screw whose head is made of plastic and other than the head. The head of the adjustment screw is a portion larger than the diameter of the screw portion, and is a portion that cannot be inserted into a screw hole such as a first through screw hole and a fool hole such as a second fool hole.
A reinforcing material RM is preferably disposed at the contact point of the upper and lower movable pieces or the left and right movable pieces that are in contact with the tip of the first adjustment screw penetrating one of the movable pieces of the vertical and left and right movable pieces. To do.
The reinforcing material RM for receiving the tip of the screw is not particularly limited, and may be a non-transparent material. For example, a plastic piece whose strength is increased by a filler, a plastic piece using a high-strength plastic, or stainless steel A metal piece such as the above may be used, and it may be bonded to the portion of the movable piece receiving the tip of the screw with an adhesive or the like.

ギャップGの間隔の伸長に寄与できる、一方の可動片を貫通し、好ましくは強化材料RMによって他方の可動片に受け止められる第1調整ねじの数及び第1貫通ねじ穴の数は、好ましくは少なくとも1組であるが、計測部がプロペラの羽根の翼面と線p−qで接触するとき、p側近辺の計測部の接触に影響を与える箇所、q側近辺の計測部の接触に影響を与える箇所に設置するためより好ましくは少なくとも2組、あるいはさらにp−qの中央部の計測部の接触に影響を与える箇所に設置するためさらに好ましくは少なくとも3組である。但し、数が増加すれば調整に要する時間も増加するため、計測部が接触する羽根の翼面がp−q間において急激な変化があるときは数を増加させ、ゆるやかな変化では数を減少させてもよい。数を増加させる代わりに、計測部の一部をやすり等で削ることも可能である。
ギャップGの間隔の収縮に寄与できる、一方の可動片を貫通する第2バカ穴からギャップに向けて挿入され、他方の可動片を好ましくは貫通する第2ねじ穴に挿入できる第2調整ねじの数、第2バカ穴の数、及び第2ねじ穴の数は、好ましくは少なくとも1組であるが、計測部がプロペラの羽根の翼面と線p−qで接触するとき、p側近辺の計測部の接触に影響を与える箇所、q側近辺の計測部の接触に影響を与える箇所に設置するためより好ましくは少なくとも2組、あるいはさらにp−qの中央部の計測部の接触に影響を与える箇所に設置するためさらに好ましくは少なくとも3組である。但し、数が増加すれば調整に要する時間も増加するため、計測部が接触する羽根の翼面がp−q間において急激な変化があるときは数を増加させ、ゆるやかな変化では数を減少させてもよい。数を増加させる代わりに、計測部の一部をやすり等で削ることも可能である。
第2バカ穴に連通する第2ねじ穴は、貫通する穴でも、貫通しない穴でもよいが、貫通しない穴を用いるときは、第2調整ねじが最大限に挿入された場合でも収納できる深さであることが好ましく、製造上の容易さの点において貫通する穴が好ましい。また、第2バカ穴は、第2調整ねじの径よりやや大きい「バカ穴」であり、バカ穴とすることにより第2調整ねじと第2ねじ穴でギャップGの収縮を行うことができる。バカ穴は、ねじよりも径が大きいためねじ切りが不要であり、通常はねじのない穴である。
ギャップGの間隔の伸長用の第1調整ねじ及び第1貫通ねじ穴の少なくとも1組と、ギャップGの間隔の収縮用の第2調整ねじ、第2バカ穴及び第2ねじ穴の少なくとも1組とのうち、いずれか一方のみを備えるプロペラゲージも有用となる場合がある。例えば、試運転等の結果により、プロペラの修正(木槌のたたき方等)の方向性が決まっている場合は、拡張用だけでも収縮用だけでも良いことになる。試運転等により回転を上げることが判明としているときが例示できる。
しかし、通常は、拡張用の少なくとも1組と収縮用の少なくとも1組の両方を備えるプロペラゲージが好ましく、組数が増えるほど精度も高くなるが、ゲージ自体が込み合い、操作しにくくなる場合がある。第1の形態例では、より好ましくは、拡張用の2組と収縮用の2組の両方を備えるプロペラゲージであり、さらに好ましくは、拡張用の少なくとも2組と収縮用の少なくとも2組の両方を備えるプロペラゲージである。第2〜4の形態例では、より好ましくは、拡張用の2組と収縮用の1組の両方を備えるプロペラゲージであり、さらに好ましくは、拡張用の少なくとも2組と収縮用の少なくとも1組の両方を備えるプロペラゲージである。第2〜4の形態例では、線p−qのそれぞれ両端近辺で翼面に計測部を接触させるために拡張用の2組を利用し、線p−qの中央部で翼面に計測部を接触させるために収縮用の1組を利用することで足りる場合があるからである。
The number of first adjustment screws and the number of first through screw holes that can contribute to the extension of the gap G and pass through one movable piece, preferably received by the other movable piece by the reinforcing material RM, are preferably at least Although it is one set, when the measurement unit contacts the blade surface of the propeller blade at the line pq, it affects the contact of the measurement unit near the p side and the contact of the measurement unit near the q side. More preferably, there are at least two sets for installation at a given location, or even more preferably at least three sets for installation at a location that affects the contact of the measurement part at the center of pq. However, since the time required for adjustment increases as the number increases, the number increases when the blade surface of the blade contacting the measuring part changes rapidly between p-q, and the number decreases when the change is gentle. You may let them. Instead of increasing the number, a part of the measuring unit can be cut with a file or the like.
A second adjustment screw that can contribute to shrinkage of the gap G and is inserted toward the gap from a second burr hole that penetrates one movable piece, and preferably can be inserted into a second screw hole that penetrates the other movable piece. The number, the number of the second hole, and the number of the second screw hole are preferably at least one set. However, when the measurement unit contacts the blade surface of the propeller blade at the line pq, it is in the vicinity of the p side. More preferably at least two sets, or even in the center of pq, to affect the contact of the measurement unit in the location that affects the contact of the measurement unit, the location that affects the contact of the measurement unit near the q side More preferably, there are at least three sets for installation at a given location. However, since the time required for adjustment increases as the number increases, the number increases when the blade surface of the blade contacting the measuring part changes rapidly between p-q, and the number decreases when the change is gentle. You may let them. Instead of increasing the number, a part of the measuring unit can be cut with a file or the like.
The second screw hole communicating with the second fool hole may be a through hole or a hole that does not penetrate, but when using a hole that does not penetrate, the depth that can be accommodated even when the second adjustment screw is inserted to the maximum extent. It is preferable that the through-hole is preferable in terms of manufacturing ease. The second hole is a “burr hole” that is slightly larger than the diameter of the second adjustment screw. By using the second hole, the gap G can be contracted between the second adjustment screw and the second screw hole. Since the diameter of the hole is larger than that of the screw, the screw hole is not required and is usually a hole without a screw.
At least one set of a first adjustment screw and a first through screw hole for extending the gap G interval, and at least one set of a second adjustment screw, a second burr hole and a second screw hole for shrinking the gap G interval. Of these, a propeller gauge having only one of them may be useful. For example, when the direction of propeller correction (how to beat a wooden mallet, etc.) is determined based on the result of a trial run or the like, only expansion or contraction may be used. A case where it is found that the rotation is increased by a trial run or the like can be exemplified.
However, normally, a propeller gauge having both at least one set for expansion and at least one set for contraction is preferable, and the accuracy increases as the number of sets increases, but the gauge itself may be crowded and difficult to operate. . In the first embodiment, more preferably, the propeller gauge includes both two sets for expansion and two sets for contraction, and more preferably, both at least two sets for expansion and at least two sets for contraction. Propeller gauge with In the second to fourth embodiments, more preferably, the propeller gauge includes both two sets for expansion and one set for contraction, and more preferably, at least two sets for expansion and at least one set for contraction. Propeller gauge with both. In the second to fourth embodiments, two sets for expansion are used to bring the measurement unit into contact with the blade surface near both ends of the line pq, and the measurement unit is provided on the blade surface at the center of the line pq. This is because it may be sufficient to use one set for contraction in order to bring them into contact with each other.

一方の可動片を貫通し、好ましくは強化材料RMによって他方の可動片に受け止められる第1調整ねじは、その先端が他方の可動片に接触した直後から、調整ねじの回転の度合いに応じてギャップの間隔の伸長に寄与できる。すなわち、第1調整ねじの先端が他方の可動片に接触した直後から、第1調整ねじを回転した角度を記録して文字化することも可能である。文字化により記録に残すことが可能となり、過去に計測した羽根の翼面の形状と比較することが可能となり、プロペラの羽根の翼面形状の最適化に有用な情報を得ることができる。
一方の可動片を貫通する第2バカ穴からギャップに向けて挿入され、他方の可動片を好ましくは貫通する第2ねじ穴に挿入できる第2調整ねじは、第2調整ねじの頭部が一方の可動片に接触した直後から、第2調整ねじの回転の度合いに応じてギャップの間隔の収縮に寄与できる。すなわち、第2調整ねじの頭部が一方の可動片に接触した直後から、第2調整ねじを回転した角度を記録して文字化することも可能である。文字化により記録に残すことが可能により、過去に計測した羽根の翼面の形状と比較することが可能になり、プロペラの羽根の翼面形状の最適化に有用な情報を得ることができる。
第1及び第2調整ねじの回転角度は、例えば、調整ねじの頭部にペン等で印をつけ、その印が移動した角度で読み取ることができる。また、調製ねじの頭部の周囲に目盛を付し、回転に対応する目盛の数を記録してもよい。
The first adjustment screw that penetrates one movable piece and is preferably received by the other movable piece by the reinforcing material RM is a gap depending on the degree of rotation of the adjustment screw immediately after its tip contacts the other movable piece. Can contribute to the extension of the interval. That is, immediately after the tip of the first adjustment screw comes into contact with the other movable piece, it is also possible to record and angle the rotation angle of the first adjustment screw. It becomes possible to leave a record by characterization, and it is possible to compare with the shape of the blade surface of the blade measured in the past, and information useful for optimizing the blade surface shape of the blade of the propeller can be obtained.
The second adjustment screw that can be inserted into the second screw hole that penetrates the other movable piece through the second burr hole that penetrates one movable piece and preferably penetrates the other movable piece has one head of the second adjustment screw. Immediately after contact with the movable piece, it is possible to contribute to contraction of the gap interval according to the degree of rotation of the second adjustment screw. That is, immediately after the head of the second adjustment screw comes into contact with one movable piece, the angle at which the second adjustment screw is rotated can be recorded and converted into text. By making it possible to record it by recording, it becomes possible to compare with the blade surface shape measured in the past, and information useful for optimizing the blade surface shape of the propeller blade can be obtained.
The rotation angle of the first and second adjustment screws can be read, for example, by marking the head of the adjustment screw with a pen or the like and moving the mark. Moreover, a scale may be attached around the head of the preparation screw, and the number of scales corresponding to the rotation may be recorded.

プロペラゲージを用いて羽根の翼面の形状を記憶した後、競艇に取り付けて試走させ感触を得る。必要であれば、さらに羽根の翼面の形状を修正した後、羽根の翼面の形状を計測して記憶し、競艇に取り付けて試走させる。これを繰り返して最適なプロペラの翼面の形状を得ると同時に、その形状を記憶する。実際のレースでも好感触を得た場合には、次のレースで新たなプロペラを供給された際にも翼面の形状を記憶しておいたプロペラゲージを用いて、効率的に翼面の形状を再現できる。競艇との組合せで最適なプロペラの翼面の形状は変動し、過去の最適な羽根の形状が今回も最適であるとは限らないため、さらに競艇に取り付けて試走して最適化を図るが、過去の最適な羽根の形状からスタートできるため、最適化に要する時間は大幅に短縮できる。
プロペラの翼面の形状の変更は、通常、シャフトと台座とを備える修正台を用い、プロペラボスの中空部をシャフトに通すことによりプロペラを台座に載せ、プロペラと台座の間に、板上に皮又はゴムを貼り付けた敷き皮をはさみ、木槌でたたいてプラペラを所望の形状を変化させることにより達成できる。
After storing the shape of the blade surface of the blade with a propeller gauge, get a feel to test run attached to competing run boat. If necessary, further after modifying the shape of the blade surface of the blade, and stores the measured shape of the blade surface of the blade, to test run attached to competing run boat. This process is repeated to obtain the optimum propeller blade surface shape, and at the same time, the shape is stored. If you get a good feel in the actual race, use the propeller gauge that remembered the shape of the wing surface even when a new propeller was supplied in the next race. Can be reproduced. The shape of the blade surface of the optimum propeller in combination with the competition run boat varies, the shape of the past optimum blade is not necessarily the ideal time, optimized test run attached to more competitive run boat However, since it is possible to start from the past optimum blade shape, the time required for the optimization can be greatly shortened.
To change the shape of the wing surface of the propeller, usually use a correction base equipped with a shaft and a pedestal, and place the propeller on the base by passing the hollow part of the propeller through the shaft, and between the propeller and the base, on the plate This can be achieved by sandwiching a leather or rubber covered sheet and striking with a mallet to change the desired shape of the plapeller.

1,11,21,31,41,111 シャフト
11a,21a,31a,41a,111a シャフトの上部
11b,21b,31b,41b,111b シャフトの下部
2,12,22,32,42,112 連結部又は可動部
10,20,30,40,110 プロペラゲージ
12a,22a,32a 上可動片
12b,22b,32b 下可動片
12s,22s スペーサ
42a 左可動片
42b 右可動片
3,13,23,33,43,113 計測部
4,14,24,34,44 固定部
15a〜c,25a〜b,35a〜b,45 第1調整ねじ
16a〜c,26a〜b,36a〜b,46 第1貫通ねじ穴
17a〜b,27,37,47 第2調整ねじ
18a〜b,28,38,48 第2バカ穴
19a〜b,29,39,49 第2ねじ穴
100 プロペラ
101 羽根
101a 前縁
101b 後縁
102 プロペラボス
103 シャーピン収納溝
BA 羽根の根元領域
RM 補強材
1, 11, 21, 31, 41, 111 Shaft 11a, 21a, 31a, 41a, 111a Shaft upper part 11b, 21b, 31b, 41b, 111b Shaft lower part 2, 12, 22, 32, 42, 112 Movable part 10, 20, 30, 40, 110 Propeller gauges 12a, 22a, 32a Upper movable piece 12b, 22b, 32b Lower movable piece 12s, 22s Spacer 42a Left movable piece 42b Right movable piece 3, 13, 23, 33, 43 , 113 Measuring parts 4, 14, 24, 34, 44 Fixing parts 15a-c, 25a-b, 35a-b, 45 First adjusting screws 16a-c, 26a-b, 36a-b, 46 First through screw holes 17a-b, 27, 37, 47 Second adjusting screws 18a-b, 28, 38, 48 Second fool holes 19a-b, 29, 39, 49 Second screw holes 100 Propeller 101 blades 101a leading 101b trailing edge 102 propeller boss 103 shear pin receiving groove BA blade root area RM reinforcements

Claims (11)

プロペラのプロペラボスの中空部に下部を挿入できるシャフトと、
前記シャフトの上部から径方向に延びる連結部と、
前記連結部の径方向をシャフト側と先端側に分けると、前記先端側において下方に延び、前記プロペラの羽根の翼面と少なくとも線p−q(但し、pとqは線の両端)で接触可能な計測部と、
前記連結部の前記シャフト側又は前記シャフトの上部において下方に延び、前記プロペラボスから延びる前記羽根の根元領域で前記羽根の翼面と接触可能となる、回転可能な前記シャフトを固定する固定部とを備える計測位置固定型のプロペラゲージ。
A shaft that can insert the lower part into the hollow part of the propeller boss of the propeller,
A connecting portion extending in a radial direction from an upper portion of the shaft;
When the radial direction of the connecting portion is divided into the shaft side and the tip side, it extends downward on the tip side, and contacts with the blade surface of the blade of the propeller at least by lines pq (where p and q are both ends of the line) Possible measuring units,
A fixing part for fixing the rotatable shaft, which extends downward on the shaft side of the connecting part or on the upper part of the shaft, and can come into contact with a blade surface of the blade in a root region of the blade extending from the propeller boss. Propeller gauge with a fixed measurement position.
前記連結部が、前記シャフト側において不動であり、前記先端側において径方向に延びるギャップを挟んで上下可動片又は周方向の左右可動片に分岐され、前記上下可動片の少なくとも一方又は前記左右可動片の少なくとも一方に設けた調整ねじで前記ギャップの間隔を収縮又は拡張させることにより上下方向又は左右方向に動かすことができる可撓性の可動部であり、
前記計測部が、前記上もしくは下可動片から、又は前記右もしくは左可動片から下方に延び、前記プロペラの羽根の翼面と少なくとも前記線p−qで接触可能であり、
前記可動部の先端側を上下方向又は左右方向に動かすことにより、前記計測部が少なくとも前記線p−qの全体を前記羽根の翼面を接触させて前記羽根の翼面をなぞることができる請求項1に記載の計測位置固定型のプロペラゲージ。
The connecting portion is immovable on the shaft side, and is branched into a vertically movable piece or a left and right movable piece in a circumferential direction across a gap extending in the radial direction on the tip side, and at least one of the vertically movable piece or the left and right movable piece It is a flexible movable part that can be moved in the vertical direction or the horizontal direction by contracting or expanding the gap interval with an adjusting screw provided on at least one of the pieces,
The measurement unit extends downward from the upper or lower movable piece or from the right or left movable piece, and can contact the blade surface of the blade of the propeller at least on the line pq.
By moving the front end side of the movable part in the up-down direction or the left-right direction, the measurement unit can trace the blade surface of the blade by bringing the blade surface of the blade into contact with at least the entire line pq. Item 3. A fixed-position propeller gauge according to item 1.
前記上可動片及び前記下可動片が、前記シャフト側に配置されたスペーサを介して前記ギャップを隔てて上可動板の板面と下可動板の板面を上下方向に重ねて構成され、
(i)前記上可動板と前記下可動板のいずれか一方が上下方向に前記ギャップに向かう第1貫通ねじ穴と、前記第1貫通ねじ穴に前記ギャップに向けて挿入される第1調整ねじを備え、かつ/又は(ii)前記第1貫通ねじ穴とは前記シャフトからの距離が異なっても同じでもよい周方向の異なる位置に前記上可動板と前記下可動板のいずれか一方が上下方向に前記ギャップに向けて第2バカ穴を備えるとともに他方が前記第2バカ穴に連通する第2ねじ穴を備え、さらに前記第2バカ穴から前記ギャップに向けて挿入され前記第2ねじ穴に挿入できる第2調整ねじを備え、
前記計測部が、周方向で前記上可動板もしくは前記下可動板から下方に延び、前記羽根の翼面と少なくとも前記線p−qで接触できるように接触可能な計測部であり、
前記第1貫通ねじ穴に前記第1調整ねじを回してねじ込むと、前記第1調整ねじの先端が他方の可動板と接触すると止まり、さらに回すと前記上可動板と前記下可動板のギャップが上下方向に拡張して、前記計測部が前記上可動板から延びるときは前記羽根の翼面から遠ざかるように作用し、前記計測部が前記下可動板から延びるときは前記羽根の翼面に近づくように作用し、
前記第2バカ穴を経て前記第2ねじ穴に前記第2調整ねじを回してねじ込むと、前記第2バカ穴を通過後前記第2ねじ穴に侵入して前記第2調整ねじの頭部が前記第2バカ穴の入口で止まり、さらに回すと前記上可動板と前記下可動板のギャップが上下方向に収縮して、前記計測部が前記上可動板から延びるときは前記羽根の翼面に近づくように作用し、前記計測部が前記下可動板から延びるときは前記羽根の翼面から遠ざかるように作用する請求項2に記載の計測位置固定型のプロペラゲージ。
The upper movable piece and the lower movable piece are configured by overlapping the plate surface of the upper movable plate and the plate surface of the lower movable plate in the vertical direction with the gap interposed therebetween via a spacer arranged on the shaft side,
(I) A first through screw hole in which one of the upper movable plate and the lower movable plate is directed in the vertical direction toward the gap, and a first adjustment screw inserted into the first through screw hole toward the gap And / or (ii) one of the upper movable plate and the lower movable plate is vertically moved at different positions in the circumferential direction that may be the same or different from the first through screw hole. The second screw hole is provided with a second screw hole in the direction toward the gap, the other having a second screw hole communicating with the second bug hole, and further inserted from the second hole toward the gap. A second adjusting screw that can be inserted into the
The measurement unit is a measurement unit that extends downward in the circumferential direction from the upper movable plate or the lower movable plate, and is capable of contacting the blade surface of the blade at least at the line pq.
When the first adjustment screw is turned and screwed into the first through screw hole, the tip of the first adjustment screw stops when it comes into contact with the other movable plate, and when further turned, the gap between the upper movable plate and the lower movable plate is increased. When the measuring unit extends from the upper movable plate, it extends away from the blade surface of the blade, and when the measuring unit extends from the lower movable plate, it approaches the blade surface of the blade. Acts as
When the second adjusting screw is turned and screwed into the second screw hole through the second hole, the head of the second adjusting screw enters the second screw hole after passing through the second hole. When stopped further, the gap between the upper movable plate and the lower movable plate contracts in the vertical direction, and when the measuring part extends from the upper movable plate, The propeller gauge of the measurement position fixed type according to claim 2, which acts so as to approach, and acts so as to move away from the blade surface of the blade when the measurement unit extends from the lower movable plate.
前記上可動片及び前記下可動片が、前記シャフト側に配置されたスペーサを介して前記ギャップを隔てて上可動板の板面と下可動板の板面を上下方向に重ねて構成され、
(i)前記上可動板と前記下可動板のいずれか一方が上下方向に前記ギャップに向かう第1貫通ねじ穴と、前記第1貫通ねじ穴に前記ギャップに向けて挿入される第1調整ねじを備え、かつ/又は(ii)前記第1貫通ねじ穴とは径方向の異なる位置に前記上可動板と前記下可動板のいずれか一方が上下方向に前記ギャップに向けて第2バカ穴を備えるとともに他方が前記第2バカ穴に連通する第2ねじ穴を備え、さらに前記第2バカ穴から前記ギャップに向けて挿入され前記第2ねじ穴に挿入できる第2調整ねじを備え、
前記計測部が、径方向で前記上可動板もしくは前記下可動板から下方に延び、前記羽根の翼面と少なくとも前記線p−qで接触できるように接触可能な計測部であり、
前記第1貫通ねじ穴に前記第1調整ねじを回してねじ込むと、前記第1調整ねじの先端が他方の可動板と接触すると止まり、さらに回すと前記上可動板と前記下可動板のギャップが上下方向に拡張して、前記計測部が前記上可動板から延びるときは前記羽根の翼面から遠ざかるように作用し、前記計測部が前記下可動板から延びるときは前記羽根の翼面に近づくように作用し、
前記第2バカ穴を経て前記第2ねじ穴に前記第2調整ねじを回してねじ込むと、前記第2バカ穴を通過後前記第2ねじ穴に侵入して前記第2調整ねじの頭部が前記第2バカ穴の入口で止まり、さらに回すと前記上可動板と前記下可動板のギャップが上下方向に収縮して、前記計測部が前記上可動板から延びるときは前記羽根の翼面に近づくように作用し、前記計測部が前記下可動板から延びるときは前記羽根の翼面から遠ざかるように作用する請求項2に記載の計測位置固定型のプロペラゲージ。
The upper movable piece and the lower movable piece are configured by overlapping the plate surface of the upper movable plate and the plate surface of the lower movable plate in the vertical direction with the gap interposed therebetween via a spacer arranged on the shaft side,
(I) A first through screw hole in which one of the upper movable plate and the lower movable plate is directed in the vertical direction toward the gap, and a first adjustment screw inserted into the first through screw hole toward the gap And / or (ii) one of the upper movable plate and the lower movable plate has a second burr hole in the vertical direction at a position different from the first through screw hole in the radial direction. And the other includes a second screw hole that communicates with the second hole, and a second adjustment screw that is inserted from the second hole toward the gap and can be inserted into the second hole.
The measurement unit is a measurement unit that extends downward in the radial direction from the upper movable plate or the lower movable plate, and is capable of contacting the blade surface of the blade at least at the line pq.
When the first adjustment screw is turned and screwed into the first through screw hole, the tip of the first adjustment screw stops when it comes into contact with the other movable plate, and when further turned, the gap between the upper movable plate and the lower movable plate is increased. When the measuring unit extends from the upper movable plate, it extends away from the blade surface of the blade, and when the measuring unit extends from the lower movable plate, it approaches the blade surface of the blade. Acts as
When the second adjusting screw is turned and screwed into the second screw hole through the second hole, the head of the second adjusting screw enters the second screw hole after passing through the second hole. When stopped further, the gap between the upper movable plate and the lower movable plate contracts in the vertical direction, and when the measuring part extends from the upper movable plate, The propeller gauge of the measurement position fixed type according to claim 2, which acts so as to approach, and acts so as to move away from the blade surface of the blade when the measurement unit extends from the lower movable plate.
前記可動部が、厚さ方向を周方向に配置して板面が上下方向に延びる可動板の先端側に導入された径方向の切込みにより前記ギャップを隔てて前記上可動片と前記下可動片に分けられ、
(i)前記上可動片と前記下可動片のいずれか一方が上下方向に第1貫通ねじ穴と、前記第1貫通ねじ穴に前記ギャップに向けて挿入される第1調整ねじを備え、かつ/又は(ii)前記第1貫通ねじ穴とは径方向の異なる位置に前記上可動片と前記下可動片のいずれか一方が上下方向に第2バカ穴を備えるとともに他方が前記第2バカ穴に連通する第2ねじ穴を備え、さらに前記第2バカ穴から前記ギャップに向けて挿入され前記第2ねじ穴に挿入できる第2調整ねじを備え、
前記計測部が、径方向で前記下可動片から下方に延び、前記羽根の翼面と少なくとも前記線p−qで接触できるように接触可能な計測部であり、
前記第1貫通ねじ穴に前記第1調整ねじを回してねじ込むと、前記第1調整ねじの先端が他方の可動片と接触すると止まり、さらに回すと前記上可動片と前記下可動片のギャップが上下方向に拡張し前記計測部が前記羽根の翼面に近づくように作用し、前記第2バカ穴を経て前記第2ねじ穴に前記第2調整ねじを回してねじ込むと、前記第2バカ穴を通過後前記第2ねじ穴に侵入して前記第2調整ねじの頭部が前記第2バカ穴の入口で止まり、さらに回すと前記上可動片と前記下可動片のギャップが上下方向に収縮し前記計測部が前記羽根の翼面から遠ざかるように作用する請求項2に記載の計測位置固定型のプロペラゲージ。
The upper movable piece and the lower movable piece are separated from each other by the radial notches introduced on the distal end side of the movable plate whose thickness direction is arranged in the circumferential direction and the plate surface extends in the vertical direction. Divided into
(I) One of the upper movable piece and the lower movable piece includes a first through screw hole in the vertical direction, and a first adjustment screw inserted into the first through screw hole toward the gap, and / Or (ii) One of the upper movable piece and the lower movable piece is provided with a second blower hole in the vertical direction at a position different from the first through screw hole in the radial direction, and the other is the second blower hole. A second screw hole that communicates with the second screw hole, and further includes a second adjustment screw that is inserted from the second hole hole toward the gap and can be inserted into the second screw hole;
The measuring unit extends downward from the lower movable piece in the radial direction, and is a measuring unit that can contact with the blade surface of the blade at least at the line pq.
When the first adjustment screw is turned and screwed into the first through screw hole, the tip of the first adjustment screw stops when it comes into contact with the other movable piece, and when further turned, the gap between the upper movable piece and the lower movable piece is increased. When the second adjustment screw is turned into the second screw hole through the second burr hole, the second burr hole is expanded by vertically extending and acting so that the measurement unit approaches the blade surface of the blade. After passing through the second screw hole, the head of the second adjustment screw stops at the entrance of the second burr hole, and when further turned, the gap between the upper movable piece and the lower movable piece contracts vertically. The measuring position fixed type propeller gauge according to claim 2, wherein the measuring unit acts so as to move away from the blade surface of the blade.
前記可動部が、板面を周方向に配置した可動板の先端側に導入された径方向の切込みにより周方向に前記ギャップを隔てて前記左可動片と前記右可動片に分けられ、
(i)前記左可動片と前記右可動片のいずれか一方が左右方向に第1貫通ねじ穴と、前記第1貫通ねじ穴に前記ギャップに向けて挿入される第1調整ねじを備え、かつ/又は(ii)前記第1貫通ねじ穴とは径方向の異なる位置に前記左可動片と前記右可動片のいずれか一方が左右方向に第2バカ穴を備えるとともに他方が前記第2バカ穴に連通する第2ねじ穴を備え、さらに前記第2バカ穴から前記ギャップに向けて挿入され前記第2ねじ穴に挿入できる第2調整ねじを備え、
前記計測部が、径方向で前記左可動片又は前記右可動片のいずれか一方から下方に延び、前記羽根の翼面とのなす角度が垂直より5〜30度の範囲で大きい又は小さい角度で前記羽根の翼面と少なくとも前記線p−qで接触可能な計測部であり、
前記第1貫通ねじ穴に前記第1調整ねじを回してねじ込むと、前記第1調整ねじの先端が他方の可動片と接触すると止まり、さらに回すと前記左可動片と前記右可動片のギャップが周方向に拡張し前記計測部が前記羽根の翼面を第1周方向に移動するように作用し、前記第2バカ穴を経て前記第2ねじ穴に前記第2調整ねじを回してねじ込むと、前記第2バカ穴を通過後前記第2ねじ穴に侵入して前記第2調整ねじの頭部が前記第2バカ穴の入口で止まり、さらに回すと前記左可動片と前記右可動片のギャップが周方向に収縮し前記計測部が前記羽根の翼面を前記第1周方向とは反対の第2周方向に移動するように作用する請求項2に記載の計測位置固定型のプロペラゲージ。
The movable portion is divided into the left movable piece and the right movable piece with a gap in the circumferential direction by a radial cut introduced on the distal end side of the movable plate having a plate surface arranged in the circumferential direction,
(I) One of the left movable piece and the right movable piece includes a first through screw hole in the left-right direction, and a first adjustment screw inserted into the first through screw hole toward the gap, and / Or (ii) One of the left movable piece and the right movable piece has a second burr hole in the left-right direction at a position different from the first through screw hole in the radial direction, and the other is the second burr hole. A second screw hole that communicates with the second screw hole, and further includes a second adjustment screw that is inserted from the second hole hole toward the gap and can be inserted into the second screw hole;
The measurement part extends downward from either the left movable piece or the right movable piece in the radial direction, and the angle formed with the blade surface of the blade is larger or smaller in the range of 5 to 30 degrees from the vertical. A measuring unit capable of contacting at least the line pq with the blade surface of the blade;
When the first adjusting screw is turned and screwed into the first through screw hole, it stops when the tip of the first adjusting screw comes into contact with the other movable piece, and when further turned, the gap between the left movable piece and the right movable piece is increased. Expanding in the circumferential direction, the measuring unit acts so as to move the blade surface of the blade in the first circumferential direction, and when the second adjustment screw is turned and screwed into the second screw hole through the second burr hole, Then, after passing through the second hole, it enters the second screw hole, the head of the second adjustment screw stops at the entrance of the second hole, and when further turned, the left movable piece and the right movable piece The fixed position type propeller gauge according to claim 2, wherein the gap contracts in the circumferential direction and the measurement unit acts so as to move the blade surface of the blade in a second circumferential direction opposite to the first circumferential direction. .
前記可動部の周方向で前記シャフトからの距離が異なっても同じでもよい位置に、前記第1貫通ねじ穴と前記第1調整ねじが少なくとも2組存在し、前記第2バカ穴と前記第2ねじ穴と前記第2調整ねじが少なくとも2組存在する請求項3に記載の計測位置固定型のプロペラゲージ。   There are at least two sets of the first through screw hole and the first adjustment screw at positions where the distance from the shaft may be different or the same in the circumferential direction of the movable portion, and the second burr hole and the second The propeller gauge of the measurement position fixed type according to claim 3, wherein there are at least two pairs of screw holes and the second adjustment screw. 前記可動部の径方向で前記シャフトからの距離が異なる位置に、前記第1貫通ねじ穴と前記第1調整ねじが少なくとも2組存在し、前記第2バカ穴と前記第2ねじ穴と前記第2調整ねじが少なくとも1組存在する請求項4〜6のいずれかに記載の計測位置固定型のプロペラゲージ。   At least two sets of the first through screw hole and the first adjustment screw are present at positions where the distance from the shaft is different in the radial direction of the movable portion, and the second burr hole, the second screw hole, and the first screw The measurement position fixed type propeller gauge according to any one of claims 4 to 6, wherein at least one set of two adjusting screws is present. 前記連結部又は前記可動部の上下方向が、前記シャフトの上下方向から前記プロぺラのピッチ角に対応させて傾いている請求項〜8のいずれかに記載の計測位置固定型のプロペラゲージ。 The fixed position type propeller gauge according to any one of claims 3 to 8, wherein the vertical direction of the connecting portion or the movable portion is inclined in correspondence with the pitch angle of the propeller from the vertical direction of the shaft. . 前記第1調整ねじの先端が接触する、前記他方となる前記上可動片もしくは前記下可動片又は前記左可動片もしくは前記右可動片の接触箇所に補強材を配置する請求項〜9のいずれかに記載の計測位置固定型のプロペラゲージ。 Tip of the first adjustment screw is in contact, either Claim 3-9 to place a reinforcing material to the contact portion of the upper movable piece or the lower movable piece or the left movable piece or the right movable piece formed and the other Propeller gauge with fixed measuring position as described in Crab. 前記連結部又は前記可動部の上下方向が、前記シャフトの上下方向から前記プロぺラのピッチ角に対応させて傾いている請求項1又は請求項2に記載の計測位置固定型のプロペラゲージ。 The propeller gauge of a fixed measurement position type according to claim 1 or 2 , wherein a vertical direction of the connecting portion or the movable portion is inclined in correspondence with a pitch angle of the propeller from a vertical direction of the shaft.
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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN116734702A (en) * 2023-08-07 2023-09-12 江苏烨培干燥工程有限公司 Screw blade continuous detection equipment for blade dryer

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Publication number Priority date Publication date Assignee Title
JPS58155301A (en) * 1982-03-12 1983-09-16 Tokyo Seimitsu Co Ltd Configuration measuring device by using three dimensional coordinate measuring machine
JP5073864B1 (en) * 2012-04-23 2012-11-14 ヤマト発動機株式会社 Wing surface shape recording device for propeller of outboard motor of race boat
JP2014016331A (en) * 2012-07-09 2014-01-30 Takuma Saito Propeller gage

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS58155301A (en) * 1982-03-12 1983-09-16 Tokyo Seimitsu Co Ltd Configuration measuring device by using three dimensional coordinate measuring machine
JP5073864B1 (en) * 2012-04-23 2012-11-14 ヤマト発動機株式会社 Wing surface shape recording device for propeller of outboard motor of race boat
JP2014016331A (en) * 2012-07-09 2014-01-30 Takuma Saito Propeller gage

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN116734702A (en) * 2023-08-07 2023-09-12 江苏烨培干燥工程有限公司 Screw blade continuous detection equipment for blade dryer
CN116734702B (en) * 2023-08-07 2023-10-13 江苏烨培干燥工程有限公司 Screw blade continuous detection equipment for blade dryer

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