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JP2005270610A - Simulator for paraglider - Google Patents

Simulator for paraglider Download PDF

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Publication number
JP2005270610A
JP2005270610A JP2004124859A JP2004124859A JP2005270610A JP 2005270610 A JP2005270610 A JP 2005270610A JP 2004124859 A JP2004124859 A JP 2004124859A JP 2004124859 A JP2004124859 A JP 2004124859A JP 2005270610 A JP2005270610 A JP 2005270610A
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JP
Japan
Prior art keywords
pulley
harness
body frame
paraglider
simulator
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
Application number
JP2004124859A
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Japanese (ja)
Inventor
Hiroshi Takahashi
広志 高橋
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.)
Individual
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Individual
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Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to JP2004124859A priority Critical patent/JP2005270610A/en
Publication of JP2005270610A publication Critical patent/JP2005270610A/en
Pending legal-status Critical Current

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Abstract

<P>PROBLEM TO BE SOLVED: To provide a simulator for a paraglider allowing a user to virtually experience the adjustment of a harness and the flying by reproducing the state of the harness generated in the flying while maneuvering the paraglider even if the user is on the ground. <P>SOLUTION: A spring with a pulley is mounted on top of a support, and break cords, passing through pulleys of a riser, are attached to left and right corners in the rear of a body frame via the pulley on top of the support on the opposite side. The body frame and the harness are rotated while banking by pulling a grip. <P>COPYRIGHT: (C)2006,JPO&NCIPI

Description

本発明は、地上にいながら、飛行中に起きるパラグライダー操作時のハーネス状態を、よりリアルに再現することによりハーネスの調整、及び飛行中の疑似体験ができる、パラグライダー用シミュレーターに関するものである。  The present invention relates to a simulator for a paraglider that allows a harness to be adjusted and a simulated experience during flight by more realistically reproducing a harness state during a paraglider operation that occurs during flight while on the ground.

従来は、シミュレーターにハーネスを取り付け、ハーネスに座り込み体に合わせてハーネスのベルトの調整や座り心地などを試していた。  Conventionally, a harness was attached to the simulator, and the harness belt was adjusted and the seating comfort was tested according to the body.

そのため次のような問題があった。
(イ)上空でのいろいろな動きに対しての不安があった。
(ロ)上空でブレ−クコードを操作した時に起こるバンクがかかった状態での旋回時のハーネスの状態、また、体重移動の掛け方などがわからなかった。
本発明は、以上の問題点を解決するためになされたものである。
Therefore, there were the following problems.
(B) I was worried about various movements in the sky.
(B) I didn't know the state of the harness when turning with the bank applied when operating the break cord in the sky, and how to apply weight shift.
The present invention has been made to solve the above problems.

支柱(1)の上部にプーリー(2)のついたスプリング(8)を設け、ブレークコード(5)はライザー(10)のプーリー(4)を通り、反対側の支柱(1)上部のプーリー(2)を介して本体フレーム(3)後部の左右コーナーにそれぞれ取り付ける。フライヤーはハーネスをライザー(10)のカラビナ(11)に取り付け、グリップ(6)を引くことによりブレークコード(5)が各プーリーを通りそれに繋がれた本体フレーム(3)のコーナーが引かれ、これにより本体フレーム(3)及びハーネスが傾き、バンクをかけながら回転する。以上を特徴とするパラグライダー用シミュレーターである。  The spring (8) with the pulley (2) is provided on the upper part of the support (1), the break cord (5) passes through the pulley (4) of the riser (10), and the pulley ( Attach to the left and right corners of the rear part of the body frame (3) via 2). The flyer attaches the harness to the carabiner (11) of the riser (10) and pulls the grip (6) to pull the corner of the body frame (3) where the break cord (5) passes through each pulley and is connected to it. As a result, the main body frame (3) and the harness are tilted and rotated while applying the bank. This is a paraglider simulator characterized by the above.

上空でのブレークコード操作時のハーネスの傾きがよくわかり、体重移動の掛け方や地上での練習に役立てることができる。  Knowing the inclination of the harness when operating a break cord in the sky, it can be used for weight transfer and practice on the ground.

以下、本発明の実施の形態について説明する。
(イ)4本の支柱(1)の上部に水平に橋渡しされた天頂軸(12)の中央に支点(7)が設けられその支点から放射状に4方向に伸びたチェーン(9)に四角枠の本体フレーム(3)を吊り下げる。
(ロ)本体フレーム(3)の枠の対向する辺に、下端にリング(14)を有するフック(13)が複数設けられ、そのリングにライザー(10)の先端を取り付ける。
(ハ)支柱(1)の上部にプーリー(2)のついたスプリング(8)を本体フレーム(3)の前縁より少し内側に設ける。
(ニ)グリップ(6)に繋がったブレークコード(5)をライザー(10)に取り付いてあるプーリー(4)を通り、反対側の支柱(1)上部のスプリングのプーリー(2)を介して本体フレーム(3)後部の左右コーナーにそれぞれ取り付ける。
本発明は、以上の構造よりなっている。
本発明を使用するときは、まず、ハーネスをカラビナ(11)に取り付けフライヤーがハーネスに座り込む。フライヤーは、左右のグリップ(6)を取り、旋回したいほうのグリップ(6)を引き込む。すると、このブレークコード(5)に繋がれた側の本体フレーム(3)のコーナーは、支柱(1)上部に取り付けたスプリング(8)とプーリー(2)を介してライザー(10)のプーリー(4)を通りひっぱられることになる。このとき本体フレーム(3)のコーナーは支柱(1)上部のスプリング(8)のほうへ引き寄せられることになる。これによって本体フレーム(3)は、チェーン(9)によって支点(7)で支えられているため、グリップ(6)を引っ張ったほうへバンクをつけながら回転をはじめる。
また、実際のフライトでは、グリップ(6)を引っ張ってからすぐに機体、及びハーネスが反応するのではないのでこれをスプリング(8)を取り付けることによってタイムラグを生じさせ、尚且つ柔らかな旋回ができるようにしているのである。
Embodiments of the present invention will be described below.
(A) A fulcrum (7) is provided at the center of the zenith shaft (12) horizontally bridged above the four columns (1). Suspend the body frame (3).
(B) A plurality of hooks (13) having a ring (14) at the lower end are provided on opposite sides of the frame of the main body frame (3), and the tip of the riser (10) is attached to the ring.
(C) A spring (8) with a pulley (2) on the upper part of the support (1) is provided slightly inside the front edge of the main body frame (3).
(D) The break cord (5) connected to the grip (6) passes through the pulley (4) attached to the riser (10) and passes through the pulley (2) of the spring on the opposite column (1) to the main body Attach to the left and right corners at the rear of the frame (3).
The present invention has the above structure.
When using the present invention, the harness is first attached to the carabiner (11) and the flyer sits on the harness. The flyer takes the left and right grips (6) and pulls in the grip (6) that wants to turn. Then, the corner of the main body frame (3) connected to the break cord (5) is connected to the pulley ( It will be pulled through 4). At this time, the corner of the main body frame (3) is drawn toward the spring (8) at the top of the column (1). As a result, the main body frame (3) is supported by the fulcrum (7) by the chain (9), and thus starts rotating while attaching the bank to the side where the grip (6) is pulled.
In actual flight, the aircraft and harness do not react immediately after the grip (6) is pulled. Therefore, by attaching a spring (8) to this, a time lag is generated, and a soft turn is possible. It is doing so.

本発明の斜視図Perspective view of the present invention 本発明の平面図Plan view of the present invention 本発明の正面図Front view of the present invention 本発明の側面図Side view of the present invention 本発明の操作時の斜視図The perspective view at the time of operation of this invention

符号の説明Explanation of symbols

1 支柱
2 プーリー
3 本体フレーム
4 プーリー
5 ブレークコード
6 グリップ
7 支点
8 スプリング
9 チェーン
10 ライザー
11 カラビナ
12 天頂軸
13 フック
14 リング部
1 Strut 2 Pulley 3 Body Frame 4 Pulley 5 Break Cord 6 Grip 7 Support Point 8 Spring 9 Chain 10 Riser 11 Carabiner 12 Zenith Shaft 13 Hook 14 Ring

Claims (1)

支柱の上部にプーリーのついたスプリングを設け、ブレークコードがライザーのプーリーを通り、反対側の支柱上部のプーリーを介して本体フレーム後部の左右コーナーにそれぞれとりつけられ、グリップを引くことにより本体フレーム、およびハーネスがバンクをかけながら回転することを特徴とするパラグライダー用シミュレーター。    A spring with a pulley is installed on the top of the column, the break cord passes through the pulley of the riser, it is attached to the left and right corners of the rear of the main unit frame via the pulley on the other side of the column, and the body frame by pulling the grip, And a paraglider simulator, in which the harness rotates while banking.
JP2004124859A 2004-03-23 2004-03-23 Simulator for paraglider Pending JP2005270610A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP2004124859A JP2005270610A (en) 2004-03-23 2004-03-23 Simulator for paraglider

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2004124859A JP2005270610A (en) 2004-03-23 2004-03-23 Simulator for paraglider

Publications (1)

Publication Number Publication Date
JP2005270610A true JP2005270610A (en) 2005-10-06

Family

ID=35170866

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2004124859A Pending JP2005270610A (en) 2004-03-23 2004-03-23 Simulator for paraglider

Country Status (1)

Country Link
JP (1) JP2005270610A (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2487369A (en) * 2011-01-18 2012-07-25 Maelstrom Virtual Productions Ltd Simulator apparatus for parachute training
WO2012144690A1 (en) * 2011-04-20 2012-10-26 (주)엔투스 Glider motion simulator
CN104616560A (en) * 2014-12-28 2015-05-13 上海电机学院 Suspension experience simulator
CN105664465A (en) * 2016-03-30 2016-06-15 上海电机学院 Bird-imitation experience simulation equipment
CN107233726A (en) * 2016-03-28 2017-10-10 大连奥马科技有限公司 3D paraglider device for experiencing

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2487369A (en) * 2011-01-18 2012-07-25 Maelstrom Virtual Productions Ltd Simulator apparatus for parachute training
GB2487369B (en) * 2011-01-18 2013-05-01 Maelstrom Virtual Productions Ltd Parachute training simulators
WO2012144690A1 (en) * 2011-04-20 2012-10-26 (주)엔투스 Glider motion simulator
CN104616560A (en) * 2014-12-28 2015-05-13 上海电机学院 Suspension experience simulator
CN104616560B (en) * 2014-12-28 2017-04-19 上海电机学院 Suspension experience simulator
CN107233726A (en) * 2016-03-28 2017-10-10 大连奥马科技有限公司 3D paraglider device for experiencing
CN105664465A (en) * 2016-03-30 2016-06-15 上海电机学院 Bird-imitation experience simulation equipment

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