JP2016188770A - Propeller characteristics measuring apparatus - Google Patents

Propeller characteristics measuring apparatus Download PDF

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JP2016188770A
JP2016188770A JP2015067955A JP2015067955A JP2016188770A JP 2016188770 A JP2016188770 A JP 2016188770A JP 2015067955 A JP2015067955 A JP 2015067955A JP 2015067955 A JP2015067955 A JP 2015067955A JP 2016188770 A JP2016188770 A JP 2016188770A
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propeller
motor
base
installation base
sensor
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JP6429236B2 (en
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広泰 下地
Hiroyasu Shimoji
広泰 下地
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Oita Prefectural Government
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Abstract

PROBLEM TO BE SOLVED: To enable propeller characteristics to be accurately measured in a state close to that of a real flying object even if the object is not actually flown.SOLUTION: In a propeller characteristics measuring apparatus (1) for measuring characteristics of a propeller (8), an installation base (3) for installing a motor (9) fitted with the propeller (8) is disposed via a guide mechanism (4) for so guiding the installation base (3) as to be able to move up and down but unable to rotate relative to a base plate (2) is provided on the base plate (2); further, a moving extent sensor (14) for detecting the moving extent of the propeller (8) in the rotating direction, a driving electric power sensor (22) for detecting the driving electric power supplied to the motor (9) and a floating force sensor (10) for detecting the floating force provided by the motor (9) are connected to a controller (20); and the controller (20) is thereby enabled to measure the characteristics in a state in which the propeller (8) is fitted to the motor (9).SELECTED DRAWING: Figure 1

Description

本発明は、プロペラをモータに装着した状態における駆動電力と浮上力との関係を計測することができるプロペラ特性測定装置に関するものである。   The present invention relates to a propeller characteristic measuring apparatus capable of measuring the relationship between driving power and levitation force in a state where a propeller is mounted on a motor.

近年、モータに装着したプロペラを用いて飛行するヘリコプター等の飛行体が農薬散布や航空撮影や遊技等を目的として多用されている（たとえば、特許文献１参照。）。   In recent years, flying objects such as helicopters that fly using propellers mounted on motors have been widely used for the purpose of spraying agricultural chemicals, aerial photography, games, and the like (for example, see Patent Document 1).

プロペラを用いた飛行体は、モータでプロペラを回転駆動させて飛行するために、モータで回転するプロペラの特性によって性能が左右される。   Since a flying object using a propeller is driven by rotating the propeller with a motor to fly, the performance depends on the characteristics of the propeller rotating with the motor.

そのため、従来においては、飛行体の性能を評価するために、プロペラ単体で設計値を満足するものか否かといったプロペラ特性を測定し評価していた。   Therefore, conventionally, in order to evaluate the performance of the flying object, propeller characteristics such as whether or not the propeller alone satisfies the design value have been measured and evaluated.

特開２００９−２７９３６８号公報JP 2009-279368 A

ところが、従来においてはプロペラ単体での測定に留まっていたために、モータに装着した状態でのプロペラの特性を正確には評価することができていなかった。   However, in the past, since the measurement was limited to the propeller alone, the characteristics of the propeller when mounted on the motor could not be accurately evaluated.

そのため、プロペラ単体での設計値は満足するものであっても、実際にプロペラをモータに装着して飛行させた際に、プロペラをモータに装着した状態での特性が低く、飛行体が落下し破損するおそれがあった。   For this reason, even if the design value of the propeller alone is satisfactory, when the propeller is actually mounted on the motor, the characteristics when the propeller is mounted on the motor are low, and the flying object falls. There was a risk of damage.

そこで、請求項１に係る本発明では、プロペラ特性測定装置において、基台に、プロペラを装着したモータを設置するための設置台を、基台に対して設置台が昇降可能かつ回動不能にガイドするためのガイド機構を介して設けるとともに、プロペラの回転方向の移動量を検出するための移動量センサと、モータに供給される駆動電力を検出するための駆動電力センサと、モータによる浮上力を検出するための浮上力センサとをコントローラに接続し、コントローラでプロペラをモータに装着した状態における特性を計測可能とすることにした。   Therefore, according to the first aspect of the present invention, in the propeller characteristic measuring device, the installation base for installing the motor equipped with the propeller is installed on the base so that the installation base can be lifted and lowered with respect to the base. Provided via a guide mechanism for guiding, a movement amount sensor for detecting the movement amount of the propeller in the rotation direction, a driving power sensor for detecting the driving power supplied to the motor, and a levitation force by the motor A levitation force sensor for detecting the propeller is connected to the controller, and the controller can measure the characteristics when the propeller is attached to the motor.

また、請求項２に係る本発明では、前記請求項１に係る本発明において、前記ガイド機構は、基台に上下方向へ向けて伸延させた左右一対のロッドを設けるとともに、設置台に左右方向へ向けて伸延させたアームを設け、アームの左右端部にロッドを昇降可能に挿通させることにした。   Further, in the present invention according to claim 2, in the present invention according to claim 1, the guide mechanism is provided with a pair of left and right rods extended in the vertical direction on the base and in the horizontal direction on the installation base. The arm extended toward the side was provided, and the rod was inserted into the left and right ends of the arm so as to be movable up and down.

また、請求項３に係る本発明では、前記請求項１又は請求項２に係る本発明において、前記設置台の上方に、前記プロペラと対向する他のプロペラをモータに装着した状態で設置するための他の設置台を上下位置変更可能に設けることにした。   Moreover, in this invention which concerns on Claim 3, in this invention which concerns on the said Claim 1 or Claim 2, in order to install in the state with which the other propeller facing the said propeller was mounted | worn with the motor above the said installation stand. The other installation base was decided to be able to change the vertical position.

そして、本発明では、以下に記載する効果を奏する。   And in this invention, there exists an effect described below.

すなわち、本発明では、プロペラ特性測定装置において、基台に、プロペラを装着したモータを設置するための設置台を、基台に対して設置台が昇降可能かつ回動不能にガイドするためのガイド機構を介して設けるとともに、プロペラの回転方向の移動量を検出するための移動量センサと、モータに供給される駆動電力を検出するための駆動電力センサと、モータによる浮上力を検出するための浮上力センサとをコントローラに接続しているために、コントローラでプロペラをモータに装着した状態における回転数と浮上力との関係や回転数と駆動効率との関係などの特性を計測することができ、プロペラの特性を実際の飛行体に近い状態で正確に計測することができる。   That is, according to the present invention, in the propeller characteristic measuring apparatus, a guide for guiding an installation base for installing a motor equipped with a propeller to the base so that the installation base can be lifted and lowered with respect to the base. A movement amount sensor for detecting the amount of movement of the propeller in the rotation direction, a driving power sensor for detecting the driving power supplied to the motor, and for detecting the levitation force by the motor Since the levitation force sensor is connected to the controller, the controller can measure characteristics such as the relationship between the rotational speed and the levitation force and the relationship between the rotational speed and the drive efficiency when the propeller is mounted on the motor. Propeller characteristics can be accurately measured in a state close to an actual flying object.

特に、前記ガイド機構の構成を、基台に上下方向へ向けて伸延させた左右一対のロッドを設けるとともに、設置台に左右方向へ向けて伸延させたアームを設け、アームの左右端部にロッドを昇降可能に挿通させた構成とした場合には、プロペラの回動によって生じる回転力を強固に抑制し、昇降可能かつ回動不能の状態を保持することができ、プロペラの特性を正確に計測することができる。   In particular, the structure of the guide mechanism is provided with a pair of left and right rods that extend in the vertical direction on the base, and an arm that is extended in the left and right directions on the installation base, and rods on the left and right ends of the arms. When it is configured so that it can be moved up and down, the rotational force generated by the rotation of the propeller can be firmly suppressed, and the state that can be moved up and down and cannot be rotated can be maintained, and the characteristics of the propeller can be accurately measured can do.

また、前記設置台の上方に、前記プロペラと対向する他のプロペラをモータに装着した状態で設置するための他の設置台を上下位置変更可能に設けた場合には、２個のプロペラを上下に対向させて配置した２重反転プロペラ構造におけるプロペラの特性や上下のプロペラの間の最適な距離等をも計測することができる。   In addition, when another installation base for installing another propeller facing the propeller is mounted on the motor above the installation base so that the vertical position can be changed, the two propellers are moved up and down. It is also possible to measure the propeller characteristics, the optimum distance between the upper and lower propellers, etc., in the double-reversed propeller structure arranged so as to be opposed to each other.

本発明に係るプロペラ特性測定装置を示す正面図。The front view which shows the propeller characteristic measuring apparatus which concerns on this invention. 同左側面図。The left side view. 同ブロック図。The block diagram. 測定結果の説明図。Explanatory drawing of a measurement result.

以下に、本発明に係るプロペラ特性測定装置の具体的な構成について図面を参照しながら説明する。   Hereinafter, a specific configuration of the propeller characteristic measuring apparatus according to the present invention will be described with reference to the drawings.

図１及び図２に示すように、プロペラ特性測定装置１は、基台２に設置台３をガイド機構４を介して取付けた構成となっている。   As shown in FIGS. 1 and 2, the propeller characteristic measuring apparatus 1 has a configuration in which an installation base 3 is attached to a base 2 via a guide mechanism 4.

基台２は、床５に矩形箱枠状のフレーム６を固定し、フレーム６に支持体７を取付けている。フレーム６には、開閉扉や安全柵や窓などを取付けてもよい。支持体７は、床５に対して固定されればよく、矩形状の板体で形成してもよく、また、複数の枠体で形成してもよい。   In the base 2, a frame 6 having a rectangular box frame shape is fixed to a floor 5, and a support body 7 is attached to the frame 6. An open / close door, a safety fence, a window, and the like may be attached to the frame 6. The support body 7 should just be fixed with respect to the floor | bed 5, may be formed with a rectangular-shaped board body, and may be formed with a some frame.

設置台３は、プロペラ８を装着したモータ９を設置するものであり、基台２の支持体７の上方に配置されている。設置台３と基台２の支持体７との間には、モータ９によって回転駆動させたプロペラ８による浮上力を検出するための浮上力センサ10としての圧力センサが介設されている。   The installation table 3 is for installing a motor 9 equipped with a propeller 8 and is disposed above the support 7 of the base 2. A pressure sensor as a levitation force sensor 10 for detecting a levitation force by a propeller 8 driven to rotate by a motor 9 is interposed between the installation base 3 and the support 7 of the base 2.

設置台３は、上部にモータ９のステータ11を着脱可能に取付ける。モータ９は、ステータ11の上方外周部にロータ12が設けられ、ロータ12の上部中央に回転軸13が設けられ、回転軸13にプロペラ８が装着される。設置台３には、モータ９のロータ12の回転方向への移動量を検出するための移動量センサ14としての近接センサが設けられている。この移動量センサ14でロータ12に貼付した金属等を検出することでモータ９のロータ12とともに回転するプロペラ８の回転方向への移動量（回転量）を検出するようにしている。   The mounting base 3 is detachably mounted with a stator 11 of the motor 9 on the top. In the motor 9, a rotor 12 is provided on the upper outer peripheral portion of the stator 11, a rotating shaft 13 is provided in the upper center of the rotor 12, and a propeller 8 is attached to the rotating shaft 13. The installation table 3 is provided with a proximity sensor as a movement amount sensor 14 for detecting the movement amount of the motor 9 in the rotation direction of the rotor 12. By detecting the metal or the like stuck on the rotor 12 by the movement amount sensor 14, the movement amount (rotation amount) of the propeller 8 rotating with the rotor 12 of the motor 9 in the rotation direction is detected.

ガイド機構４は、基台２の支持体７に対して設置台３を昇降可能かつ回動不能な状態を保持しながらガイドするための機構であり、基台２の支持体７の左右端部に上下方向へ向けて伸延させた左右一対のロッド16,17を設け、一方、設置台３を左右方向へ向けて伸延させた形状とすることで設置台３の左右側部に左右方向へ向けて伸延するアーム18,19を形成し、そして、アーム18,19の左右端部をロッド16,17に昇降可能に挿通させている。   The guide mechanism 4 is a mechanism for guiding the installation base 3 with respect to the support 7 of the base 2 while maintaining the state in which the installation base 3 can be moved up and down and cannot be rotated, and the left and right ends of the support 7 of the base 2 Is provided with a pair of left and right rods 16 and 17 extended in the vertical direction, while the installation base 3 is extended in the left and right direction so that the left and right sides of the installation base 3 are directed in the horizontal direction. The extending arms 18 and 19 are formed, and the left and right ends of the arms 18 and 19 are inserted into the rods 16 and 17 so as to be movable up and down.

プロペラ８をモータ９で回転駆動させると、プロペラ８の回転に伴って設置台３に上下方向の浮上力と円周方向の回転力とが作用するが、基台２と設置台３との間にガイド機構４を介設することで、設置台３をロッド16,17に沿って上下方向には移動できるが回転できないようにすることができる。これにより、浮上力センサ10や移動量センサ14で浮上力や移動量を正確に計測することができる。   When the propeller 8 is driven to rotate by the motor 9, vertical lifting force and circumferential rotational force act on the installation base 3 as the propeller 8 rotates. By installing the guide mechanism 4 at the top, the installation base 3 can be moved up and down along the rods 16 and 17 but cannot be rotated. Thereby, the levitation force and the movement amount can be accurately measured by the levitation force sensor 10 and the movement amount sensor 14.

なお、ガイド機構４は、基台２に対して設置台３を昇降可能かつ回動不能にガイドできればよく、上記構成に限られず、基台２に円柱部を形成するとともに、設置台３に円筒部を形成し、設置台３の円筒部を基台２の円柱部にキーを介して挿通させる構成などにすることもできる。上記構成のように、左右に伸延させたアーム18,19の端部をロッド16,17に挿通させることで回動を阻止する構成とした場合には、回動を阻止するために作用する回転モーメントを大きくすることができ、設置台３の回動をより確実に阻止することができ、より正確に計測を行うことができる。   The guide mechanism 4 is not limited to the above-described configuration as long as it can guide the installation table 3 up and down and non-rotatably with respect to the base 2, and forms a cylindrical portion on the base 2 and a cylinder on the installation table 3. The cylindrical portion of the installation table 3 can be inserted into the column portion of the base 2 through a key. Rotation that acts to prevent rotation when configured to prevent rotation by inserting the ends of the arms 18 and 19 extended left and right into the rods 16 and 17 as in the above configuration. The moment can be increased, the rotation of the installation table 3 can be more reliably prevented, and the measurement can be performed more accurately.

プロペラ特性測定装置１は、図３に示すように、汎用コンピュータ等から構成されるコントローラ20が設けられている。コントローラ20には、浮上力センサ10や移動量センサ14が接続されている。また、コントローラ20には、モータ９を駆動するドライバー回路21と、ドライバー回路21からモータ９に供給される駆動電力を検出する駆動電力センサ22とが接続されている。なお、ドライバー回路21をコントローラ20に接続して、コントローラ20からの指示でドライバー回路21を駆動するように構成しているが、これに限られず、ドライバー回路21に専用のモータコントローラを接続してもよい。   As shown in FIG. 3, the propeller characteristic measuring apparatus 1 is provided with a controller 20 composed of a general-purpose computer or the like. A levitation force sensor 10 and a movement amount sensor 14 are connected to the controller 20. The controller 20 is connected to a driver circuit 21 that drives the motor 9 and a drive power sensor 22 that detects drive power supplied from the driver circuit 21 to the motor 9. The driver circuit 21 is connected to the controller 20, and the driver circuit 21 is driven by an instruction from the controller 20. However, the present invention is not limited to this, and a dedicated motor controller is connected to the driver circuit 21. Also good.

コントローラ20は、ドライバー回路21から駆動電力をモータ９に供給してプロペラ８を回転駆動させた状態で、浮上力センサ10や移動量センサ14や駆動電力センサ22からプロペラ８の回転によって生じる浮上力や回転方向の移動量や駆動電力を計測する。これにより、たとえば、図４に示すように、プロペラ８の回転数と浮上力との関係や、プロペラ８の回転数と駆動効率（浮上力／駆動電力）との関係などといったプロペラ８の特性を計測することができる。これらプロペラ８の特性は、コントローラ20に設けられたモニターに表示したりプリンターで印刷することもできる。   The controller 20 supplies the driving power from the driver circuit 21 to the motor 9 to rotate the propeller 8, and the levitation force generated by the rotation of the propeller 8 from the levitation force sensor 10, the movement amount sensor 14, and the driving power sensor 22. Measure the amount of movement and the driving power in the rotation direction. Thereby, for example, as shown in FIG. 4, the characteristics of the propeller 8 such as the relationship between the rotational speed of the propeller 8 and the levitation force, the relationship between the rotational speed of the propeller 8 and the driving efficiency (levitation force / driving power), and the like. It can be measured. The characteristics of these propellers 8 can be displayed on a monitor provided in the controller 20 or printed by a printer.

プロペラ特性測定装置１では、さらに、図１及び図２に示すように、測定対象となるプロペラ８及びモータ９の上方に他のプロペラ23及びモータ24を配置して、２重反転プロペラ構造における特性の測定もできるようにしている。具体的には、設置台３の左右のアーム18,19の上部に上下方向へ向けて伸延させた左右一対のロッド25,26を取付け、左右のロッド25,26に設置台27を上下位置を変更可能に取付けている。この上方に配置した設置台27の下部にプロペラ23を装着したモータ24を取付ける。モータ24は、モータ９と同様にドライバー回路を介してコントローラ20に接続して駆動するようにしてもよく、また、専用のモータコントローラに接続して駆動するようにしてもよい。上方の設置台27の取付位置を上下に変更することで、下方のプロペラ８と上方のプロペラ23との間の距離を変更することができる。これにより、コントローラ20は、上下のプロペラ8,23を回転駆動させた状態で、浮上力センサ10や移動量センサ14や駆動電力センサ22からプロペラ８の回転によって生じる浮上力や回転方向の移動量や駆動電力を計測することができ、２個のプロペラ8,23を上下に対向させて配置した２重反転プロペラ構造におけるプロペラ８の特性や上下のプロペラ8,23の間の最適な距離等をも計測することができる。   In the propeller characteristic measuring apparatus 1, as shown in FIGS. 1 and 2, another propeller 23 and a motor 24 are arranged above the propeller 8 and the motor 9 to be measured, and the characteristics in the double reversing propeller structure are obtained. It is also possible to measure. Specifically, a pair of left and right rods 25 and 26 extended in the vertical direction are attached to the upper portions of the left and right arms 18 and 19 of the installation table 3, and the installation table 27 is placed in the vertical position on the left and right rods 25 and 26. It can be changed. A motor 24 equipped with a propeller 23 is attached to the lower part of the installation base 27 disposed above. Similarly to the motor 9, the motor 24 may be driven by being connected to the controller 20 via a driver circuit, or may be driven by being connected to a dedicated motor controller. By changing the mounting position of the upper installation base 27 up and down, the distance between the lower propeller 8 and the upper propeller 23 can be changed. As a result, the controller 20 causes the levitation force and the amount of movement in the direction of rotation generated by the rotation of the propeller 8 from the levitation force sensor 10, the movement amount sensor 14, and the drive power sensor 22 in a state where the upper and lower propellers 8 and 23 are rotationally driven. The drive power can be measured, and the characteristics of the propeller 8 in the double reversing propeller structure in which the two propellers 8 and 23 are opposed to each other up and down, the optimum distance between the upper and lower propellers 8 and 23, etc. Can also be measured.

以上に説明したように、上記プロペラ特性測定装置１は、基台２に、プロペラ８を装着したモータ９を設置するための設置台３を、基台２に対して設置台３が昇降可能かつ回動不能にガイドするためのガイド機構４を介して設けるとともに、プロペラ８の回転方向の移動量を検出するための移動量センサ14と、モータ９に供給される駆動電力を検出するための駆動電力センサ22と、モータ９による浮上力を検出するための浮上力センサ10とをコントローラ20に接続した構成となっている。   As described above, the propeller characteristic measuring apparatus 1 is configured such that the installation base 3 for installing the motor 9 with the propeller 8 mounted on the base 2 can be moved up and down with respect to the base 2. Provided via a guide mechanism 4 for guiding the rotation of the propeller 8 in a non-rotatable manner, a movement amount sensor 14 for detecting the movement amount of the propeller 8 in the rotation direction, and a drive for detecting the driving power supplied to the motor 9 The power sensor 22 and a levitation force sensor 10 for detecting the levitation force by the motor 9 are connected to the controller 20.

そのため、上記構成のプロペラ特性測定装置１では、コントローラ20でプロペラ８をモータ９に装着した状態における回転数と浮上力との関係や回転数と駆動効率との関係などの特性を計測することができ、飛行体を実際に飛行させなくても、プロペラ８の特性を実際の飛行体に近い状態で安全かつ正確に計測することができる。   Therefore, in the propeller characteristic measuring apparatus 1 configured as described above, the controller 20 can measure characteristics such as the relationship between the rotational speed and the levitation force and the relationship between the rotational speed and the driving efficiency when the propeller 8 is mounted on the motor 9. Even without actually flying the flying object, the characteristics of the propeller 8 can be measured safely and accurately in a state close to that of the actual flying object.

また、上記プロペラ特性測定装置１は、ガイド機構４の構成を、基台２に上下方向へ向けて伸延させた左右一対のロッド16,17を設けるとともに、設置台３に左右方向へ向けて伸延させたアーム18,19を設け、アーム18,19の左右端部にロッド16,17を昇降可能に挿通させた構成としている。   Further, the propeller characteristic measuring device 1 is provided with a pair of left and right rods 16 and 17 in which the configuration of the guide mechanism 4 is extended in the vertical direction on the base 2 and is extended in the horizontal direction on the installation base 3. Arms 18 and 19 are provided, and rods 16 and 17 are inserted into the left and right ends of arms 18 and 19 so as to be movable up and down.

そのため、上記構成のプロペラ特性測定装置１では、プロペラ８の回動によって生じる回転力を強固に抑制し、昇降可能かつ回動不能の状態を保持することができ、プロペラ８の特性を正確に計測することができる。   Therefore, in the propeller characteristic measuring apparatus 1 having the above-described configuration, the rotational force generated by the rotation of the propeller 8 can be strongly suppressed, and the state where the propeller 8 can be moved up and down and cannot be rotated can be maintained, and the characteristics of the propeller 8 can be accurately measured. can do.

また、上記プロペラ特性測定装置１は、設置台３の上方に、測定対象と成るプロペラ８と対向する他のプロペラ23をモータ24に装着した状態で設置するための他の設置台27を上下位置変更可能に設けた構成としている。   Further, the propeller characteristic measuring apparatus 1 has another installation stand 27 for installing another propeller 23 facing the propeller 8 to be measured mounted on the motor 24 above the installation stand 3 in the vertical position. It is configured to be changeable.

そのため、上記構成のプロペラ特性測定装置１では、２個のプロペラ8,23を上下に対向させて配置した２重反転プロペラ構造におけるプロペラ８の特性や上下のプロペラ8,23の間の最適な距離等をも計測することができる。   Therefore, in the propeller characteristic measuring apparatus 1 having the above-described configuration, the characteristics of the propeller 8 and the optimum distance between the upper and lower propellers 8 and 23 in the double inverted propeller structure in which the two propellers 8 and 23 are arranged to face each other. Etc. can also be measured.

１ プロペラ特性測定装置 ２ 基台
３ 設置台 ４ ガイド機構
５ 床 ６ フレーム
７ 支持体 ８ プロペラ
９ モータ 10 浮上力センサ
11 ステータ 12 ロータ
13 回転軸 14 移動量センサ
16,17 ロッド 18,19 アーム
20 コントローラ 21 ドライバー回路
22 駆動電力センサ 23 プロペラ
24 モータ 25,26 ロッド
27 設置台 DESCRIPTION OF SYMBOLS 1 Propeller characteristic measuring device 2 Base 3 Installation stand 4 Guide mechanism 5 Floor 6 Frame 7 Support body 8 Propeller 9 Motor 10 Levitation force sensor
11 Stator 12 Rotor
13 Rotating shaft 14 Travel distance sensor
16,17 Rod 18,19 Arm
20 Controller 21 Driver circuit
22 Drive power sensor 23 Propeller
24 Motor 25, 26 Rod
27 Installation base

Claims (3)

基台に、プロペラを装着したモータを設置するための設置台を、基台に対して設置台が昇降可能かつ回動不能にガイドするためのガイド機構を介して設けるとともに、プロペラの回転方向の移動量を検出するための移動量センサと、モータに供給される駆動電力を検出するための駆動電力センサと、モータによる浮上力を検出するための浮上力センサとをコントローラに接続し、コントローラでプロペラをモータに装着した状態における特性を計測可能としたことを特徴とするプロペラ特性測定装置。   An installation base for installing a motor equipped with a propeller is provided on the base via a guide mechanism for guiding the installation base so that the installation base can be raised and lowered with respect to the base and cannot rotate. A movement amount sensor for detecting movement amount, a driving power sensor for detecting driving power supplied to the motor, and a levitation force sensor for detecting levitation force by the motor are connected to the controller. A propeller characteristic measuring device characterized in that it can measure characteristics when the propeller is mounted on a motor. 前記ガイド機構は、基台に上下方向へ向けて伸延させた左右一対のロッドを設けるとともに、設置台に左右方向へ向けて伸延させたアームを設け、アームの左右端部にロッドを昇降可能に挿通させたことを特徴とする請求項１に記載のプロペラ特性測定装置。   The guide mechanism is provided with a pair of left and right rods extended in the vertical direction on the base, and an arm extended in the horizontal direction on the installation base, so that the rod can be raised and lowered at the left and right ends of the arm. The propeller characteristic measuring device according to claim 1, wherein the propeller characteristic measuring device is inserted. 前記設置台の上方に、前記プロペラと対向する他のプロペラをモータに装着した状態で設置するための他の設置台を上下位置変更可能に設けたことを特徴とする請求項１又は請求項２に記載のプロペラ特性測定装置。   The other installation base for installing in the state which mounted | wore the motor with the other propeller facing the said propeller was provided above the said installation base so that a vertical position change is possible. The propeller characteristic measuring device described in 1.
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CN106516160B (en) * 2016-12-12 2018-11-23 哈尔滨理工大学 A kind of remote-controlled test device of rotor lift parameter
CN106516160A (en) * 2016-12-12 2017-03-22 哈尔滨理工大学 Remote control testing device for rotor lift force parameters
CN106772043A (en) * 2016-12-26 2017-05-31 歌尔科技有限公司 Unmanned plane propeller detecting device for motor and method
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KR102064491B1 (en) * 2017-11-09 2020-01-10 주식회사 피스퀘어 Drone with Safety Monitoring Function
CN107839897A (en) * 2017-11-15 2018-03-27 深圳市科比特航空科技有限公司 The disconnected oar test device of unmanned plane
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CN108327925B (en) * 2017-12-14 2021-05-28 中国航空工业集团公司上海航空测控技术研究所 Simulation platform for detecting rotor cone and dynamic balancing instrument
CN108327925A (en) * 2017-12-14 2018-07-27 中国航空工业集团公司上海航空测控技术研究所 A kind of emulation platform for track-height and dynamic balance instrument detection
CN108820248A (en) * 2018-05-29 2018-11-16 上海歌尔泰克机器人有限公司 A kind of unmanned plane dynamical system test platform
CN109000841A (en) * 2018-08-24 2018-12-14 中国兵器工业计算机应用技术研究所 A kind of general tensile test tooling rack of propeller
CN109436376A (en) * 2018-12-29 2019-03-08 深圳市赛为智能股份有限公司 Devices and methods therefor for unmanned plane propeller tensile test
CN109436376B (en) * 2018-12-29 2023-12-22 深圳市赛为智能股份有限公司 Device and method for testing pull force of propeller of unmanned aerial vehicle
JP2021031008A (en) * 2019-08-29 2021-03-01 株式会社デンソー Operation checking device of electric vertical takeoff and landing machine
WO2021039502A1 (en) * 2019-08-29 2021-03-04 株式会社デンソー Operation confirmation device for electrical vertical take-off/landing aircraft
JP7234865B2 (en) 2019-08-29 2023-03-08 株式会社デンソー Equipment for checking the operation of electric vertical take-off and landing aircraft
WO2023106535A1 (en) * 2021-12-08 2023-06-15 에디슨모터스 주식회사 Apparatus for testing motor thrust
CN114199544A (en) * 2021-12-14 2022-03-18 王陆峰 Propeller test bench capable of detecting three-dimensional pulling pressure

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