JPH026244A - Transporting device of midget unmanned helicopter - Google Patents
Transporting device of midget unmanned helicopterInfo
- Publication number
- JPH026244A JPH026244A JP15356288A JP15356288A JPH026244A JP H026244 A JPH026244 A JP H026244A JP 15356288 A JP15356288 A JP 15356288A JP 15356288 A JP15356288 A JP 15356288A JP H026244 A JPH026244 A JP H026244A
- Authority
- JP
- Japan
- Prior art keywords
- helicopter
- support plate
- midget
- sled
- unmanned helicopter
- 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.)
- Granted
Links
- 241000519996 Teucrium chamaedrys Species 0.000 title abstract 5
- 239000003814 drug Substances 0.000 abstract 1
- 229940079593 drug Drugs 0.000 abstract 1
- 238000009434 installation Methods 0.000 abstract 1
- 239000000463 material Substances 0.000 description 2
- 238000005507 spraying Methods 0.000 description 2
- 239000000126 substance Substances 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 1
- 239000011347 resin Substances 0.000 description 1
- 229920005989 resin Polymers 0.000 description 1
- 239000007921 spray Substances 0.000 description 1
Landscapes
- Handcart (AREA)
- Toys (AREA)
Abstract
Description
【発明の詳細な説明】
〔産業上の利用分野〕
本発明は例えば薬剤散布などに用いられる無線操縦式の
小型無人ヘリコプタの運搬装置に関するものである。DETAILED DESCRIPTION OF THE INVENTION [Field of Industrial Application] The present invention relates to a transport device for a radio-controlled small unmanned helicopter used for, for example, spraying chemicals.
近年、無線操縦式の小型無人ヘリコプタは、散布装置を
搭載して薬剤散布したり、あるいはカメラを搭載して危
険な場所を調査探索するなど、様々な用途に使用される
ようになってきた。In recent years, radio-controlled small unmanned helicopters have come to be used for a variety of purposes, such as being equipped with a spraying device to spray chemicals, or equipped with a camera to investigate and explore dangerous areas.
そして、この種の小型無人ヘリコプタを使用する場合は
、トラックやパンタイプの車両で使用目的地まで運搬す
るのが望ましい。When using this type of small unmanned helicopter, it is desirable to transport it to the destination using a truck or pan-type vehicle.
ところで、小型無人ヘリコプタの運搬時には、小型無人
ヘリコプタが路面の凹凸によって跳ねたり、車両の加減
速時に移動したりしないように荷台に固定する必要があ
るが、小型無人ヘリコプタは複雑な形状をしているだけ
でなく、機体は樹脂材などを用いて形成する場合が多く
それほど強度を有してないために、従来から知られてい
るロープ等を用いて確実に固定するのがきわめて困難と
なっている。本発明はこのような事情に鑑みなされたも
ので、小型無人ヘリコプタを荷台に確実に固定すること
ができる小型無人ヘリコプタの運搬装置を提供するもの
である。By the way, when transporting a small unmanned helicopter, it is necessary to secure it to the cargo platform so that it does not bounce due to uneven road surfaces or move when the vehicle accelerates or decelerates, but small unmanned helicopters have a complex shape. Not only that, but the fuselage is often made of resin and other materials that are not very strong, making it extremely difficult to securely secure it using conventional ropes. There is. The present invention was made in view of the above circumstances, and provides a small unmanned helicopter transporting device that can securely fix the small unmanned helicopter to a cargo platform.
本発明に係る運搬装置は、荷台の床板上に着脱自在に取
付けられ小型無人ヘリコプタの降着そりを支承する支持
板と、この支持板に着脱自在に取付けられ降着そりを上
方から覆うそり保持部を有する固定具とから構成したも
のである。The transportation device according to the present invention includes a support plate that is detachably attached to the floor plate of a cargo platform and supports the landing sled of a small unmanned helicopter, and a sled holding section that is detachably attached to the support plate and covers the landing sled from above. It consists of a fixture with a
本発明においては、荷台の床板上に支持板を取付け、こ
の支持板上に小型無人ヘリコプタを載置して固定具を取
付けると、降着そりがそり保持部で保持される。In the present invention, a support plate is attached to the floor plate of the loading platform, and when the small unmanned helicopter is placed on the support plate and the fixture is attached, the landing sled is held by the sled holding portion.
以下、本発明の一実施例を図により詳細に説明する。第
１図は本発明に係る運搬装置で小型無人ヘリコプタを固
定した状態を示す斜視図、第２図は第１図のｎ−ｕ線断
面図、第３図は支持板を示す斜視図、第４図は機体右側
の固定具を示す斜視図である。第１図に７１号１で示す
ものは小型無人ヘリコプタであり、機体２の下部には前
後の支持脚３，３を介して左右一対の降着そり４．４が
設けられている。これら降着そり４．４は機体２の前後
方向に延在しており、上方へ折曲げられた前端部には、
機体後部を持ち上げて運搬するときに使用する補助車輪
５，５が回転自在に支持されている。６は機体２の前部
に収容されたエンジンで回転駆動される主回転翼、７は
機体２の後部に配され前記主回転翼６の駆動反力を打ち
消す補助回転翼である。Hereinafter, one embodiment of the present invention will be described in detail with reference to the drawings. Fig. 1 is a perspective view showing a state in which a small unmanned helicopter is fixed with the transportation device according to the present invention, Fig. 2 is a sectional view taken along line nu in Fig. FIG. 4 is a perspective view showing the fixture on the right side of the fuselage. The one designated by No. 71 1 in FIG. 1 is a small unmanned helicopter, and a pair of left and right landing sleds 4.4 are provided at the bottom of the fuselage 2 via front and rear support legs 3, 3. These landing sleds 4.4 extend in the longitudinal direction of the fuselage 2, and have a front end bent upward.
Auxiliary wheels 5, 5 used when lifting and transporting the rear part of the fuselage are rotatably supported. Reference numeral 6 denotes a main rotor that is rotatably driven by an engine housed in the front of the fuselage 2, and 7 is an auxiliary rotor that is disposed at the rear of the fuselage 2 and cancels out the driving reaction force of the main rotor 6.
１１は小型無人ヘリコプタの運搬装置である。11 is a transportation device for a small unmanned helicopter.
この運搬装置１１は降着そり４，４を支承する支持板１
２と、この支持板１２に着脱自在に取付けられた固定具
１３とからなる。支持板１２は機体２０幅方向に延びる
帯板状に形成され、降着そり４．４の内側に対応する部
位には、支持板１２をトラックの箱荷台の床板１４に螺
合する取付ボルト１５が貫通する貫通孔１６が穿設され
、降着そり４．４の外側に対応する部位には、固定具１
３を支持板１２に固定するためのフック１７が突設され
ている。取付ポル１−１５の頭部には工具を使用するこ
となくこのボルトを回転させるハンドル１８が設けられ
ている。This transport device 11 includes a support plate 1 that supports the accretion sleds 4, 4.
2, and a fixture 13 detachably attached to the support plate 12. The support plate 12 is formed in the shape of a strip extending in the width direction of the fuselage 20, and a mounting bolt 15 for screwing the support plate 12 to the floor plate 14 of the truck bed is provided at a portion corresponding to the inside of the landing sled 4.4. A through hole 16 is drilled through the accretion sled 4.4, and a fixture 1 is provided at a portion corresponding to the outside of the accretion sled 4.4.
A hook 17 for fixing 3 to the support plate 12 is provided in a protruding manner. The head of the mounting bolt 1-15 is provided with a handle 18 for rotating this bolt without the use of tools.
前記固定具１３はフック１７を貫通させる透孔２１を有
する固定板２２と、この固定板２２に枢軸２３で枢着さ
れた棒状の固定ハンドル２４と、この固定ハンドル２４
上に長さ方向に摺動自在に支持されたスライダ２５と、
このスライダ２５に枢着され前記フック１７に掛けられ
る掛止部材２６と、前記スライダ２５を枢軸２３から離
れる方向に付勢するコイルばね２７などからなり、固定
板２２の内側には降着そり４．４を上方から覆うそり保
持部２８が溶接されている。このそり保持部２８は下方
へ開放された断面溝形に形成され、降着そり４に沿って
機体前後方向に延在している。The fixture 13 includes a fixing plate 22 having a through hole 21 through which the hook 17 passes, a rod-shaped fixing handle 24 pivotally attached to the fixing plate 22 with a pivot 23, and the fixing handle 24.
a slider 25 supported slidably in the length direction;
It consists of a hooking member 26 that is pivotally attached to the slider 25 and hooked to the hook 17, a coil spring 27 that urges the slider 25 away from the pivot 23, and an accretion sled 4. A sled holding part 28 that covers 4 from above is welded. The sled holding portion 28 is formed in a groove-shaped cross section that is open downward, and extends in the longitudinal direction of the aircraft body along the accretion sled 4.
２９はそり保持部２８の内側上壁面に貼着された緩衝ゴ
ムである。Reference numeral 29 denotes a cushioning rubber attached to the inner upper wall surface of the sled holding portion 28.
３１は小型無人ヘリコプタ１の機体後部を支持する支柱
である。この支柱３１は上端部に円弧状の受は部３２が
設けられ、両側部には一対のフック３３．３３が突設さ
れている。３４はこれらフック３３．３３間に掛けられ
るバンド、３５は機体後部と受は部３２との間に介装さ
れる緩衝材である。ここで、本実施例においては、床板
の平面図を第５図に示すように、床板１４の前後に二枚
の支持板１２が車幅方向に平行に配置されており、前側
の支持板１２の両側部および後側の支持板１２の中央部
にそれぞれ支柱３１が配置されている。Reference numeral 31 denotes a support column that supports the rear part of the small unmanned helicopter 1. This support column 31 is provided with an arcuate receiving portion 32 at its upper end, and a pair of hooks 33, 33 are provided protruding from both sides. 34 is a band hung between these hooks 33, 33, and 35 is a cushioning material interposed between the rear part of the fuselage and the receiver part 32. Here, in this embodiment, as shown in the plan view of the floor plate in FIG. Pillars 31 are arranged at both sides of the support plate 12 and at the center of the rear support plate 12, respectively.
このように構成された小型無人ヘリコプタの運搬装置に
おいては、小型無人ヘリコプタ１を運搬する時は、先ず
、取付ボルト１５を床板１４に螺合させて床板１４上に
支持板１２を取付ける。次いで、小型無人ヘリコプタ１
を降着そり４が支持板１２で支承され、機体後部が支柱
３１で支承されるように載置する。そして、そり保持部
２８が降着そり４を上方から覆いかつフック１７が透孔
２１を貫通するように固定具１３を載置し、第２図中鎖
線で示すように掛止部材２６をフ・ツク１７に掛止させ
る。この状態で固定ハンドル２４をコイルばね２７の弾
撥力に抗して押し下げると、第２図中実線で示すように
、掛止部材２６の枢着部が枢軸２３よりも下方へ回動す
るため、固定板２２はコイルばね２７の弾撥力によって
床板１４側へ押圧され固定具１３は支持板１２に固定さ
れる。In the transport device for a small unmanned helicopter configured as described above, when transporting the small unmanned helicopter 1, first, the mounting bolts 15 are screwed into the floor plate 14, and the support plate 12 is mounted on the floor plate 14. Next, small unmanned helicopter 1
is placed so that the landing sled 4 is supported by the support plate 12 and the rear part of the fuselage is supported by the strut 31. Then, the fixture 13 is placed so that the sled holding part 28 covers the accretion sled 4 from above and the hook 17 passes through the through hole 21, and the hooking member 26 is opened as shown by the chain line in FIG. Hook it on hook 17. In this state, when the fixed handle 24 is pushed down against the elastic force of the coil spring 27, the pivoting part of the latching member 26 rotates downward relative to the pivot 23, as shown by the solid line in FIG. The fixing plate 22 is pressed toward the floor plate 14 by the elastic force of the coil spring 27, and the fixture 13 is fixed to the support plate 12.
したがって、固定具１３のそり保持部２８によって降着
そり４を保持することができる。そのため、機体２を支
持するために比較的強度を有している降着そり４を利用
して小型無人ヘリコプタ１を床板１４上に固定すること
ができるから、機体２などを利用して固定する構造に比
較して確実に荷台に固定することができる。そのため、
運搬中に路面の凹凸によって、小型無人ヘリコプタ１が
跳ねたり、車両の加減速時に移動するのを防止できるか
ら、小型無人ヘリコプタ１が互いにあるいは車両の荷台
に接触するを防止し、運搬時に破損するのを防止するこ
とができる。しかも、緩衝ゴム２９で降着そり４を保持
しているから、降着そり４を傷めたりするおそれもない
。Therefore, the accretion sled 4 can be held by the sled holding portion 28 of the fixture 13. Therefore, since the small unmanned helicopter 1 can be fixed on the floor plate 14 by using the landing sled 4 which has a relatively strong strength to support the fuselage 2, a structure in which the small unmanned helicopter 1 is fixed using the fuselage 2 etc. It can be fixed to the loading platform more reliably than the previous model. Therefore,
Since it is possible to prevent the small unmanned helicopters 1 from bouncing due to unevenness of the road surface during transportation and from moving when the vehicle accelerates or decelerates, it is possible to prevent the small unmanned helicopters 1 from coming into contact with each other or with the loading platform of the vehicle, resulting in damage during transportation. can be prevented. Furthermore, since the accretion sled 4 is held by the buffer rubber 29, there is no risk of damaging the accretion sled 4.
一方、固定ハンドル２４を上方へ引き上げれば、掛止部
材２６をフック１７から外すことができる。On the other hand, by pulling up the fixed handle 24, the latching member 26 can be removed from the hook 17.
そして、この状態で固定具１３を上方へ持ち上げれば降
着そり４の保持を解除することができる。Then, by lifting the fixture 13 upward in this state, the holding of the landing sled 4 can be released.
また、実施例においては、機体後部を支柱３１で支持し
ているので、機体後部を支持している機体前部に加わる
荷重を軽減することができる。さらに、支持板１２の降
着そり支承部および支柱３１を車幅方向に交互に並べて
いるので、トラックの荷台を有効に利用し、３台の小型
無人ヘリコプタ１をコンパクトに搭載することができる
。Furthermore, in the embodiment, since the rear part of the fuselage is supported by the struts 31, it is possible to reduce the load applied to the front part of the fuselage that supports the rear part of the fuselage. Further, since the landing sled support portions of the support plate 12 and the struts 31 are arranged alternately in the vehicle width direction, the truck bed can be used effectively and three small unmanned helicopters 1 can be mounted compactly.
以上説明したように本発明によれば、荷台の床板に着脱
自在に取付けられ小型無人ヘリコプタの降着そりを支承
する支持板と、この支持板に着脱自在に取付けられ降着
そりを上方から覆うそり保持部を有する固定具とから構
成したから、運搬時において、荷台の床板上に支持板を
取付け、この支持板上に小型無人ヘリコプタを載置して
固定具を取付けることによって、降着そりをそり保持部
で保持することができる。As explained above, according to the present invention, there is provided a support plate that is detachably attached to the floor plate of a loading platform and supports the landing sled of a small unmanned helicopter, and a sled holder that is detachably attached to the support plate and covers the landing sled from above. During transportation, the landing sled can be held in place by attaching a support plate to the floor plate of the loading platform, placing the small unmanned helicopter on this support plate, and attaching the fixing device. It can be held in the section.
したがって、比較的強度を有する降着そりを利用して固
定することができるから、小型無人ヘリコプタを確実に
荷台に固定することができる。Therefore, the small unmanned helicopter can be securely fixed to the cargo platform because it can be fixed using the relatively strong landing sled.
第１図は本発明に係る運搬装置で小型無人ヘリコプタを
固定した状態を示す斜視図、第２図は第１図のｎ−ｎ線
断面図、第３図は支持板を示す斜視図、第４図は機体右
側の固定具を示す斜視図、第５図は荷台の床板を示す平
面図である。
４・・・・降着そり、１１・・・・運搬装置、１２・・
・・支持板、１３・・・・固定具、１４・・・・床板、
２２・・・・固定板、２８・・・・保持部。
特許出願人 ヤマハ発動機株式会社FIG. 1 is a perspective view showing a state in which a small unmanned helicopter is fixed with the transportation device according to the present invention, FIG. 2 is a sectional view taken along the line nn of FIG. 1, and FIG. FIG. 4 is a perspective view showing the fixture on the right side of the fuselage, and FIG. 5 is a plan view showing the floor plate of the cargo platform. 4...Accretion sled, 11...Transportation device, 12...
・・Support plate, 13・・Fixing tool, 14・・・Floor board,
22... Fixed plate, 28... Holding part. Patent applicant Yamaha Motor Co., Ltd.
Claims (1)
の左右一対の降着そりを支承する支持板と、この支持板
に着脱自在に取付けられ前記降着そりを上方から覆うそ
り保持部を有する固定具とからなる小型無人ヘリコプタ
の運搬装置。A support plate that is detachably attached to the floor plate of a cargo platform and supports a pair of left and right landing sleds of a small unmanned helicopter, and a fixture that is detachably attached to the support plate and has a sled holding part that covers the landing sled from above. A small unmanned helicopter transport device.
Priority Applications (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP63153562A JP2694537B2 (en) | 1988-06-23 | 1988-06-23 | Small unmanned helicopter carrier |
| JP15356289A JPH0324951A (en) | 1988-06-09 | 1989-06-15 | Multi-layer polymer film |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP63153562A JP2694537B2 (en) | 1988-06-23 | 1988-06-23 | Small unmanned helicopter carrier |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPH026244A true JPH026244A (en) | 1990-01-10 |
| JP2694537B2 JP2694537B2 (en) | 1997-12-24 |
Family
ID=15565210
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP63153562A Expired - Fee Related JP2694537B2 (en) | 1988-06-09 | 1988-06-23 | Small unmanned helicopter carrier |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JP2694537B2 (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5607270A (en) * | 1994-04-28 | 1997-03-04 | Zimmerman; Karl M. | Retention system for transporting ski-type vehicles |
| US5785471A (en) * | 1997-01-28 | 1998-07-28 | Godbersen; Byron L. | Ski bar tie down device for a snowmobile trailer |
| US5816757A (en) * | 1996-12-31 | 1998-10-06 | Huston; Ronald Wayne | Utility trailer retaining bar hold down clamp |
| JP2011046364A (en) * | 2009-08-28 | 2011-03-10 | Yanmar Co Ltd | On-vehicle device for transportation of unmanned helicopter |
| CN105730313A (en) * | 2016-04-15 | 2016-07-06 | 西安天鹰防务科技有限公司 | Automatic locking device for unmanned aerial vehicle on vehicle-mounted landing platform |
Citations (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH01108841U (en) * | 1988-01-14 | 1989-07-24 |
-
1988
- 1988-06-23 JP JP63153562A patent/JP2694537B2/en not_active Expired - Fee Related
Patent Citations (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH01108841U (en) * | 1988-01-14 | 1989-07-24 |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5607270A (en) * | 1994-04-28 | 1997-03-04 | Zimmerman; Karl M. | Retention system for transporting ski-type vehicles |
| US5816757A (en) * | 1996-12-31 | 1998-10-06 | Huston; Ronald Wayne | Utility trailer retaining bar hold down clamp |
| US5785471A (en) * | 1997-01-28 | 1998-07-28 | Godbersen; Byron L. | Ski bar tie down device for a snowmobile trailer |
| JP2011046364A (en) * | 2009-08-28 | 2011-03-10 | Yanmar Co Ltd | On-vehicle device for transportation of unmanned helicopter |
| CN105730313A (en) * | 2016-04-15 | 2016-07-06 | 西安天鹰防务科技有限公司 | Automatic locking device for unmanned aerial vehicle on vehicle-mounted landing platform |
Also Published As
| Publication number | Publication date |
|---|---|
| JP2694537B2 (en) | 1997-12-24 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| LAPS | Cancellation because of no payment of annual fees |