JP2022007832A - Vibration control for rotary sphere frame for unmanned aircraft and shock absorbing device second version - Google Patents
Vibration control for rotary sphere frame for unmanned aircraft and shock absorbing device second version Download PDFInfo
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- 230000035939 shock Effects 0.000 title claims abstract description 15
- 230000002265 prevention Effects 0.000 claims description 7
- 239000006096 absorbing agent Substances 0.000 claims description 5
- 238000007689 inspection Methods 0.000 description 3
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 2
- 229910052799 carbon Inorganic materials 0.000 description 2
- 230000032683 aging Effects 0.000 description 1
- 230000001066 destructive effect Effects 0.000 description 1
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/40—Weight reduction
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Abstract
Description
この発明は、無人航空機および無人航空機の周りに設置する回転球体フレームの振動防止かつ衝撃緩衝装置に関する。 The present invention relates to an unmanned aerial vehicle and a vibration-preventing and shock-cushioning device for a rotating spherical frame installed around the unmanned aerial vehicle.
回転球体フレームは、ジャイロスコープを応用したジンバル構造を有する。このため、図1に示すように、内部の無人航空機を水平に保ちながら、回転球体フレームは全方向に回転する。これにより回転球体フレーム付き無人航空機は、対象物へ安全に接近または接着し、搭載カメラで各種インフラ点検を行うことができる。 The rotating sphere frame has a gimbal structure to which a gyroscope is applied. Therefore, as shown in FIG. 1, the rotating sphere frame rotates in all directions while keeping the internal unmanned aerial vehicle horizontal. This allows an unmanned aerial vehicle with a rotating sphere frame to safely approach or adhere to an object and perform various infrastructure inspections with the onboard camera.
約6年前の本特許出願人製作の回転球体フレームのジンバル接続は、図2に示すように、ジンバルの穴にネジを通すだけで、穴とネジに隙間があるため、無人航空機および回転球体フレームは振動した。
そこで、約5年半前の本特許出願人製作の回転球体フレームのジンバル接続は、図3に示すように、固定ベアリングにネジを接着し、振動防止に成功した。
しかし、ベアリングにネジを接着するため、ジンバルに遊びがなく衝撃を緩衝できず、回転球体フレームが壁などに強く当たると回転球体フレームは一部破損した。
そこで、この発明は、無人航空機および回転球体フレームの振動防止と衝撃緩衝を両立して実現することを課題とする。As shown in Fig. 2, the gimbal connection of the rotating sphere frame manufactured by the patent applicant about 6 years ago is an unmanned aerial vehicle and a rotating sphere because there is a gap between the hole and the screw just by passing the screw through the hole of the gimbal. The frame vibrated.
Therefore, the gimbal connection of the rotating sphere frame manufactured by the applicant for this patent about five and a half years ago succeeded in preventing vibration by adhering a screw to a fixed bearing as shown in FIG.
However, since the screws were adhered to the bearings, there was no play in the gimbal and the impact could not be cushioned, and when the rotating sphere frame hit a wall or the like strongly, the rotating sphere frame was partially damaged.
Therefore, it is an object of the present invention to realize both vibration prevention and shock cushioning of an unmanned aerial vehicle and a rotating sphere frame.
以上の課題を解決するために、第一発明は、図4の固定ベアリングにほぼ隙間のないネジを通すことで振動を防止し、かつ図5および図6に示すように、ネジがベアリングの軸方向(図5の左右)に動くことで衝撃を緩衝する装置である。 In order to solve the above problems, in the first invention, vibration is prevented by passing a screw having almost no gap through the fixed bearing of FIG. 4, and as shown in FIGS. 5 and 6, the screw is the shaft of the bearing. It is a device that cushions the impact by moving in the direction (left and right in FIG. 5).
また第二発明は、固定ベアリングと同様の機能を有する部位にほぼ隙間のないネジを通すことで振動を防止し、かつ図8および図9に示すように、ネジが部位の軸方向(図7の1と3を結ぶ方向)に動くことで衝撃を緩衝する装置である。
固定ベアリングと同様の機能を有する部位とは、図7の1、2、3、4をいう。図7の右側をひっくり返して左側にかぶせると、1と2および3と4は穴となる。穴の直径は、3Dプリンタ等で精巧に確定できるので、固定ベアリングと同様に、ほぼ隙間のないネジを通すことで振動を防止し、ネジが部位の軸方向(図7の1と3を結ぶ方向)に動くことで衝撃を緩衝することができる。Further, in the second invention, vibration is prevented by passing a screw having almost no gap through a part having a function similar to that of a fixed bearing, and as shown in FIGS. 8 and 9, the screw is in the axial direction of the part (FIG. 7). It is a device that cushions the impact by moving in the direction connecting 1 and 3 of.
The parts having the same function as the fixed bearing refer to 1, 2, 3 and 4 in FIG. When the right side of FIG. 7 is turned over and put on the left side, 1 and 2 and 3 and 4 become holes. Since the diameter of the hole can be precisely determined with a 3D printer or the like, vibration is prevented by passing a screw with almost no gap, and the screw connects 1 and 3 of the part in the axial direction of the part (connecting 1 and 3 in FIG. 7). The impact can be buffered by moving in the direction).
請求項1の振動防止かつ衝撃緩衝装置とは、図5に図6をかぶせたもの(カーボン棒を除く)を一例とする、ベアリング固定部分、ネジ可動部分、ベアリング、ネジを一体とする装置である。 The vibration prevention and impact shock absorber according to claim 1 is a device that integrates a bearing fixing part, a screw movable part, a bearing, and a screw, for example, a device covered with FIG. 6 in FIG. 5 (excluding a carbon rod). be.
請求項2の振動防止かつ衝撃緩衝装置とは、図8に図9をかぶせたもの(カーボン棒を除く)を一例とする、固定ベアリングと同様の機能を有する部位、ネジ可動部分、ネジを一体とする装置である。 The vibration prevention and impact shock absorber according to claim 2, for example, the one covered with FIG. 9 in FIG. 8 (excluding the carbon rod), has a part having the same function as a fixed bearing, a screw movable part, and a screw. It is a device.
第一発明または第二発明によれば、振動防止かつ衝撃緩衝装置をつけて、無人航空機および回転球体フレームの振動防止と衝撃緩衝を両立して実現することができる。 According to the first invention or the second invention, it is possible to realize both vibration prevention and shock cushioning of an unmanned aerial vehicle and a rotating spherical frame by attaching a vibration prevention and shock shock absorber.
この発明の一実施形態を、図10に示す。
振動防止かつ衝撃緩衝装置を回転球体フレーム内6ヶ所に設置することにより、無人航空機および回転球体フレームの振動防止と衝撃緩衝を両立して実現することができる。
これにより、回転球体フレームが壁などに強く当たっても、衝撃は相当程度緩和され、回転球体フレームは容易に破損しない。
無人航空機とは、飛行機、回転翼航空機等であって人が乗ることができないもののうち、遠隔操作又は自動操縦により飛行させることができるものをいう(超軽量のものなどを除く)。
無人航空機用回転球体フレームとは、ジャイロスコープを応用したジンバル構造を有し、内部の無人航空機を水平に保ちながら、球体フレームは全方向に回転する構造体をいう。An embodiment of the present invention is shown in FIG.
By installing anti-vibration and shock-cushioning devices at six locations in the rotating sphere frame, it is possible to achieve both vibration prevention and shock-cushioning for unmanned aerial vehicles and rotating sphere frames.
As a result, even if the rotating sphere frame strongly hits a wall or the like, the impact is considerably reduced and the rotating sphere frame is not easily damaged.
An unmanned aerial vehicle is an airplane, a rotary wing aircraft, etc. that cannot be boarded by a person and can be flown by remote control or autopilot (excluding ultra-lightweight aircraft).
The rotating spherical frame for an unmanned aerial vehicle has a gimbal structure to which a gyroscope is applied, and the spherical frame is a structure that rotates in all directions while keeping the unmanned aerial vehicle inside horizontal.
無人航空機および回転球体フレームの振動防止かつ衝撃緩衝装置は、回転球体フレーム付き無人航空機の安全性を高める。このため橋梁、トンネルなどのインフラ点検に広く活用される可能性は高い。
政府は、2015年1月に発表したロボット新戦略の中で、2020年頃までに、国内の重要インフラ・老朽化インフラの20%はセンサー、ロボット、非破壊検査技術等を活用して点検・補修を高効率化する旨、明記している。回転球体フレーム付き無人航空機は、ロボットに該当する。Anti-vibration and shock shock absorbers for unmanned aerial vehicles and rotating sphere frames enhance the safety of unmanned aerial vehicles with rotating sphere frames. Therefore, it is highly possible that it will be widely used for infrastructure inspections such as bridges and tunnels.
In the new robot strategy announced in January 2015, the government will inspect and repair 20% of domestic important infrastructure and aging infrastructure using sensors, robots, non-destructive inspection technology, etc. by around 2020. It is clearly stated that the efficiency will be improved. An unmanned aerial vehicle with a rotating sphere frame corresponds to a robot.
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CN117382941A (en) * | 2023-12-11 | 2024-01-12 | 山东字节信息科技有限公司 | Single rotor unmanned aerial vehicle |
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JP2018100063A (en) * | 2016-12-22 | 2018-06-28 | 学校法人早稲田大学 | Movable body, and remote inspection system using the same, and remote inspection method in pipe |
JP2020163953A (en) * | 2019-03-28 | 2020-10-08 | 光司商会株式会社 | Hanging work assist system |
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JPH06156394A (en) * | 1992-11-26 | 1994-06-03 | Mitsubishi Electric Corp | Shock absorber |
JP2000142585A (en) * | 1998-10-30 | 2000-05-23 | Sikorsky Aircraft Corp | Cabin interior assembly and helicopter equipped therewith |
CN203680323U (en) * | 2013-12-31 | 2014-07-02 | 深圳大学 | Universal multi-rotor-wing robot framework supporting safety protection system |
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Cited By (2)
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CN117382941B (en) * | 2023-12-11 | 2024-03-05 | 山东字节信息科技有限公司 | Single rotor unmanned aerial vehicle |
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