JPH0446799Y2 - - Google Patents
Info
- Publication number
- JPH0446799Y2 JPH0446799Y2 JP7670986U JP7670986U JPH0446799Y2 JP H0446799 Y2 JPH0446799 Y2 JP H0446799Y2 JP 7670986 U JP7670986 U JP 7670986U JP 7670986 U JP7670986 U JP 7670986U JP H0446799 Y2 JPH0446799 Y2 JP H0446799Y2
- Authority
- JP
- Japan
- Prior art keywords
- motor
- propeller
- aircraft
- airplane
- battery
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired
Links
- 230000008054 signal transmission Effects 0.000 description 2
- 230000000630 rising effect Effects 0.000 description 1
Landscapes
- Toys (AREA)
Description
【考案の詳細な説明】
「産業上の利用分野」
本考案は電池に連なるモータによる動力装置と
無線の遠隔操作機構を具えてなる模型飛行機に関
し、とくに上記モータを1チヤンネルの信号によ
つて遠隔操作する様にして構造を簡易化した模型
飛行機を提供するものである。[Detailed Description of the Invention] "Industrial Application Field" The present invention relates to a model airplane that is equipped with a power device using a motor connected to a battery and a wireless remote control mechanism, and in particular, the invention relates to a model airplane that is equipped with a power device using a motor connected to a battery and a wireless remote control mechanism. To provide a model airplane whose structure is simplified so that it can be operated.
「従来の技術」
従来、機体11内に電池とこれに連なるモータ
12を具え、これをプロペラ13の動力装置とし
た模型飛行機において動力飛行時にプロペラ13
の回転によるトルクの反作用とプロペラ後流の影
響を打ち消すためにモータ12の出力軸X1を機
軸線Xにたいして角度θ(例えば略2度程度右方
向)に傾けていた。またこれに無線操縦装置を構
成する場合、主翼もしくは尾翼を動かして機体の
飛行姿勢を制御するための操作機構を構成すると
ともに上記モータの出力を調節して飛行高度を調
節するための操作装置を構成していた。``Prior Art'' Conventionally, in a model airplane that includes a battery and a motor 12 connected to the battery in the fuselage 11, and uses this as a power device for the propeller 13, the propeller 13 is operated during powered flight.
The output shaft X1 of the motor 12 is tilted at an angle θ (for example, approximately 2 degrees to the right) with respect to the machine axis line X in order to cancel out the torque reaction caused by the rotation of the motor and the influence of the propeller wake. In addition, when a radio control device is configured in this, an operating mechanism is configured to control the flight attitude of the aircraft by moving the main wings or tail, and an operating device is also provided to adjust the output of the motor to adjust the flight altitude. It was composed.
「考案が解決しようとする問題点」
しかしながら上記従来型の模型飛行機の構造に
よると、無線操縦装置として最も簡単な回路を採
用するとしても、独立した信号の伝送路として少
なくとも2チヤンネルが必要であり、したがつて
夫々のチヤンネルにたいしてサーボ機構が付属す
るので構造が複雑となり、部品点数も多く組立が
面倒でコスト高となるとともに、相対的に重量が
重くなり、飛行性能も阻害される等の欠点を有し
ていた。``Problem that the invention aims to solve'' However, according to the structure of the conventional model airplane mentioned above, even if the simplest circuit is adopted as a radio control device, at least two channels are required as independent signal transmission paths. Therefore, since a servo mechanism is attached to each channel, the structure becomes complicated, the number of parts is large, and assembly is troublesome, resulting in high cost.In addition, the weight becomes relatively heavy, and flight performance is hindered. It had
「問題点を解決するための手段」
本考案は上記従来型の欠点を除去するものであ
つて、機体にたいして固定された主翼と尾翼と、
電池およびスイツチ素子を介して連なるモータを
具えてなる模型飛行機において、上記スイツチ素
子には無線による1チヤンネルの遠隔操作機構を
具えてなり、かつ上記モータはプロペラを駆動す
るための出力軸を機体の機軸線に略平行させてな
るものである。"Means for Solving the Problems" The present invention eliminates the drawbacks of the conventional type described above, and includes a main wing and a tail fixed to the aircraft body,
In a model airplane equipped with a motor connected via a battery and a switch element, the switch element is equipped with a wireless one-channel remote control mechanism, and the motor connects an output shaft for driving a propeller to the aircraft body. It is approximately parallel to the machine axis.
「作用」
上記の構成において、スイツチ素子は無線の1
チヤンネルの遠隔操作機構によつて簡単に操作す
ることができ、この操作によつて少なくともモー
タの動力をオン、オフして推力を切替え飛行高度
を調節することができる。しかもこのモータのプ
ロペラを駆動するための出力軸を機体の機軸線に
略平行させることにより、モータの回転時にトル
クの反作用とプロペラ後流の影響を受けて機体が
例えば若干左の方向に旋回する飛行特性を示し、
この動力飛行時の飛行特性を利用して機体の向き
を変えて飛行させることができる。"Operation" In the above configuration, the switch element is
It can be easily operated by a remote control mechanism of the channel, and by this operation, at least the power of the motor can be turned on and off, the thrust can be switched, and the flight altitude can be adjusted. Furthermore, by arranging the output shaft for driving the propeller of this motor approximately parallel to the axis of the aircraft, the aircraft turns slightly to the left due to the reaction of the torque and the wake of the propeller when the motor rotates. Indicates flight characteristics,
Utilizing this flight characteristic during powered flight, it is possible to change the direction of the aircraft and fly it.
「実施例」
以下図に示す一実施例について本考案を説明す
ると、1は模型飛行機の機体であつて、同機体1
には固定された主翼2と尾翼3を具え、同機体1
内には電池4と、これに連なるスイツチ素子を含
む制御器5およびモータ6と、上記制御器5にた
いする遠隔制御のための1チヤンネルの受信機7
を設けている。また上記モータ6にはプロペラ8
を装設するとともに、その出力軸を61を機体1
の機軸線Xにたいして略平行させている。``Example'' The present invention will be explained with reference to an example shown in the figure below. 1 is the fuselage of a model airplane;
is equipped with fixed main wings 2 and tail 3, and the aircraft 1
Inside are a battery 4, a controller 5 including a switch element connected thereto, a motor 6, and a one-channel receiver 7 for remote control of the controller 5.
has been established. In addition, the motor 6 has a propeller 8.
At the same time, the output shaft 61 is connected to the fuselage 1.
It is made substantially parallel to the machine axis line X.
以上の様な構成により、上記受信機7にたいす
る送信機9を操作することにより、同受信機7を
介して所要の信号を受け、同信号に基いて上記制
御器5のスイツチ素子がオンオフ制御され、これ
に連なる電池4の電力によりモータ6をオンオフ
制御することができる。 With the above configuration, by operating the transmitter 9 for the receiver 7, a required signal is received via the receiver 7, and the switch element of the controller 5 is controlled to turn on and off based on the signal. , the motor 6 can be controlled on and off by the power of the battery 4 connected thereto.
しかして同モータ6が回動するとき、第2図a
の様に、モータ6のトルクの反作用とプロペラ後
流の影響を受け、プロペラ8の回転と反対方向の
力が作用して機体1は上昇しながら左方向に旋回
させることができる。 However, when the motor 6 rotates, as shown in FIG.
Under the influence of the reaction of the torque of the motor 6 and the wake of the propeller, a force in the opposite direction to the rotation of the propeller 8 acts, and the aircraft 1 can turn to the left while rising.
つぎに同モータ6が停止すると、第2図bの様
に上記モータの回転によるトルクの反作用とプロ
ペラ後流の影響がなくなり、プロペラ8は風を受
けてフリー回転するとともに機体1は滑空しなが
ら直進して降下する。 Next, when the motor 6 stops, as shown in Figure 2b, the torque reaction due to the rotation of the motor and the influence of the propeller wake disappear, and the propeller 8 rotates freely due to the wind, and the aircraft 1 continues to glide. Go straight and descend.
「考案の効果」
以上の様に1チヤンネルの遠隔操作装置によつ
てモータをオンオフ制御するだけで、モータの回
動時に機体を上昇旋回し、同モータの停止時に機
体を直進降下させることができる。これによつて
このモータのオン、オフのタイミングを調整する
ことにより、機体を任意に上昇、降下させるとと
もにその上昇時の旋回を利用して任意の方向旋回
飛行させることができる。``Effect of the invention'' As described above, by simply controlling the motor on and off using a single-channel remote control device, the aircraft can ascend and turn when the motor rotates, and descend in a straight line when the motor stops. . By adjusting the on/off timing of this motor, the aircraft can be raised or lowered as desired, and the aircraft can be made to fly in any direction using the turning during the ascent.
また上記の構成において、モータをオン、オフ
制御するだけでよいので遠隔制御の信号伝送路は
1チヤンネルでよく、構造が極めて簡単になり部
品点数も少なくなり組立が簡易化され、コストを
低減できるとともに、相対的に重量が軽くなり、
飛行性能も向上させることができる。 In addition, in the above configuration, since it is only necessary to control the motor on and off, the signal transmission path for remote control only needs to be one channel, which simplifies the structure, reduces the number of parts, simplifies assembly, and reduces costs. At the same time, the weight becomes relatively lighter,
Flight performance can also be improved.
第1図は本考案の一実施例を示す模型飛行機の
斜視図、第2図は同じく飛行時のモータのオン、
オフに伴う飛行姿勢の説明図、第3図は同じく機
体の機首部の要部平面図、第4図は従来型の模型
飛行機の機首部の要部平面図である。
同図中、1は機体、2は主翼、3は尾翼、4は
電池、5は制御器、6はモータ、7は受信機、8
はプロペラ、61は出力軸、Xは機軸線である。
FIG. 1 is a perspective view of a model airplane showing an embodiment of the present invention, and FIG.
FIG. 3 is a plan view of the main part of the nose of the aircraft, and FIG. 4 is a plan view of the main part of the nose of a conventional model airplane. In the figure, 1 is the fuselage, 2 is the main wing, 3 is the tail, 4 is the battery, 5 is the controller, 6 is the motor, 7 is the receiver, 8
is a propeller, 61 is an output shaft, and X is a machine axis line.
Claims (1)
およびスイツチ素子を介して連なるモータを具え
てなる模型飛行機において、上記スイツチ素子に
は無線による1チヤンネルの遠隔操作機構を具え
てなり、かつ上記モータはプロペラを駆動するた
めの出力軸を機体の機軸線に略平行されてなるこ
とを特徴とする模型飛行機。 In a model airplane comprising a main wing and a tail fixed to the fuselage, and a motor connected via a battery and a switch element, the switch element is equipped with a wireless one-channel remote control mechanism, and the motor is connected to a propeller. A model airplane characterized in that an output shaft for driving the airplane is substantially parallel to the axis of the airplane.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP7670986U JPH0446799Y2 (en) | 1986-05-21 | 1986-05-21 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP7670986U JPH0446799Y2 (en) | 1986-05-21 | 1986-05-21 |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS62186798U JPS62186798U (en) | 1987-11-27 |
| JPH0446799Y2 true JPH0446799Y2 (en) | 1992-11-04 |
Family
ID=30924046
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP7670986U Expired JPH0446799Y2 (en) | 1986-05-21 | 1986-05-21 |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH0446799Y2 (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP4130209B2 (en) * | 2006-01-24 | 2008-08-06 | 株式会社タカラトミー | Propeller airplane toy |
-
1986
- 1986-05-21 JP JP7670986U patent/JPH0446799Y2/ja not_active Expired
Also Published As
| Publication number | Publication date |
|---|---|
| JPS62186798U (en) | 1987-11-27 |
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