JPH01245285A - Hovering training device for radio manipulated helicopter - Google Patents
Hovering training device for radio manipulated helicopterInfo
- Publication number
- JPH01245285A JPH01245285A JP63072023A JP7202388A JPH01245285A JP H01245285 A JPH01245285 A JP H01245285A JP 63072023 A JP63072023 A JP 63072023A JP 7202388 A JP7202388 A JP 7202388A JP H01245285 A JPH01245285 A JP H01245285A
- Authority
- JP
- Japan
- Prior art keywords
- hovering
- pantographs
- perpendicular direction
- training device
- training
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
- 230000003247 decreasing effect Effects 0.000 abstract 2
- 230000008602 contraction Effects 0.000 abstract 1
- 238000000034 method Methods 0.000 description 2
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000006073 displacement reaction Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
Abstract
Description
【発明の詳細な説明】
(産業上の利用分野)
この発明は、無線操縦ヘリコプタ−のホバーリング訓練
装置に関する。DETAILED DESCRIPTION OF THE INVENTION (Field of Industrial Application) The present invention relates to a hovering training device for a radio-controlled helicopter.
(従来の技術)
昨今、ヘリコプタ−等の飛翔体を用いて空中から地上を
撮影する、いわゆる空撮が多々行なわれているが、この
空撮にを大の実機を用いるとコストが嵩むうえに、危険
防止上いかなるフィールドでも撮影可能という訳にはい
かなかった。そこでスチルカメラ、ビデオカメラ等を搭
αした遠隔無線操縦の高性能小型ヘリコプタ−を用いる
ことにより、実機以上の確実、安全な空撮を行うように
なってきている。(Prior art) In recent years, so-called aerial photography, in which images of the ground are photographed from the air using a flying object such as a helicopter, has been frequently carried out, but using a large actual aircraft for this aerial photography not only increases the cost. However, to prevent danger, it was not possible to shoot in any field. Therefore, by using remote radio-controlled, high-performance small helicopters equipped with still cameras, video cameras, etc., aerial photography is becoming more reliable and safe than with actual aircraft.
ところで、このような遠隔無線操縦の小型ヘリコプタ−
の操縦には熟練を要し、操作を誤ると失速して墜落し、
高価な機体並びに搭載機器を損傷する虞れがある。この
為、オペレーターは一般に第3図に示すごとき構成のホ
バーリング訓練装置lOに無線操縦の小型ヘリコプタ−
20を載置して、操縦技術の中で最も困難なホバーりン
グ(空中停止)の訓練を行っている。このホバーリング
訓練装置10は、支柱11上に揺動自在に横架した棹1
2の一端に小型ヘリコプタ−20を固定し他端にはmす
13を取り付けて両者のバランスをとる構造となってい
る。By the way, such a remote radio-controlled small helicopter
It requires skill to operate, and if you make a mistake, it will stall and crash.
There is a risk of damaging the expensive aircraft and onboard equipment. For this reason, an operator generally uses a radio-controlled small helicopter in a hovering training device IO with the configuration shown in Figure 3.
20 is mounted on the aircraft to conduct hovering training, which is the most difficult maneuvering technique. This hovering training device 10 consists of a pole 1 horizontally suspended on a support 11 so as to be swingable.
The structure is such that a small helicopter 20 is fixed to one end of the helicopter 2, and an MS 13 is attached to the other end to balance the two.
(発明が解決しようとする課題)
このようなホバーリング!lII棟装置ftl0は、そ
の構造から支柱11と小型ヘリコプタ−20とを結ぶ半
径方向の移動が制限されるために自在な飛行訓練ができ
ないばかりでなく、棹12が通常5〜7mと長くしかも
支柱11を中心に回転するため比較的広い場所を必要と
し、手軽に訓練することができないという問題点を有し
ていた。(Problem to be solved by the invention) Hovering like this! The structure of the II building equipment ftl0 not only restricts movement in the radial direction connecting the support 11 and the small helicopter 20, but also prevents flexible flight training. 11, it requires a relatively large space and has the problem of not being easy to train.
(課題を解決するための手段)
このような問題を解決するために本発明は、下端に水平
irM機構を備え一対の摺動軸を存する台枠と、前記各
摺動軸にそれぞれ一端が摺動自在に係合されて垂直方向
に伸縮する一対のパンタグラフと、該パンタグラフの他
端に水平方向に摺動自在に係合されたX−Yテーブルと
、該テーブル上に揺動自在に係止された載置部材とを備
えるようにしたものである。(Means for Solving the Problems) In order to solve such problems, the present invention provides an underframe having a horizontal IRM mechanism at its lower end and a pair of sliding shafts, and a frame having one end sliding on each of the sliding shafts. A pair of pantographs that are movably engaged and expand and contract in the vertical direction; an X-Y table that is slidably engaged with the other end of the pantograph in the horizontal direction; and a pair of pantographs that are movably engaged on the table. The mounting member is provided with a mounting member.
(作 用)
パンタグラフの伸縮によるZ方向、x−yテーブルによ
るXおよびY方向、揺動自在の8置部材によるθ方向の
全ての方向に自在に移動するととができ、かつ下端の水
平m 節m byを調節することによって装置全体の摺
動抵抗を低減させることができる。(Function) It can be moved freely in all directions including the Z direction by expanding and contracting the pantograph, the X and Y directions by the x-y table, and the θ direction by the swingable 8-position member, and the horizontal m node at the lower end. By adjusting m by, the sliding resistance of the entire device can be reduced.
(実施例)
以下、本発明の一実施例につき、図面を参照して説明す
る。(Example) Hereinafter, an example of the present invention will be described with reference to the drawings.
第1図は本発明によるホバーリング訓練装置の正面図で
あり、第2図は第1図の右側面図である両面において、
31および32は一対の摺動軸であり、これらの端部は
支持枠33および34に適宜の間隙を設けて平行に固定
されて、台枠35を構成している。台枠35の支持枠3
3お上び34のそれぞれの側端には!lif!iネジ3
6.37.38および39が螺入されて、台枠35を水
平に保つための水平態f!i機構40を構成している。FIG. 1 is a front view of the hovering training device according to the present invention, and FIG. 2 is a right side view of FIG.
Reference numerals 31 and 32 denote a pair of sliding shafts, the ends of which are fixed in parallel to support frames 33 and 34 with an appropriate gap therebetween, thereby forming an underframe 35. Support frame 3 of underframe 35
At each side edge of 3 and 34! lif! i screw 3
6.37.38 and 39 are screwed into the horizontal position f! to keep the underframe 35 horizontal. It constitutes the i mechanism 40.
このように構成された台枠35の摺動軸31−32には
それぞれ一対の摺動ブロック41および42並びに43
および44が挿入され、摺動軸31・32上を摺動する
。これらの摺動ブロック41〜44には一対のパンタグ
ラフ45および46の下部開放端47および48並びに
49および50が回動自在に軸着されている。パンタグ
ラフ45・46の下部開放端51および52並びに53
および54は、やはり摺動ブロック55および56並び
に57および58に回動自在に軸着されており、これら
の摺動ブロック55〜58はX−Yテーブル70の台板
71の下面に平行に横架した摺動軸59および60に挿
入され、これらの軸59・60上を摺動する。従って、
一対のパンタグラフ45・46の伸縮によって、X−Y
テーブル70は垂直方向即ちZ方向に上下動することが
できる。A pair of sliding blocks 41 and 42 and a pair of sliding blocks 43 are respectively attached to the sliding shafts 31-32 of the underframe 35 configured in this way.
and 44 are inserted and slide on the sliding shafts 31 and 32. Lower open ends 47 and 48 and 49 and 50 of a pair of pantographs 45 and 46 are rotatably pivoted to these sliding blocks 41-44. Lower open ends 51 and 52 and 53 of pantographs 45 and 46
and 54 are also rotatably pivoted to sliding blocks 55 and 56 and 57 and 58, and these sliding blocks 55 to 58 are horizontally parallel to the lower surface of the base plate 71 of the X-Y table 70. It is inserted into the suspended sliding shafts 59 and 60 and slides on these shafts 59 and 60. Therefore,
By expanding and contracting a pair of pantographs 45 and 46,
The table 70 can move up and down in the vertical direction, that is, the Z direction.
X−Yテーブル70はX軸、Y軸共に同構造であり、台
板71上に平行に横架された摺動軸72および73にそ
れぞれ挿入された摺動ブロック74および75と、これ
らの摺動ブロック74・75上に横架された台板76上
に前記摺動軸72・73とは直角でかつ互に平行に横架
された摺動軸77および78にそれぞれ挿入され互に連
結された摺動ブロック80および81とからなっている
。The X-Y table 70 has the same structure for both the X-axis and the Y-axis, and has sliding blocks 74 and 75 inserted into sliding shafts 72 and 73, which are horizontally suspended in parallel on a base plate 71, and sliding blocks 74 and 75, respectively. Sliding shafts 77 and 78, which are horizontally supported at right angles to the sliding shafts 72 and 73 and parallel to each other, are inserted onto a base plate 76 that is horizontally supported on the moving blocks 74 and 75, and are connected to each other. It consists of sliding blocks 80 and 81.
このX−Yテーブル70の摺動ブロック80・81上に
は軸82が植設されており、被ホバーリング機体をIJ
置するに適した形状に成形された載置部材83に埋設さ
れたピロボール84が前記軸82の先端に圧入されて、
@置部材83が軸82に対し回転かつrA動自在に取り
付けられている。A shaft 82 is installed on the sliding blocks 80 and 81 of this X-Y table 70, and the hovering aircraft is
A pillow ball 84 embedded in a mounting member 83 formed into a shape suitable for mounting is press-fitted into the tip of the shaft 82,
A mounting member 83 is attached to the shaft 82 so as to be rotatable and movable.
以上本発明になるホバーリング訓練装置の概要を説明し
たが、ホバーリング訓練装置はその使用目的から、被ホ
バーリング機体を搭載した状態で全ての方向に零に近い
抵抗で自在に動く必要があり、このため回動あるいは摺
動部にはそれぞれ図示しないベアリングを用いて抵抗を
減じると共にパンタグラフ45.48の支点90.91
.92および93近傍に、パンタグラフ45.4Bを垂
直方向に伸長させるように引張りコイルバネ9495.
9Bおよび97を張榮して、垂直方向の荷重を減殺させ
ている。なお、垂直方向の荷重を減殺させるには、図示
のごとく引張りコイルバネ94.95.96および97
を設ける他に、支持枠33.34とt8vIブロック4
1.42.43および44間に圧縮コイルバネを挿入し
てもよい。The outline of the hovering training device according to the present invention has been explained above, but due to its purpose of use, the hovering training device needs to be able to move freely in all directions with near zero resistance while carrying the hovering object. , For this reason, bearings (not shown) are used for each rotating or sliding part to reduce resistance, and the fulcrum 90.91 of the pantograph 45.48 is
.. Near 92 and 93, tension coil springs 9495.4B are installed to extend the pantograph 45.4B in the vertical direction.
9B and 97 are stretched to reduce the vertical load. In addition, in order to reduce the vertical load, use tension coil springs 94, 95, 96 and 97 as shown in the figure.
In addition to providing support frames 33 and 34 and t8vI block 4
1.42. A compression coil spring may be inserted between 43 and 44.
(発明の効果)
本発明は、パンタグラフ、X−Yテーブルおよび摺動自
在なU置部材を垂直方向に係合し、かつ被ホバーリング
機体を搭載した杖態で垂直方向の荷重を零に減殺する構
成としたので、被ホバーリング機体が全ての方向にほと
んど抵抗なく移動し空中で行うと同様のホバーリング訓
練を行うことができる。(Effects of the Invention) The present invention reduces the vertical load to zero by vertically engaging a pantograph, an X-Y table, and a slidable U-mounting member, and in a crutch configuration carrying a hovering aircraft. Because of this configuration, the hovering target aircraft moves in all directions with almost no resistance, and hovering training similar to that performed in the air can be performed.
また、垂直方向の変位にパンタグラフを用いたため訓v
J装置を小型化でき、狭い場所でも訓練し得ると共に運
搬も容易であるという効果を奏するIn addition, since a pantograph was used for vertical displacement,
The J device can be made smaller, training can be performed even in narrow spaces, and it is easy to transport.
第1図は本発明になるホバーリング訓[装置の正面図、
第2図は第1図の右側面図であり、第3図は従来のホバ
ーリング訓練装置を示す模式図である。
35・・・台枠、40・・・水平調*a構、45・46
・・・パンタグラフ、70・・・X−Yテーブル、83
・・・載置部材Figure 1 shows the hovering technique according to the present invention [a front view of the device,
FIG. 2 is a right side view of FIG. 1, and FIG. 3 is a schematic diagram showing a conventional hovering training device. 35...Underframe, 40...Horizontal *a structure, 45/46
... Pantograph, 70 ... X-Y table, 83
...Placement member
Claims (1)
、前記各摺動軸にそれぞれ一端が摺動自在に係合されて
垂直方向に伸縮する一対のパンタグラフと、該パンタグ
ラフの他端に水平方向に摺動自在に、係合されたX−Y
テーブルと、該テーブル上に揺動自在に係止された載置
部材とからなることを特徴とする無線操縦ヘリコプター
のホバーリング訓練装置。An underframe having a horizontal adjustment mechanism at its lower end and a pair of sliding shafts, a pair of pantographs whose one ends are slidably engaged with each of the sliding shafts and expand and contract in the vertical direction, and the other end of the pantographs. X-Y that is slidably engaged in the horizontal direction.
1. A hovering training device for a radio-controlled helicopter, comprising a table and a mounting member swingably secured to the table.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP63072023A JPH01245285A (en) | 1988-03-28 | 1988-03-28 | Hovering training device for radio manipulated helicopter |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP63072023A JPH01245285A (en) | 1988-03-28 | 1988-03-28 | Hovering training device for radio manipulated helicopter |
Publications (1)
Publication Number | Publication Date |
---|---|
JPH01245285A true JPH01245285A (en) | 1989-09-29 |
Family
ID=13477398
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP63072023A Pending JPH01245285A (en) | 1988-03-28 | 1988-03-28 | Hovering training device for radio manipulated helicopter |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPH01245285A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2014196461A1 (en) * | 2013-06-06 | 2014-12-11 | AKIYAMA Yasufumi | Flying vehicle flight training device |
-
1988
- 1988-03-28 JP JP63072023A patent/JPH01245285A/en active Pending
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2014196461A1 (en) * | 2013-06-06 | 2014-12-11 | AKIYAMA Yasufumi | Flying vehicle flight training device |
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