JP5238049B2 - Remote control helicopter operation training device - Google Patents

Remote control helicopter operation training device Download PDF

Info

Publication number
JP5238049B2
JP5238049B2 JP2011038313A JP2011038313A JP5238049B2 JP 5238049 B2 JP5238049 B2 JP 5238049B2 JP 2011038313 A JP2011038313 A JP 2011038313A JP 2011038313 A JP2011038313 A JP 2011038313A JP 5238049 B2 JP5238049 B2 JP 5238049B2
Authority
JP
Japan
Prior art keywords
mast
helicopter
tilt
buffer member
training device
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 - Fee Related
Application number
JP2011038313A
Other languages
Japanese (ja)
Other versions
JP2012170776A (en
Inventor
俊一 鈴木
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Hirobo Ltd
Original Assignee
Hirobo Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Hirobo Ltd filed Critical Hirobo Ltd
Priority to JP2011038313A priority Critical patent/JP5238049B2/en
Publication of JP2012170776A publication Critical patent/JP2012170776A/en
Application granted granted Critical
Publication of JP5238049B2 publication Critical patent/JP5238049B2/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Landscapes

  • Toys (AREA)

Description

本発明は、遠隔操縦式ヘリコプタ（ラジオコントロールヘリコプタ、以下、「Ｒ／Ｃヘリ」という）を一定の姿勢に保持するホバリングを練習するために使用されるＲ／Ｃヘリの操縦練習装置に関する。   The present invention relates to an R / C helicopter training practice device used for practicing hovering in which a remotely controlled helicopter (radio control helicopter, hereinafter referred to as “R / C helicopter”) is held in a fixed posture.

Ｒ／Ｃヘリを墜落させることなく、ホバリングの練習をするための装置として、例えば図８に示される構成のものが知られている。
この装置は、脚体１０１で支持されるベース板１０２上に、外周にスリーブ１０３がスライド自在に取付けられた銅棒１０４をボール継手１０５で傾倒自在に取付け、スリーブ１０３の上端部にはＲ／Ｃヘリ１００の機体下部に接続する組立板１０６をボール継手１０７を介して連結し、前記ベース板１０２の上方に円形孔１０８ａが中央に形成された輪郭フレーム１０８を取付けてなり、前記組立板１０６にＲ／Ｃヘリ１００の機体下部を取付けてＲ／Ｃヘリ１００をスリーブ１０３の上端でロール、ピッチ及びヨ−の各軸廻りで揺動可能に支持するとともに、起動したＲ／Ｃヘリ１００を銅棒１０４に沿ってスリーブ１０３がスライドする範囲で上下動させ、且つ輪郭フレーム１０８の円形孔１０８ａ内で側方へ移動させることができるように構成されている。
また、スリーブ１０３の周囲に複数のバネ１０９を取付けてスリーブ１０３を倒れ難くすることで、Ｒ／Ｃヘリ１００が前後左右方向へ急激に移動したときの勢いを緩衝するように設けてある（例えば特許文献１参照）。 As a device for practicing hovering without causing the R / C helicopter to crash, for example, a device having the configuration shown in FIG. 8 is known.
In this apparatus, on a base plate 102 supported by a leg 101, a copper rod 104 having a sleeve 103 slidably mounted on its outer periphery is slidably mounted by a ball joint 105, and an R / R is attached to the upper end of the sleeve 103. An assembly plate 106 connected to the lower part of the C helicopter 100 is connected via a ball joint 107, and a contour frame 108 having a circular hole 108a formed in the center is attached above the base plate 102. The lower part of the R / C helicopter 100 is attached to the R / C helicopter 100, and the R / C helicopter 100 is supported at the upper end of the sleeve 103 so as to be swingable around the roll, pitch and yaw axes. The sleeve 103 can be moved up and down within a range in which the sleeve 103 slides along the copper rod 104, and can be moved laterally within the circular hole 108a of the contour frame 108. Is constructed sea urchin.
Further, by attaching a plurality of springs 109 around the sleeve 103 so that the sleeve 103 does not easily fall over, the moment when the R / C helicopter 100 suddenly moves in the front-rear and left-right directions is provided to buffer the momentum (for example, Patent Document 1).

特開昭５３−１２３２４４号公報JP-A-53-123244

図示した操縦練習装置は、スリーブ１０３が輪郭フレーム１０８の円形孔１０８ａの縁部に当たる位置まで傾倒可能に取付けられて、ベース板１０２上でのＲ／Ｃヘリ１００の浮上高さに関わりなく、前記スリーブ１０３の傾倒可能な範囲でＲ／Ｃヘリ１００が前後左右に移動できるように設けてある。
そのため、Ｒ／Ｃヘリ１００の起動直後に機体が傾いていると、Ｒ／Ｃヘリ１００が傾いた方向に流れて大きく変位してしまい、Ｒ／Ｃヘリ１００を操縦するコントローラの操作に慣れない初心者にとってＲ／Ｃヘリ１００をベース板１０２上で徐々に浮上させて同位置にとどまるように操作することは難しかった。
この場合、スリーブ１０２に複数のバネ１０９を取付けてスリーブ１０３が倒れ難くしてあれば、Ｒ／Ｃヘリ１００が起動直後に大きく流れて変位することはないが、スリーブ１０３に対するバネ１０９の取付け位置は段階的に変えることしかできず、また、前記図８（Ｂ）に示されるように、バネ１０９の取付け位置によってはＲ／Ｃヘリ１００が上昇した際にスリーブ１０３からバネ１０９が外れてしまうことがある。 The illustrated pilot training device is attached so that the sleeve 103 can be tilted to a position where it comes into contact with the edge of the circular hole 108a of the contour frame 108, regardless of the flying height of the R / C helicopter 100 on the base plate 102. The R / C helicopter 100 is provided so that it can move back and forth and right and left within a range in which the sleeve 103 can be tilted.
Therefore, if the fuselage is tilted immediately after activation of the R / C helicopter 100, the R / C helicopter 100 flows in the tilted direction and is greatly displaced, and is unaccustomed to the operation of the controller that controls the R / C helicopter 100. It has been difficult for beginners to operate the R / C helicopter 100 so that it gradually floats on the base plate 102 and stays at the same position.
In this case, if the plurality of springs 109 are attached to the sleeve 102 so that the sleeve 103 does not easily fall down, the R / C helicopter 100 does not flow greatly and is displaced immediately after activation, but the attachment position of the spring 109 with respect to the sleeve 103 8 can only be changed stepwise, and as shown in FIG. 8B, depending on the mounting position of the spring 109, the spring 109 is detached from the sleeve 103 when the R / C helicopter 100 is raised. Sometimes.

また何より、スリーブ１０３の周囲四方にバネ１０９を取付けたのでは、Ｒ／Ｃヘリ１００の変位に連動してスリーブ１０３が傾倒したときにこれを引き戻す方向に常にバネ１０９の弾性力が作用するため、換言すればＲ／Ｃヘリ１００は前後左右に移動した際にバネ１０９により移動方向とは反対方向の力を常に受けるため、コントローラの操作によるＲ／Ｃヘリ１００の実際の制御量と装置上でのＲ／Ｃヘリ１００の挙動とにズレが生じることは避けられない。
図示した装置では、「エルロン」、「エレベータ」の「当て舵」の適正な操作技術を習得することはできない。 Above all, when the springs 109 are attached to the four sides around the sleeve 103, the elastic force of the springs 109 always acts in the direction in which the sleeve 103 is pulled back in response to the displacement of the R / C helicopter 100. In other words, since the R / C helicopter 100 always receives a force in the direction opposite to the moving direction by the spring 109 when it moves back and forth, left and right, the actual control amount of the R / C helicopter 100 by the operation of the controller and on the device It is inevitable that the R / C helicopter 100 behaves in a different manner.
With the illustrated apparatus, it is not possible to learn proper operation techniques for “aileron” and “elevator” “slider”.

本発明は従来技術の有するこのような問題点に鑑み、Ｒ／Ｃヘリの操縦練習装置において、初心者から熟練者までＲ／Ｃヘリの機体を損傷させることなく安全にホバリングの練習を行え、Ｒ／Ｃヘリの操縦技術を適正に習得することができるようにすることを課題とする。   In view of such problems of the prior art, the present invention can safely practice hovering without damaging the R / C helicopter from beginners to experts in the R / C helicopter training practice device. It is an object to be able to properly acquire / C helicopter maneuvering technology.

前記課題を解決するため本発明は、基台の上面に形成された開口部に、一端に球面軸受けを介して機体スタンドが連結され、他端にストッパが取付けられたマストを通し、開口部内でマストを上下移動及び傾倒自在に支持して構成されるＲ／Ｃヘリの操縦練習装置において、前記開口部の下側にマストの傾倒範囲を制限するスカート状の筒材からなる傾倒規制体が取付けられ、この傾倒規制体内にマストを通して構成されていることを特徴とする。   In order to solve the above-mentioned problems, the present invention passes a mast in which an airframe stand is connected to an opening formed on the upper surface of a base via a spherical bearing at one end and a stopper is attached to the other end. In an R / C helicopter practice training device configured to support the mast so that it can be moved up and down and tilted, a tilt restricting body made of a skirt-like tubular member for limiting the tilt range of the mast is attached to the lower side of the opening. It is characterized in that it is configured through a mast in this tilt regulating body.

これによれば、Ｒ／Ｃヘリの脚部を構成するスキッドに機体スタンドを接続し、Ｒ／Ｃヘリを基台に載せた状態でＲ／Ｃヘリを起動し、コントローラを操作してＲ／Ｃヘリを浮上させてホバリングの練習をすることができる。
Ｒ／Ｃヘリのスキッドに接続した機体スタンドは球面軸受けを介してマストに連結しているので、マストの上端においてＲ／Ｃヘリはロール、ピッチ及びヨ−の各軸廻りに揺動可能であり、また、基台上にＲ／Ｃヘリを載せた位置からストッパでマストの上方変位が制限される位置までＲ／Ｃヘリを上下動させるとともに、開口部の中心を通る鉛直軸線廻りでマストが傾倒する範囲で、浮上させたＲ／Ｃヘリを前後左右に移動させることができる。
そして、開口部の下側にマストの傾倒範囲を制限する傾倒規制体が取付けてあるので、Ｒ／Ｃヘリの前後左右方向の移動はマストの傾倒が傾倒規制体によって規制される位置までの範囲に制限され、さらに、この傾倒規制体がスカート状の筒体からなるので、Ｒ／Ｃヘリの前後左右方向の変位量は浮上したＲ／Ｃヘリが低いときは小さく、高いときには大きくなり、Ｒ／Ｃヘリを起動した直後、つまり浮上位置が低いときに機体の位置が前後左右に大きく流れるようなことはない。 According to this, the fuselage stand is connected to the skid constituting the legs of the R / C helicopter, the R / C helicopter is activated with the R / C helicopter mounted on the base, and the controller is operated to operate the R / C helicopter. C helicopter can be lifted to practice hovering.
Since the airframe stand connected to the ski of the R / C helicopter is connected to the mast via a spherical bearing, the R / C helicopter can swing around the roll, pitch and yaw axes at the upper end of the mast. In addition, the R / C helicopter is moved up and down from the position where the R / C helicopter is placed on the base to a position where the upper displacement of the mast is restricted by the stopper, and the mast is moved around the vertical axis passing through the center of the opening. The lifted R / C helicopter can be moved back and forth and left and right within a tilting range.
Since the tilt restricting body for limiting the tilt range of the mast is attached to the lower side of the opening, the movement of the R / C helicopter in the front-rear and left-right directions is a range up to the position where the tilt of the mast is regulated by the tilt restricting body Further, since the tilt restricting body is formed of a skirt-shaped cylinder, the amount of displacement in the front / rear and left / right directions of the R / C helicopter is small when the R / C helicopter is low, and is large when the R / C helicopter is high. / C The helicopter does not flow forward, backward, left and right immediately after the helicopter is activated, that is, when the flying position is low.

前記構成において、傾倒規制体内に、傾倒するマストに抵抗を加えてマストが傾倒することを抑制する傾倒抑制機構を設けることが好ましい。
これによれば、マストが傾倒しようとすると傾倒抑制機構が傾倒を抑制するようにマストに抵抗を加えるので、Ｒ／Ｃヘリが前後左右方向へ変位するのに伴ってマストが傾倒したときにマストを介して傾倒抑制機構による抵抗がＲ／Ｃヘリに作用し、変位する勢いが緩衝されて機体の動作安定性が高まり、コントローラで「エルロン」、「エレベータ」の「当て舵」をしたときの操作感覚を容易に習得することができる。 In the above-described configuration, it is preferable that a tilt suppression mechanism is provided in the tilt regulating body to prevent the mast from tilting by adding resistance to the tilting mast.
According to this, when the mast is tilted, the tilt suppression mechanism adds resistance to the mast so that the tilt is suppressed. Therefore, when the mast tilts as the R / C helicopter is displaced in the front / rear / left / right direction, the mast is tilted. When the resistance by the tilt suppression mechanism acts on the R / C helicopter via the dam, the momentum of the displacement is buffered and the operational stability of the fuselage is increased, and when the “aileron” and “elevator” “steer” are controlled by the controller The operation feeling can be easily learned.

前記傾倒抑制機構は、傾倒規制体内に着脱自在に設けることが好ましく、例えば中央に上下に貫通する通孔を有し、外周面が傾倒規制体の内面に接合するように形成された適宜な厚みの緩衝部材と、前記通孔にマストを通してこの緩衝部材を傾倒規制体内に保持する保持部材とで、前記緩衝部材の保持位置をマストに沿って調節可能に設けた構成とするのが好ましい。
前記緩衝部材としては、合成樹脂材やゴム材などの弾性を有する収縮自在な部材を用い、スポンジを用いることがより好ましい。
これによれば、傾倒規制体内で傾倒抑制機構の保持位置を適宜に変えることで傾倒抑制機構が傾倒するマストに及ぼす抵抗力が変わり、それによりＲ／Ｃヘリが前後左右に変位したときの機体の動作安定性が調整され、Ｒ／Ｃヘリの操縦の習熟度に応じた機体の動作安定性を簡単に設定して操縦練習をすることが可能である。 The tilt suppressing mechanism is preferably provided detachably in the tilt regulating body, for example, having a through-hole penetrating vertically in the center and having an appropriate thickness formed so that the outer peripheral surface is joined to the inner surface of the tilt regulating body. It is preferable that the buffer member and the holding member that holds the buffer member in the tilt regulating body through the mast through the through hole are provided so that the holding position of the buffer member can be adjusted along the mast.
As the buffer member, it is more preferable to use a contractible member having elasticity such as a synthetic resin material or a rubber material, and to use a sponge.
According to this, the resistance force exerted on the mast to which the tilt suppression mechanism tilts is changed by appropriately changing the holding position of the tilt suppression mechanism in the tilt regulating body, thereby the aircraft when the R / C helicopter is displaced back and forth and left and right It is possible to adjust the operational stability of the aircraft and easily set the operational stability of the aircraft according to the level of proficiency in the operation of the R / C helicopter.

本発明の一実施形態の操縦練習装置にＲ／Ｃヘリを接続した状態の外観図である。It is an external view of the state which connected the R / C helicopter to the piloting practice apparatus of one Embodiment of this invention. 図１の操縦練習装置の平面図（Ａ）、正面図（Ｂ）及び下側斜視図（Ｃ）である。It is the top view (A), front view (B), and lower side perspective view (C) of the steering practice apparatus of FIG. 図１の操縦練習装置の構成を示す上部断面図である。FIG. 2 is an upper cross-sectional view illustrating a configuration of the steering practice device of FIG. Ｒ／Ｃヘリに機体スタンドを接続した状態を示す外観図である。It is an external view which shows the state which connected the airframe stand to R / C helicopter. 基台の開口部の部分の拡大断面図（Ａ）とスライドガイドパイプ下端部の拡大断面図（Ｂ）である。It is the expanded sectional view (A) of the part of the opening part of a base, and the expanded sectional view (B) of a slide guide pipe lower end part. 緩衝部材の拡大外観図である。It is an expansion external view of a buffer member. マストの下端部の拡大外観図である。It is an expansion external view of the lower end part of a mast. 従来のＲ／Ｃヘリの操縦練習装置の外観図（Ａ）とその上側半面の拡大断面図である。It is the external view (A) of the conventional pilot training apparatus of R / C helicopter, and the expanded sectional view of the upper half.

本発明の好適な実施形態を図面を参照して説明する。
図１はＲ／Ｃヘリ１を本発明の一実施形態の操縦練習装置２に接続して載せた状態を示しており、本形態の操縦練習装置２は、基台３の上面に形成された開口部４ａに、Ｒ／Ｃヘリ１が上端に接続されるマスト６を通し、開口部４ａ内でマスト６を上下移動及び傾倒自在に支持して構成されている。 Preferred embodiments of the present invention will be described with reference to the drawings.
FIG. 1 shows a state in which an R / C helicopter 1 is connected to and placed on a control practice device 2 according to an embodiment of the present invention. The control practice device 2 of this embodiment is formed on the upper surface of a base 3. A mast 6 connected to the upper end of the R / C helicopter 1 is passed through the opening 4a, and the mast 6 is supported in the opening 4a so as to be movable up and down and tilted.

基台３は、平坦な上面の中央に上下に貫通する開口部４ａが形成されてなるテーブル４の下側を、三本の脚体５で適宜な高さに支持して形成されている。
各脚体５はテーブル４の下部に固着されたマウント５ａに回転自在に取付けられ、各マウント５ａに沿って各脚体５を広げた位置でテーブル４が水平に支持されるようになっている。
また、基台３の開口部４ａの下側には、後述する傾倒抑制機構１２を内部に備えた傾倒規制体９を取付けてある。 The base 3 is formed by supporting the lower side of a table 4 formed with an opening 4a penetrating vertically in the center of a flat upper surface with three legs 5 at an appropriate height.
Each leg 5 is rotatably attached to a mount 5a fixed to the lower part of the table 4, and the table 4 is horizontally supported at a position where each leg 5 is spread along each mount 5a. .
Further, a tilt restricting body 9 having a tilt suppressing mechanism 12 to be described later is attached to the lower side of the opening 4 a of the base 3.

マスト６は、適宜な長さの細い鋼製の棒体であり、その上端にＲ／Ｃヘリ１の脚体が接続する機体スタンド７が球面軸受け８を介して連結され、下端には後述するストッパ１５を一体に取付けて形成され、後述するスライドガイドパイプ１０内に挿通されて前記開口部４ａ内に上下移動及び鉛直軸廻りに傾倒し得るように取付けてある。
機体スタンド７は、図２及び図４に示されるように、平面視略々Ｈ字形の枠材であり、その中央に固着された球面軸受け８のホルダ８ｂで、マスト６の上端に取付けられた球面軸受け８の内輪８ａを包持してマスト６の上端に連結させ、前記枠材の左右のステー７ａ、７ａにＲ／Ｃヘリ１の脚部を構成するスキッドをそれぞれ接続して、Ｒ／Ｃヘリ１をマスト６の上端でロール、ピッチ及びヨ−の各軸廻りに揺動可能に支持するように設けてある。 The mast 6 is a thin steel rod having an appropriate length, and an airframe stand 7 to which the leg of the R / C helicopter 1 is connected is connected to the upper end of the mast 6 via a spherical bearing 8, and the lower end will be described later. The stopper 15 is integrally attached, and is inserted into a slide guide pipe 10 to be described later, and is attached so as to be able to move up and down and tilt around a vertical axis in the opening 4a.
As shown in FIGS. 2 and 4, the airframe stand 7 is a frame member that is substantially H-shaped in plan view, and is attached to the upper end of the mast 6 by a holder 8 b of a spherical bearing 8 fixed to the center thereof. The inner ring 8a of the spherical bearing 8 is held and connected to the upper end of the mast 6, and skids constituting the legs of the R / C helicopter 1 are connected to the left and right stays 7a and 7a of the frame member, respectively. The C helicopter 1 is provided at the upper end of the mast 6 so as to be swingable around the roll, pitch and yaw axes.

傾倒規制体９は、図２及び図３に示されるように、上部から下部に亘って内径を漸次大きくして内面が傾斜したスカート状に形成された筒体であり、その中心軸を前記開口部４ａの中心軸に合わせてテーブル４の下面に一体に取付けてあるとともに、開口部４ａ直下の上部内面に前記マスト６を支持するスライドガイドパイプ１０を球面軸受け１１を介して取付けてある。
より詳しくは、スライドガイドパイプ１０は傾倒規制体９よりも若干長い管体であり、図５（Ａ）に示されるように、その上端が、傾倒規制体９の上部内面に取付けられた球面軸受け１１のホルダ１１ｂが包持する内輪１１ａに固着され、傾倒規制体８の上部内面において前記内輪１１ａと一体に鉛直軸線廻りに適宜に回転し且つ傾斜することができるように取付けてある。
そして、図５（Ｂ）に示されるように、スライドガイドパイプ１０の上下端部に装着されたスライドガイド１０ａを挟んで内部にマスト６が挿通されて、マスト６がスライドガイドパイプ１０に沿ってスライド自在に支持されている。 As shown in FIGS. 2 and 3, the tilt restricting body 9 is a cylindrical body formed in a skirt shape in which the inner diameter is gradually increased from the upper part to the lower part and the inner surface is inclined, and the central axis thereof is the opening. The slide guide pipe 10 that supports the mast 6 is attached to the lower inner surface of the table 4 in accordance with the central axis of the portion 4a through the spherical bearing 11 on the upper inner surface directly below the opening 4a.
More specifically, the slide guide pipe 10 is a tube body slightly longer than the tilt restricting body 9, and a spherical bearing whose upper end is attached to the upper inner surface of the tilt restricting body 9 as shown in FIG. 11 is fixed to the inner ring 11a held by the holder 11b, and is attached to the upper inner surface of the tilt regulating body 8 so as to be able to rotate and tilt appropriately around the vertical axis integrally with the inner ring 11a.
Then, as shown in FIG. 5B, the mast 6 is inserted through the slide guide 10 a mounted on the upper and lower ends of the slide guide pipe 10, and the mast 6 extends along the slide guide pipe 10. It is slidably supported.

さらに、傾倒規制体９の内部には、傾倒規制体９内でスライドガイドパイプ１０と一体にマスト６が傾倒することを抑制する、適宜な厚みのスポンジからなる緩衝部材１３とこれを傾倒規制体９内に保持する保持部材１４からなる傾倒抑制機構１２を取付けてある。
より詳しくは、緩衝部材１３はポリウレタンなどの合成樹脂を発泡成形して形成される合成スポンジであり、図２及び図６に示されるように、その中央に上下に貫通する通孔１３ａを有して外周面が傾倒規制体９の下端部内面に適宜な高さで接合し得るように円錐台状に形成されており、また、保持部材１４はスライドガイドパイプ１０の外周面にスライド自在に嵌着し、その下端部に設けられた固定ネジ１４ａで位置固定される管体により形成されている。そして、上下両面にワッシャー１４ｂ、１４ｂが取付けられた緩衝部材１３をその通孔１３ａにスライドガイドパイプ１０を通し、さらにその下側でスライドガイドパイプ１０の外周面に保持部材１４を嵌着して、スライドガイドパイプ１０に沿って緩衝部材１３と保持部材１４を上下に配置し、その状態で、前記固定ネジ１４ａをスライドガイドパイプ１０の表面に締め付けることにより、保持部材１４の上端に載った緩衝部材１３の位置を固定せしめ、固定ネジ１４ａを緩めて保持部材１４をスライドガイドパイプ１０に沿ってスライドさせて、緩衝部材１３の固定位置を調節できるように設けてある。 Further, inside the tilt regulating body 9, a buffer member 13 made of a sponge having an appropriate thickness for suppressing the mast 6 from tilting integrally with the slide guide pipe 10 in the tilt regulating body 9 and the tilt regulating body 9. A tilt restraining mechanism 12 comprising a holding member 14 held in 9 is attached.
More specifically, the buffer member 13 is a synthetic sponge formed by foaming a synthetic resin such as polyurethane, and as shown in FIGS. 2 and 6, has a through hole 13a penetrating vertically in the center thereof. The outer peripheral surface is formed in a truncated cone shape so that it can be joined to the inner surface of the lower end portion of the tilt regulating body 9 at an appropriate height, and the holding member 14 is slidably fitted on the outer peripheral surface of the slide guide pipe 10. It is formed by a tubular body that is attached and fixed by a fixing screw 14a provided at the lower end thereof. Then, the buffer member 13 having the washer 14b, 14b attached to both the upper and lower surfaces is passed through the slide guide pipe 10 through the through hole 13a, and the holding member 14 is fitted to the outer peripheral surface of the slide guide pipe 10 at the lower side. The buffer member 13 and the holding member 14 are vertically arranged along the slide guide pipe 10, and in this state, the fixing screw 14 a is fastened to the surface of the slide guide pipe 10, thereby buffering the upper end of the holding member 14. The position of the member 13 is fixed, the fixing screw 14a is loosened, and the holding member 14 is slid along the slide guide pipe 10 so that the fixing position of the buffer member 13 can be adjusted.

また、図７に示されるように、前記マスト６の下端部には円柱状のストッパ１５が一体に取付けられており、このストッパ１５が前記スライドガイドパイプ１０の下端部に当接することによりマスト６の上方への移動が規制されるように設けてある。   As shown in FIG. 7, a columnar stopper 15 is integrally attached to the lower end portion of the mast 6, and the stopper 15 abuts against the lower end portion of the slide guide pipe 10, thereby Is provided so as to be restricted from moving upward.

このように構成された本形態の操縦練習装置２によれば、Ｒ／Ｃヘリ１の脚部を機体スタンド７に接続し、Ｒ／Ｃヘリ１をテーブル４に載せた状態でＲ／Ｃヘリ１を起動し、コントローラを操作してホバリングの練習をすることができる。
機体スタンド７は球面軸受け８を介してマスト６に連結しているので、マスト６の上端でＲ／Ｃヘリ１の揺動運動が可能であり、また、テーブル４上にＲ／Ｃヘリ１を載せた位置からストッパ１５でマスト６の上方変位が制限される位置までＲ／Ｃヘリ１を上下動させるとともに、開口部４ａの中心を通る鉛直軸線廻りでスライドガイドパイプ１０と一体にマスト６を傾倒させることができる範囲で、浮上させたＲ／Ｃヘリ１を前後左右に移動させることができる。 According to the control practice device 2 of the present embodiment configured as described above, the R / C helicopter 1 is connected to the body stand 7 and the R / C helicopter 1 is placed on the table 4 with the R / C helicopter 1 mounted on the table 4. 1 can be activated and the controller can be operated to practice hovering.
Since the airframe stand 7 is connected to the mast 6 via the spherical bearing 8, the R / C helicopter 1 can swing at the upper end of the mast 6, and the R / C helicopter 1 is mounted on the table 4. The R / C helicopter 1 is moved up and down from the mounted position to a position where the upper displacement of the mast 6 is restricted by the stopper 15, and the mast 6 is integrated with the slide guide pipe 10 around the vertical axis passing through the center of the opening 4a. The lifted R / C helicopter 1 can be moved back and forth and left and right within a range in which it can be tilted.

マスト６が傾倒する範囲は、前記開口部４ａの下側に取付けられたスカート状の傾倒規制体９にマスト６とともにスライドガイドパイプ１０が当接する位置までの範囲に規制されるので、コントローラの操作を誤ってもＲ／Ｃヘリ１の機体の位置が前後左右に大きく流れるようなことはない。
また、傾倒規制体９の内部には、傾倒抑制機構１２の緩衝部材１３を設置し、この緩衝部材１３がマスト６とともに傾倒するスライドガイドパイプ１０の傾倒度合いに応じて、傾倒規制体９の内面とスライドガイドパイプ１０の外周面との間で収縮することにより、Ｒ／Ｃヘリ１が前後左右方向に変位する勢いを緩衝し、機体の動作安定性を高めることができる。 The range in which the mast 6 tilts is restricted to the range up to the position where the slide guide pipe 10 abuts with the mast 6 on the skirt-like tilt regulating body 9 attached to the lower side of the opening 4a. The position of the R / C helicopter 1 body does not flow greatly forward, backward, left and right even if
In addition, a buffer member 13 of the tilt suppression mechanism 12 is installed inside the tilt restricting body 9, and the inner surface of the tilt restricting body 9 depends on the tilting degree of the slide guide pipe 10 in which the buffer member 13 tilts together with the mast 6. And the outer peripheral surface of the slide guide pipe 10 can buffer the momentum that the R / C helicopter 1 is displaced in the front-rear and left-right directions, and can improve the operational stability of the aircraft.

そして、傾倒規制体９内で緩衝部材１３の固定位置を適宜に変えることで、緩衝部材１３の収縮に伴って傾倒するマスト６に及ぼす抵抗力が適宜に調節され、これによりＲ／Ｃヘリ１が前後左右に変位したときの機体の動作安定性を調節することができる。
すなわち、図３には傾倒規制体９内の下部に緩衝部材１３を保持した状態が示されており、この状態で緩衝部材１３は「柔らかく広がった状態」なので、マスト６が傾倒して緩衝部材１３に当たったときにマスト６に加わる抵抗は小さく、そのためＲ／Ｃヘリ１の機体の動作安定性は低くなり、他方、保持部材１４を操作して傾倒規制体９内の上部に緩衝部材１３を固定した状態では、緩衝部材１３が傾倒規制体９の内周面に圧接して「硬く収縮した状態」なので、マスト６が傾倒して緩衝部材１３に当たったときにマスト６に加わる抵抗は大きくなって、Ｒ／Ｃヘリ１の機体の変動を吸収する緩衝機能が高まり、動作安定性は高くなる。
よって、緩衝部材１３の保持位置を調節して機体の動作安定性を適宜に設定することにより、Ｒ／Ｃヘリ１の操縦の習熟度に応じた操作感覚が得られ、コントローラで「エルロン」、「エレベータ」の「当て舵」をしたときの操作感覚を容易に習得することが可能である。 Then, by appropriately changing the fixing position of the buffer member 13 in the tilt restricting body 9, the resistance force exerted on the mast 6 tilting with the contraction of the buffer member 13 is adjusted as appropriate, whereby the R / C helicopter 1 is adjusted. It is possible to adjust the operational stability of the aircraft when it is displaced back and forth and left and right.
That is, FIG. 3 shows a state in which the buffer member 13 is held in the lower part of the tilt regulating body 9, and since the buffer member 13 is in a “softly spread state” in this state, the mast 6 tilts and the buffer member is tilted. 13, the resistance applied to the mast 6 is small, so that the operational stability of the airframe of the R / C helicopter 1 is lowered. On the other hand, the holding member 14 is operated and the shock absorber 13 Since the buffer member 13 is in a “hardly contracted state” by pressing against the inner peripheral surface of the tilt regulating body 9 in a state where the mast 6 is fixed, the resistance applied to the mast 6 when the mast 6 tilts and hits the buffer member 13 is As it becomes larger, the buffer function that absorbs the fluctuations in the airframe of the R / C helicopter 1 increases, and the operational stability increases.
Therefore, by adjusting the holding position of the buffer member 13 and appropriately setting the operational stability of the aircraft, an operational sensation according to the mastery of the operation of the R / C helicopter 1 can be obtained. It is possible to easily learn the operational feeling when performing the “elevator” of “elevator”.

なお、図示した操縦練習装置２は本発明の実施形態の一例を示すものであり、本発明はこれに限定されない。
傾倒規制体９は、内面の傾斜角度が異なるものを幾つか取り揃え、操縦の習熟度に応じて適宜なものを選択してテーブル４の下部に取付けることでマスト６の傾倒範囲を調節できるようにしてもよい。傾倒抑制機構１２を構成する緩衝部材１３としてのスポンジは、合成スポンジの他に天然のスポンジを用いてもよく、緩衝部材１３としてスポンジの代わりに適宜に収縮する他の弾性部材を用いてもよい。また、操縦の熟練者であれば、傾倒抑制機構１２をスライドガイドパイプ１０から取り外して使用してもよい。 In addition, the illustrated piloting practice apparatus 2 shows an example of an embodiment of the present invention, and the present invention is not limited to this.
The tilt restricting body 9 has several types with different inner surface tilt angles, and an appropriate one is selected according to the skill level of operation and attached to the lower part of the table 4 so that the tilt range of the mast 6 can be adjusted. May be. The sponge as the buffer member 13 constituting the tilt suppressing mechanism 12 may be a natural sponge in addition to the synthetic sponge, or another elastic member that contracts appropriately instead of the sponge as the buffer member 13. . Moreover, if it is an expert of steering, you may remove and use the tilt suppression mechanism 12 from the slide guide pipe 10. FIG.

１ Ｒ／Ｃヘリ、２ 操縦練習装置、３ 基台、４ テーブル、３ａ 開口部、５ 脚体、５ａ マウント、６ マスト、７ 機体スタンド、８ 球面軸受け、９ 傾倒規制体、１０ スライドガイドパイプ、１１ 球面軸受け、１２ 傾倒抑制機構、１３ 緩衝部材、１４ 保持部材、１５ ストッパ

1 R / C helicopter, 2 pilot training device, 3 base, 4 table, 3a opening, 5 legs, 5a mount, 6 mast, 7 airframe stand, 8 spherical bearing, 9 tilt regulating body, 10 slide guide pipe, 11 Spherical bearing, 12 Tilt suppression mechanism, 13 Buffer member, 14 Holding member, 15 Stopper

Claims (4)

基台（３）の上面に形成された開口部（４ａ）に、一端に球面軸受け（８）を介して機体スタンド（７）が連結され、他端にストッパ（１５）が取付けられたマスト（６）を通し、開口部（４ａ）内でマスト（６）を上下移動及び傾倒自在に支持して構成される遠隔操縦式ヘリコプタの操縦練習装置（２）において、
前記開口部（４ａ）の下側にマスト（６）の傾倒範囲を制限するスカート状の筒体からなる傾倒規制体（９）が取付けられ、この傾倒規制体（９）内にマスト（６）を通して構成されていることを特徴とする遠隔操縦式ヘリコプタの操縦練習装置。 A mast with an airframe stand (7) connected to one end via a spherical bearing (8) and an stopper (15) attached to the other end to an opening (4a) formed on the upper surface of the base (3). 6), in the pilot training device (2) of the remotely controlled helicopter configured to support the mast (6) vertically movable and tiltable in the opening (4a),
A tilt restricting body (9) made of a skirt-like cylinder that restricts the tilt range of the mast (6) is attached to the lower side of the opening (4a), and the mast (6) is placed in the tilt restricting body (9). Remote control helicopter operation training device, characterized by being configured through. 傾倒規制体（９）内に、傾倒するマスト（６）に抵抗を加えてマスト（６）が傾倒することを抑制する傾倒抑制機構（１２）を設けた構成を有することを特徴とする請求項１に記載の遠隔操縦式ヘリコプタの操縦練習装置。   The tilt restricting body (9) is provided with a tilt suppression mechanism (12) for preventing the mast (6) from tilting by adding resistance to the tilting mast (6). The remote control helicopter operation training device according to claim 1. 傾倒抑制機構（１２）は、中央に上下に貫通する通孔（１３ａ）を有し、外周面が傾倒規制体（９）の内面に接合するように形成された適宜な厚みの緩衝部材（１３）と、前記通孔（１３ａ）にマスト（６）を通してこの緩衝部材（１３）を傾倒規制体（９）内に保持する保持部材（１４）からなり、前記緩衝部材（１３）の保持位置をマスト（６）に沿って調節可能に設けた構成を有することを特徴とする請求項２に記載の遠隔操縦式ヘリコプタの操縦練習装置。   The tilt suppression mechanism (12) has a through-hole (13a) penetrating vertically at the center, and a buffer member (13 having an appropriate thickness formed so that the outer peripheral surface is joined to the inner surface of the tilt regulating body (9). ) And a holding member (14) for holding the buffer member (13) in the tilt regulating body (9) through the mast (6) through the through hole (13a), and the holding position of the buffer member (13) is 3. The remote control helicopter operation training device according to claim 2, wherein the operation control device is configured to be adjustable along the mast (6). 緩衝部材（１３）としてスポンジを用いたことを特徴とする請求項３に記載の遠隔操縦式ヘリコプタの操縦練習装置。   4. The remote control helicopter operation training device according to claim 3, wherein a sponge is used as the buffer member (13).
JP2011038313A 2011-02-24 2011-02-24 Remote control helicopter operation training device Expired - Fee Related JP5238049B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP2011038313A JP5238049B2 (en) 2011-02-24 2011-02-24 Remote control helicopter operation training device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2011038313A JP5238049B2 (en) 2011-02-24 2011-02-24 Remote control helicopter operation training device

Publications (2)

Publication Number Publication Date
JP2012170776A JP2012170776A (en) 2012-09-10
JP5238049B2 true JP5238049B2 (en) 2013-07-17

Family

ID=46974212

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2011038313A Expired - Fee Related JP5238049B2 (en) 2011-02-24 2011-02-24 Remote control helicopter operation training device

Country Status (1)

Country Link
JP (1) JP5238049B2 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR20160049810A (en) * 2014-10-28 2016-05-10 충남대학교산학협력단 Apparatus for testing multirotor system

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP5350557B1 (en) * 2013-06-06 2013-11-27 康郁 秋山 Aircraft flight training device
KR102089761B1 (en) * 2019-04-25 2020-03-16 (주)메세 Motion puppet
CN114923657B (en) * 2022-07-21 2022-10-04 中国空气动力研究与发展中心高速空气动力研究所 Vertical rod rope supporting system for full-aircraft flutter wind tunnel test

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS53123244A (en) * 1977-03-30 1978-10-27 Fuetsuto Herumuuto Device for remotely controlling and training model helicopter
JP3168226B2 (en) * 1992-05-29 2001-05-21 ヤマハ発動機株式会社 Training device for remote-controlled helicopter

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR20160049810A (en) * 2014-10-28 2016-05-10 충남대학교산학협력단 Apparatus for testing multirotor system

Also Published As

Publication number Publication date
JP2012170776A (en) 2012-09-10

Similar Documents

Publication Publication Date Title
JP5238049B2 (en) Remote control helicopter operation training device
KR101853623B1 (en) Testing bed for drone
CA2678573C (en) Seat assembly such as for an amusement ride
KR101165573B1 (en) Aircraft simulator with seat shaker
KR20220045050A (en) Resistance control system and method for amusement attraction
CN202952924U (en) Vibration absorbing lifting frame and vibration absorbing fixing device
KR100997902B1 (en) Device for assembly of liquid rocket engine's nozzle extension
US10577039B2 (en) Training aid for bicycle
US8307773B2 (en) Passenger module suspension system
JP5574525B2 (en) Swing playground equipment
KR101483117B1 (en) Flying play teaching tools
WO2019069077A1 (en) Motion arrangement
US3275277A (en) Vehicle seat
JP6788303B2 (en) Motion base
CN109878738A (en) A kind of aero seat angle adjustment device
KR200489054Y1 (en) Flight Attitude For Education
JP3168226B2 (en) Training device for remote-controlled helicopter
US1822082A (en) Steering device for aeroplanes
KR20160000732U (en) A structure of the treadmill with adjustment buffer state of vibration
CN110478918B (en) Manned underwater vehicle robot
CN203666722U (en) Shooting trolley with shock absorption function
CA3148584A1 (en) Exercise device for use in microgravity environments
KR102614352B1 (en) swimming simulator
JP3345805B2 (en) Radio-controlled helicopter pilot training legs
CN110525151A (en) A kind of Intelligent flight device being lauched

Legal Events

Date Code Title Description
A977 Report on retrieval

Free format text: JAPANESE INTERMEDIATE CODE: A971007

Effective date: 20130221

TRDD Decision of grant or rejection written
A01 Written decision to grant a patent or to grant a registration (utility model)

Free format text: JAPANESE INTERMEDIATE CODE: A01

Effective date: 20130227

A61 First payment of annual fees (during grant procedure)

Free format text: JAPANESE INTERMEDIATE CODE: A61

Effective date: 20130329

R150 Certificate of patent or registration of utility model

Free format text: JAPANESE INTERMEDIATE CODE: R150

Ref document number: 5238049

Country of ref document: JP

Free format text: JAPANESE INTERMEDIATE CODE: R150

FPAY Renewal fee payment (event date is renewal date of database)

Free format text: PAYMENT UNTIL: 20160405

Year of fee payment: 3

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

LAPS Cancellation because of no payment of annual fees