Deprecated: The each() function is deprecated. This message will be suppressed on further calls in /home/zhenxiangba/zhenxiangba.com/public_html/phproxy-improved-master/index.php on line 456
JP2694537B2 - Small unmanned helicopter carrier - Google Patents
[go: Go Back, main page]

JP2694537B2 - Small unmanned helicopter carrier - Google Patents

Small unmanned helicopter carrier

Info

Publication number
JP2694537B2
JP2694537B2 JP63153562A JP15356288A JP2694537B2 JP 2694537 B2 JP2694537 B2 JP 2694537B2 JP 63153562 A JP63153562 A JP 63153562A JP 15356288 A JP15356288 A JP 15356288A JP 2694537 B2 JP2694537 B2 JP 2694537B2
Authority
JP
Japan
Prior art keywords
sled
unmanned helicopter
support plate
small unmanned
landing
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
JP63153562A
Other languages
Japanese (ja)
Other versions
JPH026244A (en
Inventor
昭英 谷山
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.)
Yamaha Motor Co Ltd
Original Assignee
Yamaha Motor Co 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 Yamaha Motor Co Ltd filed Critical Yamaha Motor Co Ltd
Priority to JP63153562A priority Critical patent/JP2694537B2/en
Priority to JP15356289A priority patent/JPH0324951A/en
Publication of JPH026244A publication Critical patent/JPH026244A/en
Application granted granted Critical
Publication of JP2694537B2 publication Critical patent/JP2694537B2/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Landscapes

  • Handcart (AREA)
  • Toys (AREA)

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。
Description: TECHNICAL FIELD The present invention relates to a radio-controlled small unmanned helicopter carrier used for, for example, spraying medicine.

〔従来の技術〕[Conventional technology]

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 various purposes such as mounting a spraying device to spray a medicine, or mounting a camera to investigate and search a dangerous place.

そして、この様な小型無人ヘリコプタを使用する場合
は、トラックやバ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 such a small unmanned helicopter, it is desirable to transport it to the destination by using a truck or van type vehicle.

〔発明が解決しようとする課題〕[Problems to be solved by the invention]

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 fix the small unmanned helicopter to the loading platform so that it will not bounce due to unevenness of the road surface or move during acceleration / deceleration of the vehicle, but the small unmanned helicopter has a complicated shape. In addition to the fact that the fuselage is often made from a resin material, etc., it does not have enough strength, so it is extremely difficult to securely fix it using ropes that have been known so far. There is. The present invention has been made in view of such circumstances, and provides a carrying device for a small unmanned helicopter capable of securely fixing the small unmanned helicopter to a luggage carrier.

〔課題を解決するための手段〕[Means for solving the problem]

本発明に係る運搬装置は、荷台の床板に取付けられ小
型無人ヘリコプタの左右一対の降着そりを支承する支持
板と、この支持板に支承された降着そりの長手方向の一
端側から見て下方に向けて開く凹状のそり保持部で降着
そりを上方から覆うことによって前記支持板上に降着そ
りを保持する固定具とを備え、この固定具を、前記そり
保持部における前記無人ヘリコプタの機体外側の一側部
を片持ち式に支持する構造とするとともに、前記無人ヘ
リコプタの機体の下方へ離隔可能に前記支持板に取付け
たものである。
The carrying device according to the present invention includes a support plate that is attached to a floor plate of a cargo bed and supports a pair of left and right landing sledges of a small unmanned helicopter, and downwards when viewed from one end side in the longitudinal direction of the landing sledge supported by the support plates. With a fixture for holding the accretion sled on the support plate by covering the accretion sled from above with a concave sled holding portion that opens toward, this fixing device is provided on the outer side of the unmanned helicopter in the sled holding portion. The one side portion is supported in a cantilever manner, and is attached to the support plate so as to be separated below the airframe of the unmanned helicopter.

〔作用〕[Action]

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, the support plate is attached on the floor plate of the cargo bed,
When a small unmanned helicopter is placed on this support plate and a fixture is attached, the landing sled is held by the sled holding portion.

〔実施例〕〔Example〕

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II-II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図に符号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, an embodiment of the present invention will be described in detail with reference to the drawings.
1 is a perspective view showing a state in which a small unmanned helicopter is fixed by a carrying device according to the present invention, FIG. 2 is a sectional view taken along the line II-II of FIG. 1, FIG. 3 is a perspective view showing a support plate, and FIG. FIG. 4 is a perspective view showing a fixture on the right side of the machine body. A small unmanned helicopter denoted by reference numeral 1 in FIG. 1 is provided with a pair of left and right landing sleds 4, 4 on the lower portion of the body 2 via front and rear support legs 3, 3. These landing sleds 4, 4 extend in the front-back direction of the machine body 2, and auxiliary wheels 5, 5 used for lifting and carrying the rear part of the machine body are rotatably provided at a front end portion bent upward. It is supported. Reference numeral 6 denotes a main rotor that is rotatably driven by an engine housed in the front portion of the machine body 2, and reference numeral 7 denotes an auxiliary rotor blade that is arranged at the rear portion of the machine body 2 and that cancels the drive 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。この運搬
装置11は降着そり4,4を支承する支持板12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2の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13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。取付ボルト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。
11 is a small unmanned helicopter carrier. The carrying device 11 includes a support plate 12 that supports the landing sledges 4, 4 and a fixture 13 that is detachably attached to the support plate 12. The support plate 12 is formed in the shape of a strip plate extending in the width direction of the machine body 2, and at a portion corresponding to the inside of the landing sled 4, 4, a mounting bolt 15 for screwing the support plate 12 to a floor plate 14 of a truck carrier. A through hole 16 is formed, and a hook for fixing the fixture 13 to the support plate 12 is provided at a portion corresponding to the outside of the landing sled 4, 4.
17 are protruding. The head of the mounting bolt 15 is provided with a handle 18 for rotating the bolt without using a tool.

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が、前
記支持板12に支承された降着そり4の長手方向の一端側
から見て下方に向けて開く凹状、すなわち下方へ開放さ
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。また、そり保持部28における小型
無人ヘリコプタ1の機体外側の一側部を、この固定具13
の前記固定板22が片持ち式に支持している。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。
The fixing tool 13 has a fixing plate 22 having a through hole 21 through which the hook 17 penetrates, and a rod-shaped fixing handle 24 pivotally attached by a pivot 23.
A slider 25 slidably supported in the longitudinal direction on the fixed handle 24, a hooking member 26 pivotally attached to the slider 25 and hung on the hook 17, and the slider 25 separated from the pivot 23. A sled holding portion 28 that covers the landing sleds 4, 4 from above is welded to the inside of the fixed plate 22. The sled holding portion 28 is formed in a concave shape that opens downward when viewed from one end side in the longitudinal direction of the landing sled 4 supported by the support plate 12, that is, in a cross-sectional groove shape that opens downward. Along the front and back of the machine. In addition, one side of the sled holding portion 28 outside the fuselage of the small unmanned helicopter 1 is fixed to the fixing member 13
The fixed plate 22 is supported in a cantilever manner. Reference numeral 29 is 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け部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
は機体後部と受け部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 is a column that supports the rear portion of the body of the small unmanned helicopter 1. An arcuate receiving portion 32 is provided at the upper end of the column 31, and a pair of hooks 33, 33 are provided on both sides so as to project. 34 is a band that can be hung between these hooks 33, 33,
Is a cushioning material interposed between the rear portion of the machine body and the receiving portion 32. Here, in the present embodiment, a plan view of the floorboard is shown in FIG.
As shown in the figure, two support plates 12 are arranged in parallel in the vehicle width direction in front of and behind the floor plate 14, and support columns are provided at both sides of the front support plate 12 and at the center of the rear support plate 12, respectively. 31 are arranged.

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をフック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の枢着部が枢着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 carrying the small unmanned helicopter 1 thus constructed, when carrying the small unmanned helicopter 1, first, the mounting bolts 15 are screwed into the floor plate 14 to mount the support plate 12 on the floor plate 14. Next, the small unmanned helicopter 1 is mounted so that the landing sled 4 is supported by the support plate 12 and the rear part of the body is supported by the support column 31. Then, the sled holding portion 28 covers the landing sled 4 from above, and the fixture 13 is placed so that the hook 17 penetrates the through hole 21, and the hooking member 26 is hooked to the hook 17 as shown by a chain line in FIG. Hang on. In this state, when the fixed handle 24 is pushed down against the elastic force of the coil spring 27, the pivot portion of the latch member 26 pivots 23 as shown by the solid line in FIG.
Since the fixing plate 22 is rotated downward, the fixing plate 22 is pressed toward the floor plate 14 side by the elastic force of the coil spring 27, and the fixing tool 13 is fixed to the supporting plate 12.
Fixed to

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 sled holder 28 of the fixture 13 can hold the landing sled 4. Therefore, since the small unmanned helicopter 1 can be fixed on the floor board 14 by using the landing sled 4 having a relatively high strength to support the body 2, a structure for fixing the body 2 etc. It can be securely fixed to the cargo bed as compared with. Therefore, it is possible to prevent the small unmanned helicopter 1 from bouncing or moving during acceleration / deceleration of the vehicle due to unevenness of the road surface during transportation.
It is possible to prevent the small unmanned helicopter 1 from contacting each other or the bed of the vehicle, and prevent damage during transportation. Moreover, since the cushioning rubber 29 holds the landing sled 4, there is no possibility of damaging the landing sled 4.

一方、固定ハンドル24を上方から引き上げれば、掛止
部材26をフック17から外すことができる。そして、この
状態で固定具13を上方に持ち上げて小型無人ヘリコプタ
1の機体の外方へ離隔させることによって、降着そり4
の保持を解除することができる。
On the other hand, by pulling up the fixed handle 24 from above, the locking member 26 can be removed from the hook 17. Then, in this state, the fixture 13 is lifted upward to separate it from the body of the small unmanned helicopter 1 so that the landing sled 4
Can be released.

したがって、この運搬装置によれば、固定具13のそり
保持部28を降着そり4に被せて降着そり4を支持板12上
に保持するときの作業および前記そり保持部28を降着そ
り4の上方から外す作業を、降着そり4の外側の広く解
放された空間で行うことができるから、前記作業がし易
い。
Therefore, according to this carrying device, the work of covering the sled holding portion 28 of the fixture 13 on the landing sled 4 and holding the landing sled 4 on the support plate 12 and the sled holding portion 28 above the landing sled 4 are performed. Since the work for removing the work can be performed in a widely opened space outside the landing sled 4, the work is easy.

しかも、固定具13はそり保持部28の一側を片持ち式に
支持しているので、固定具13を簡単な取付構造で支持板
12に取付けることができる。これは、固定具13における
そり保持部28を支持する部分に近い1箇所を支持板12に
取付ければよいからである。
Moreover, since the fixture 13 supports one side of the sled holding portion 28 in a cantilever manner, the fixture 13 has a simple mounting structure.
Can be installed on 12. This is because it is sufficient to attach one position near the portion of the fixture 13 that supports the sled holding portion 28 to the support plate 12.

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。
Further, in the embodiment, since the rear part of the machine body is supported by the column 31, it is possible to reduce the load applied to the front part of the machine body supporting the rear part of the machine body. Further, since the landing sled bearings of the support plate 12 and the columns 31 are alternately arranged in the vehicle width direction, the truck bed can be effectively used and three small unmanned helicopters 1 can be compactly mounted.

〔発明の効果〕〔The invention's effect〕

以上説明したように、本発明に係る小型無人ヘリコプ
タの運搬装置は、荷台の床板に取付けられ小型無人ヘリ
コプタの左右一対の降着そりを支承する支持板と、この
支持板に支承された降着そりの長手方向の一端側から見
て下方に向けて開く凹状のそり保持部で降着そりを上方
から覆うことによって前記支持板上に降着そりを保持す
る固定具とを備え、この固定具を、前記そり保持部にお
ける前記無人ヘリコプタの機体外側の一側部を片持ち式
に支持する構造とするとともに、前記無人ヘリコプタの
機体の下方へ離隔可能に前記支持板に取付けたため、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 described above, the carrier device for a small unmanned helicopter according to the present invention includes a support plate that is attached to the floor plate of the loading platform and that supports a pair of left and right landing sleds of the small unmanned helicopter, and a landing sled supported on this support plate. A fixture for holding the landing sled on the support plate by covering the landing sled from above with a concave sled holding portion that opens downward when viewed from one end side in the longitudinal direction, Since the one side of the outside of the unmanned helicopter in the holding part is supported in a cantilever manner, and the unmanned helicopter is attached to the support plate so that it can be separated below the fuselage, the floor plate of the loading platform during transportation. By mounting a support plate on top, mounting a small unmanned helicopter on this support plate and mounting a fixture, the landing sled can be held by the sled holder.

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。また、固定具のそり保
持部を降着そりに被せて降着そりを支持板上に保持する
ときの作業および前記そり保持部を降着そりの上方から
外す作業を、降着そりの外側の広く解放された空間で行
うことができる。このため、前記作業を容易に実施する
ことができる。
Therefore, since the landing sled having a relatively high strength can be used for fixing, the small unmanned helicopter can be reliably fixed to the luggage carrier. Further, the work of covering the sled holding part of the fixture on the accretion sled and holding the accretion sled on the support plate and the work of removing the sled holding part from above the accretion sled were widely released outside the accretion sled. Can be done in space. Therefore, the work can be easily performed.

さらに、固定具はそり保持部の一側を片持ち式に支持
しているので、固定具を簡単な取付構造で支持板に取付
けることができる。これは、固定具におけるそり保持部
を支持する部分に近い1箇所を支持板に取付ければよい
からである。
Furthermore, since the fixture supports one side of the sled holder in a cantilever manner, the fixture can be attached to the support plate with a simple attachment structure. This is because it is only necessary to attach one location near the portion of the fixture that supports the sled holding portion to the support plate.

【図面の簡単な説明】[Brief description of the drawings]

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II-II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。
1 is a perspective view showing a state in which a small unmanned helicopter is fixed by a carrying device according to the present invention, FIG. 2 is a sectional view taken along the line II-II of FIG. 1, FIG. 3 is a perspective view showing a support plate, and FIG. FIG. 4 is a perspective view showing a fixture on the right side of the machine body, and FIG. 5 is a plan view showing a floor plate of the luggage carrier. 4 ... Accretion sled, 11 ... Carriage device, 12 ... Support plate, 13 ...
… Fixing tool, 14 …… Floor plate, 22 …… Fixing plate, 28 …… Holding part.

Claims (1)

(57)【特許請求の範囲】(57) [Claims] 【請求項1】荷台の床板に取付けられ小型無人ヘリコプ
タの左右一対の降着そりを支承する支持板と、この支持
板に支承された降着そりの長手方向の一端側から見て下
方に向けて開く凹状のそり保持部で降着そりを上方から
覆うことによって前記支持板上に降着そりを保持する固
定具を備え、この固定具を、前記そり保持部における前
記無人ヘリコプタの機体外側の一側部を片持ち式に支持
する構造とするとともに、前記無人ヘリコプタの機体の
下方へ離隔可能に前記支持板に取付けたことを特徴とす
る小型無人ヘリコプタの運搬装置。
1. A support plate which is attached to a floor plate of a cargo bed and supports a pair of left and right landing sledges of a small unmanned helicopter, and the landing sledges supported by the support plates open downward as viewed from one end side in the longitudinal direction. A fixture for holding the accretion sled on the support plate by covering the accretion sled from above with a concave sled holding portion is provided, and this fixing device is provided on one side outside the fuselage of the unmanned helicopter in the sled holding portion. A carrier device for a small unmanned helicopter, which has a structure of supporting in a cantilever manner and is attached to the support plate so as to be separated below the body of the unmanned helicopter.
JP63153562A 1988-06-09 1988-06-23 Small unmanned helicopter carrier Expired - Fee Related JP2694537B2 (en)

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 JPH026244A (en) 1990-01-10
JP2694537B2 true 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)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
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
JP5362488B2 (en) * 2009-08-28 2013-12-11 ヤンマー株式会社 In-vehicle device for transporting unmanned helicopters
CN105730313B (en) * 2016-04-15 2019-01-01 芜湖文青机械设备设计有限公司 The forced locking device of unmanned plane on a kind of vehicle-mounted platform that rises and falls
CN116022348A (en) * 2022-12-29 2023-04-28 南京模拟技术研究所 A helicopter transport fixture

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH01108841U (en) * 1988-01-14 1989-07-24

Also Published As

Publication number Publication date
JPH026244A (en) 1990-01-10

Similar Documents

Publication Publication Date Title
US2338955A (en) Automobile carrier
CN210822281U (en) Anti-sliding track platform lorry
JP2694537B2 (en) Small unmanned helicopter carrier
KR20190090709A (en) Stowage system for stowing a two-wheeled vehicle in a motor vehicle
CA2490313C (en) Snowmobile support stand
US3989265A (en) Trailer for boat and motorcycle
CZ20002535A3 (en) Device for location and transportation of motorcycle
FR2648099A1 (en) Handling trolley with a tilting lifting platform
KR100832898B1 (en) Model Airplane Safety Carrier
CN220865566U (en) All-terrain vehicle
JPS61146655A (en) Sliding roof carrier
CN211252659U (en) Missile tail cabin transfer car (buggy)
CN212500096U (en) Multifunctional trailer
KR101765418B1 (en) Carrier Apparatus for a Vehicle
CN211075989U (en) Automatic upset boat tail cabin transfer car (buggy)
JPS6064099A (en) Rail device for loading loading article on outside of helicopter
CN213649452U (en) Self-discharging automobile packing box climbing mechanism and self-discharging automobile
JPH0616089A (en) Step for truck deck
JPH0638874Y2 (en) Forklift truck
JP3693284B2 (en) Battery mounting device for battery car
JPH054443Y2 (en)
JPS5932339B2 (en) roof carrier
JPH055075Y2 (en)
JP2009012956A (en) Locking device mounted on a car or the like in a picking vehicle
RU2048999C1 (en) Device for securing cars on transportation platform

Legal Events

Date Code Title Description
LAPS Cancellation because of no payment of annual fees