JPH06227496A - Installation structure for buffer member - Google Patents

Installation structure for buffer member

Info

Publication number
JPH06227496A
JPH06227496A JP3947193A JP3947193A JPH06227496A JP H06227496 A JPH06227496 A JP H06227496A JP 3947193 A JP3947193 A JP 3947193A JP 3947193 A JP3947193 A JP 3947193A JP H06227496 A JPH06227496 A JP H06227496A
Authority
JP
Japan
Prior art keywords
pallet
cushioning material
landing
cushioning
buffer
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
Application number
JP3947193A
Other languages
Japanese (ja)
Other versions
JP3190470B2 (en
Inventor
Akira Nishida
晃 西田
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.)
Showa Aircraft Industry Co Ltd
Original Assignee
Showa Aircraft Industry 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 Showa Aircraft Industry Co Ltd filed Critical Showa Aircraft Industry Co Ltd
Priority to JP03947193A priority Critical patent/JP3190470B2/en
Publication of JPH06227496A publication Critical patent/JPH06227496A/en
Application granted granted Critical
Publication of JP3190470B2 publication Critical patent/JP3190470B2/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Landscapes

  • Pallets (AREA)

Abstract

PURPOSE:To facilitate the demounting and disassembly work in a simple manner from above a pallet for a mounted article after landing by allowing a buffer member to be shiftable between a preparatory position in the vicinity of the edge and a buffer position under the pallet. CONSTITUTION:The installation structure of a buffer member 18 is used in the case where an article 3 mounted on an axle 2, etc., installed on a pallet 1 equipped with a parachute, i.e., a main umbrella 4 is thrown into air, and the article 3 is supended under the opened main unbrella 4, and landed. When the buffer member 18 is mounted into an aircraft 7, the article 3 is held at a preparatory position A in the vicinity of the rear edge of the mounted article 3 by a holding member, and displaced by a pulling means such as a wire 20, in the air in the intermediate course of drop, and positioned at a buffer position B under the pallet 1.

Description

【発明の詳細な説明】Detailed Description of the Invention

【0001】[0001]

【産業上の利用分野】本発明は緩衝材の装着構造に関す
る。すなわち、航空機から落下傘付で空中に投下された
車輌等の搭載物を着地時の落下衝撃から防護する、緩衝
材の装着構造に関するものである。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a cushioning material mounting structure. That is, the present invention relates to a cushioning material mounting structure for protecting a mounted object such as a vehicle that is dropped in the air with an umbrella from an aircraft from a drop impact at the time of landing.

【0002】[0002]

【従来の技術】図8は、この種従来例の緩衝材の装着構
造を示し、落下傘つまり主傘が開傘し搭載物等が吊り下
げられた段階の側面図である。同図にも示したように、
パレット1上に取り付けられた車輌2等の搭載物3は、
航空機から主傘4等の落下傘付で空中に投下され、落下
途中の空中において開傘した主傘4の下に吊り下げられ
て、地上に着地される。そして、着地時の落下衝撃から
搭載物3を防護するため緩衝材5が装着されているが、
従来の緩衝材5の装着構造にあっては、パレット1と搭
載物3との間に緩衝材5が介裝されており、着地時の落
下衝撃を緩衝材5が潰れることにより受け、もって車輌
2等の搭載物3を落下衝撃から防護していた。
2. Description of the Related Art FIG. 8 is a side view showing a mounting structure of a cushioning material of this type of conventional example, at a stage in which a parachute, that is, a main umbrella is opened and a mounted object or the like is suspended. As shown in the figure,
The mounted object 3 such as the vehicle 2 mounted on the pallet 1 is
It is dropped from the aircraft with a parachute such as a main umbrella 4 into the air, is hung under the main umbrella 4 that has been opened in the air during the fall, and is landed on the ground. And, the cushioning material 5 is attached to protect the mounted object 3 from a drop impact at the time of landing,
In the conventional mounting structure of the cushioning material 5, the cushioning material 5 is interposed between the pallet 1 and the mounted article 3, and the shock absorbing material 5 receives a drop impact at the time of landing, so that the vehicle is The load 3 such as 2 was protected from a drop impact.

【0003】[0003]

【発明が解決しようとする課題】ところで、このような
従来例にあっては、次の問題が指摘されていた。すなわ
ち第1に、従来の緩衝材5の装着構造では、パレット1
と搭載物3との間に緩衝材5が介裝されていたので、軟
着等により緩衝材5の潰れる量が少ないと、着地時にお
いて、搭載物3が潰れていない緩衝材5を介しパレット
1上に浮き上がったままの状態となり、搭載物3である
例えば車輌2の車輪6が、所期のごとくパレット1上に
着かない事態が発生していた。そこで着地後において、
車輌2等の搭載物3をパレット1上からジャッキアップ
して、車輪6下から潰れていない緩衝材5を抜き取る作
業を要する等、搭載物3の煩雑で面倒な取り外し,解脱
作業を要するという難点があった。第2に、そこで従来
の装着構造では、着地,降着後において、搭載物3の迅
速な使用,展開ができないという問題が指摘されてい
た。例えば、着地,降着後において、搭載物3である車
輌2を直ちに発進させることができず、迅速な空挺行動
に支障が生じていた。
By the way, the following problems have been pointed out in such a conventional example. That is, first, in the conventional cushioning member 5 mounting structure, the pallet 1
Since the cushioning material 5 is interposed between the cushioning material 5 and the load 3, if the amount of the cushioning material 5 crushed by soft landing or the like is small, the load 3 is not crushed at the time of landing and the pallet is inserted through the cushioning material 5. There is a situation in which the pallet 1 does not reach the pallet 1 as expected because the wheels 6 of the vehicle 2, which is the mounted object 3, remain on the pallet 1 as expected. So after landing,
Difficulty of complicated and troublesome removal and dismantling work of the mounting object 3 such as jacking up the mounting object 3 such as the vehicle 2 from the top of the pallet 1 and extracting the uncrushed cushioning material 5 from under the wheel 6. was there. Secondly, it has been pointed out that the conventional mounting structure has a problem in that the mounted object 3 cannot be used or deployed quickly after landing and landing. For example, after landing and landing, the vehicle 2, which is the mounted object 3, cannot be immediately started, which hinders quick airborne action.

【0004】第3に、従来の装着構造では、パレット1
と搭載物3との間に緩衝材5が固定的に介裝されてお
り、全体的に高さが高かったので、航空機への搭載時に
おいて、機内の制限高さに対し空間的なゆとりが無く、
窮屈であり機内作業に支障を生じることもあるという指
摘があった。第4に、更に従来の装着構造では、パレッ
ト1と搭載物3との間に緩衝材5が介裝され、パレット
1下には緩衝材5が存在していなかったので、着地時の
落下衝撃によりパレット1が破損し易いという問題もあ
った。
Third, in the conventional mounting structure, the pallet 1
Since the cushioning material 5 is fixedly interposed between the mounting material 3 and the loading object 3 and the overall height is high, there is a spatial allowance for the restricted height inside the aircraft when it is mounted on the aircraft. Without
It was pointed out that it is cramped and may interfere with the on-board work. Fourthly, in the conventional mounting structure, since the cushioning material 5 is interposed between the pallet 1 and the mounted object 3 and the cushioning material 5 does not exist under the pallet 1, the drop impact at the time of landing is achieved. As a result, there is a problem that the pallet 1 is easily damaged.

【0005】本発明は、このような実情に鑑み、上記従
来例の問題点を解決すべくなされたものであって、緩衝
材を、端付近の準備位置とパレット下の緩衝位置とに変
位可能とすると共に、緩衝材を、機内では保持材にて準
備位置に保持し、空中でワイヤを備えた引張手段にて変
位せしめ、位置決め手段にて緩衝位置に位置決めして、
着地するようにしたことにより、第1に、着地後におけ
る搭載物のパレット上からの取り外し,解脱作業が簡単
容易化され、第2に、もって着地,降着後に搭載物が迅
速に使用,展開できると共に、第3に、航空機への搭載
時に制限高さにゆとりが生じ、第4に、着地時のパレッ
トの破損も防止され、第5に、しかもこれらが簡単な構
造により実現される、緩衝材の装着構造を提案すること
を目的とする。
In view of such circumstances, the present invention has been made to solve the problems of the above-mentioned conventional example, and the cushioning material can be displaced between a preparation position near the end and a cushioning position under the pallet. In addition, the cushioning material is held at the preparation position by the holding material inside the machine, displaced in the air by the tensioning means equipped with the wire, and positioned by the positioning means at the cushioning position.
By landing, firstly, it is possible to easily and easily remove and dismount the loaded article from the pallet after landing, and secondly, the loaded article can be quickly used and deployed after landing and landing. At the same time, thirdly, the cushioning material has a limit height when mounted on an aircraft, fourthly, the pallet is prevented from being damaged at the time of landing, and fifthly, the cushioning material is realized by a simple structure. The purpose is to propose a mounting structure for.

【0006】[0006]

【課題を解決するための手段】この目的を達成する本発
明の技術的手段は、次のとおりである。すなわち、この
緩衝材の装着構造は、落下傘付のパレット上に直接取り
付けられた車輌等の搭載物を、航空機から落下傘付で空
中に投下し、落下途中の空中において該搭載物を該パレ
ットを介し開傘した該落下傘の下に吊り下げて、着地さ
せる際に用いられ、着地時の落下衝撃から該搭載物を防
護するものである。そして、次の緩衝材,保持材,引張
手段,位置決め手段等を有してなる。すなわち、該航空
機内等では該搭載物の端の準備位置に保持され、又、落
下途中の空中においては該パレットの底面側の緩衝位置
に保持され、着地時の落下衝撃にて潰れやすい構造より
なる緩衝材と、上記準備位置にある該緩衝材と該搭載物
やパレットとの間に介裝され、該緩衝材を上記準備位置
に保持する保持材と、上記準備位置にある該緩衝材に対
し該パレットの底面を介し連結されたワイヤを備え、落
下途中の空中において、該ワイヤにて該緩衝材に引張力
を加えることが可能であり、該保持材による保持を解除
すると共に、該緩衝材を上記準備位置から緩衝位置へと
廻り込ませて保持する引張手段と、上記緩衝位置にある
該緩衝材と該パレットとの間に介裝され、該緩衝材を上
記緩衝位置に安定的に位置決めする位置決め手段と、を
有してなる。
The technical means of the present invention for achieving this object are as follows. That is, the mounting structure of the cushioning material is such that a mounted object such as a vehicle directly mounted on a pallet with a parachute is dropped from the aircraft into the air with a parachute, and the mounted object is passed through the pallet in the air during the fall. It is used for landing by hanging under the opened parachute, and protects the mounted object from a drop impact at the time of landing. Further, it has the following cushioning material, holding material, pulling means, positioning means and the like. That is, in a structure such as being held in a preparation position at the end of the loaded object in the aircraft or the like, and in a buffer position on the bottom surface side of the pallet in the middle of falling, it is more likely to be crushed by a drop impact at the time of landing. A cushioning material, a holding material interposed between the cushioning material in the preparation position and the mounted object or pallet, and holding the cushioning material in the preparation position, and the cushioning material in the preparation position. On the other hand, a wire connected through the bottom surface of the pallet is provided, and it is possible to apply a tensile force to the cushioning material with the wire in the air in the middle of falling, and release the holding by the holding material, Pulling means for wrapping the material from the preparation position to the buffering position and holding it, and interposed between the buffering material and the pallet at the buffering position, the buffering material is stably placed at the buffering position. Positioning means for positioning, And composed.

【0007】[0007]

【作用】本発明は、このような手段よりなるので、次の
ように作用する。この緩衝材の装着構造では、緩衝材
を、搭載物の端付近の準備位置とパレット下の緩衝位置
とに変位可能とすると共に、緩衝材を、航空機内への搭
載時には保持材にて準備位置に保持し、落下途中の空中
においてワイヤを備えた引張手段にて変位させ、位置決
め手段にて緩衝位置に位置決めして、着地するようにな
っている。
Since the present invention comprises such means, it operates as follows. In this cushioning material mounting structure, the cushioning material is displaceable between the preparation position near the end of the loaded object and the cushioning position under the pallet, and the cushioning material is prepared by the holding material when mounted in the aircraft. In this way, the wire is displaced by pulling means provided with a wire in the air while being dropped, positioned at a buffer position by the positioning means, and landed.

【0008】そこで第1に、車輌等の搭載物は、パレッ
ト上に直接接した状態で着地されるので、ジャッキアッ
プや緩衝材の抜き取り等の作業を要せず、パレット上か
ら簡単容易に取り外し,解脱される。第2に、そこで着
地,降着後において、車輌等の搭載物は、直ちに発進,
使用,展開できる。第3に、更に航空機への搭載時にお
いて、緩衝材は搭載物の端付近の準備位置に保持されて
いるので、搭載物やパレットの全体的高さが低く、機内
の制限高さに対し空間的なゆとりが生じる。第4に、着
地時において、パレット下の緩衝位置に緩衝材が位置決
め保持されているので、着地時の落下衝撃からパレット
も防護される。第5に、しかもこれらは、簡単な構造に
より実現される。
[0008] Therefore, firstly, since a mounted object such as a vehicle is landed on the pallet in a state of being directly in contact with the pallet, it is possible to easily and easily remove it from the pallet without the need for jacking up or removing the cushioning material. , Unleashed. Secondly, after landing and landing there, the mounted objects such as vehicles immediately start,
Can be used and expanded. Thirdly, since the cushioning material is held at the preparatory position near the end of the loaded object when it is loaded on the aircraft, the overall height of the loaded object or pallet is low, and there is space for the height limit inside the aircraft. There is a clear margin. Fourthly, since the cushioning material is positioned and held at the cushioning position under the pallet at the time of landing, the pallet is also protected from the drop impact at the time of landing. Fifth, and yet they are realized with a simple structure.

【0009】[0009]

【実施例】以下本発明を、図面に示すその実施例に基づ
いて、詳細に説明する。図1から図7は本発明の実施例
を示し、図1の側面概略図において(1)図は抽出傘が
開傘した段階を、(2)図は搭載物等が引き出された段
階を、(3)図は抽出傘と主傘が分離された段階を、
(4)図は主傘が開傘し搭載物等が吊り下げられた段階
を示す。図2から図6の側面図において、図2は航空機
内を、図3は抽出傘が開傘した段階を、図4は搭載物等
が引き出される途中の段階を、図5の(1)図は搭載物
等が引き出された段階を、図5の(2)図は抽出傘と主
傘が分離された段階を、図6は主傘が開傘し搭載物等が
吊り下げられた段階を示す。図7は緩衝材のシートパッ
ク構造を示し、(1)図は側面説明図、(3)図は斜視
説明図である。
DESCRIPTION OF THE PREFERRED EMBODIMENTS The present invention will be described in detail below based on the embodiments shown in the drawings. 1 to 7 show an embodiment of the present invention. In the schematic side view of FIG. 1, (1) shows the stage when the extraction umbrella is opened, (2) shows the stage when the loaded object is pulled out, (3) The figure shows the stage when the extraction umbrella and the main umbrella are separated,
(4) The figure shows the stage when the main umbrella is opened and the mounted items are hung. In the side views of FIGS. 2 to 6, FIG. 2 shows the inside of the aircraft, FIG. 3 shows the stage when the extraction umbrella is opened, FIG. 4 shows the stage where the loaded object is being pulled out, and FIG. Shows the stage when the loaded items are pulled out, Fig. 5 (2) shows the stage when the extraction umbrella and the main umbrella are separated, and Fig. 6 shows the stage when the main umbrella is opened and the loaded items are hung. Show. 7A and 7B show a sheet pack structure of a cushioning material, FIG. 1A is a side view, and FIG. 3C is a perspective view.

【0010】まず、主傘4等の落下傘付のパレット1上
に直接取り付けられた車輌2等の搭載物3は、航空機7
から空中に投下され、落下途中の空中においてパレット
1を介し開傘した主傘4の下に吊り下げて、地上に着地
されるようになっている。これらについて詳述すると、
まず図2等に示したように、搭載物3である車輌2は、
前後のバンド8等によりパレット1上に着脱自在に取り
付けられており、パレット1との間には、前後の車輪6
間に車輌2のスプリングを浮かせておくための緩衝部材
9が介裝されている。そして、アルミニウム製等よりな
るこのパレット1の各隅部には、主傘4の各懸吊帯10
の下端が止着されており、主傘4は車輌2上に折り畳ま
れ載置されている。
First, the mounted object 3 such as the vehicle 2 directly mounted on the pallet 1 with the parachute such as the main umbrella 4 is the aircraft 7
From the above, it is dropped into the air, and is suspended under the main umbrella 4 that has been opened via the pallet 1 in the air in the middle of falling, and landed on the ground. To explain these in detail,
First, as shown in FIG. 2 etc.,
It is detachably attached to the pallet 1 by the front and rear bands 8 and the like, and the front and rear wheels 6 are attached to the pallet 1.
A cushioning member 9 for suspending the spring of the vehicle 2 is interposed therebetween. Then, at each corner of the pallet 1 made of aluminum or the like, each suspension band 10 of the main umbrella 4 is provided.
Is fixed at its lower end, and the main umbrella 4 is folded and placed on the vehicle 2.

【0011】図2中11は袋であり、この袋11内には
畳まれた抽出傘12が収納されており、これらは航空機
7内では、フック13にて天井付近に吊り下げられてい
る。そして、この畳まれた抽出傘12は、抽出索14に
て主傘4の包カバー15に連結されており、図2に示し
たように航空機7内に搭載された状態において、この抽
出索14は、途中がフック16にてパレット1の前端を
経由するようになっている。又、図2中17は自動索で
あり、この自動索17は、航空機7の天井付近とフック
16間に配され例えばその先端にカッターを備えてお
り、搭載物3やパレット1等が機外に引き出され空中に
投下された場合に、抽出索14をフック16そしてパレ
ット1から切り離すべく機能する。
Reference numeral 11 in FIG. 2 denotes a bag, and the folded extraction umbrella 12 is accommodated in the bag 11, and these are suspended in the aircraft 7 by a hook 13 near the ceiling. The folded extraction umbrella 12 is connected to the envelope cover 15 of the main umbrella 4 by the extraction cord 14, and the extraction cord 14 is installed in the aircraft 7 as shown in FIG. Has a hook 16 on its way through the front end of the pallet 1. Reference numeral 17 in FIG. 2 denotes an automatic rope. This automatic rope 17 is arranged near the ceiling of the aircraft 7 and between the hooks 16, and has a cutter at its tip, for example. It functions to disconnect the extraction cord 14 from the hook 16 and the pallet 1 when it is pulled out and dropped in the air.

【0012】抽出傘12は、図3や図1の(1)図に示
したように、搭載物3やパレット1等の引き出しそして
空中への投下に際し、まず袋11から解放されて空中で
開傘されるが、この開傘した抽出傘12の抽出索14を
介した抽出力により、パレット1そして搭載物3が機外
へと引き出される。そして図4に示したように、パレッ
ト1等が、航空機7から引き出されて離れる際に、抽出
索14が、上述した自動索17によりパレット1から切
り離され、抽出傘12は、この抽出索14により主傘4
の包カバー15に直結される。このようにして、パレッ
ト1そして搭載物3は、抽出索14を介した抽出傘12
の抽出力にて更に空中へと引き出され、図5の(1)図
や図1の(2)図に示したように、完全に引き出され空
中に投下される。しかる後、図5の(2)図や図1の
(3)図に示したように、抽出傘12の抽出力にて包カ
バー15が主傘4から解放され、抽出傘12側と主傘4
側とが分離すると共に、主傘4が開傘する。そして図6
や図1の(4)図に示したように、搭載物3は、懸吊帯
10やパレット1を介し、このように開傘した主傘4下
に吊り下げられて、空中を降下し、地上に着地するよう
になっている。
As shown in FIG. 3 and FIG. 1 (1), the extraction umbrella 12 is first released from the bag 11 and opened in the air when the loaded article 3, the pallet 1, etc. are pulled out and dropped into the air. The pallet 1 and the mounted object 3 are pulled out of the machine by the extraction force of the opened extraction umbrella 12 through the extraction ropes 14. Then, as shown in FIG. 4, when the pallet 1 or the like is pulled out from the aircraft 7 and leaves, the extraction rope 14 is separated from the pallet 1 by the automatic rope 17 described above, and the extraction umbrella 12 is separated by the extraction rope 14 By the main umbrella 4
It is directly connected to the envelope cover 15. In this way, the pallet 1 and the mounted object 3 are connected to the extraction umbrella 12 via the extraction cord 14.
Is further extracted into the air by the extraction force of, and as shown in FIG. 5 (1) and FIG. 1 (2), it is completely extracted and dropped into the air. Then, as shown in FIG. 5 (2) and FIG. 1 (3), the wrapping cover 15 is released from the main umbrella 4 by the extraction force of the extraction umbrella 12, and the extraction umbrella 12 side and the main umbrella. Four
The main umbrella 4 opens as the side separates. And FIG.
As shown in FIG. 1 (4), the mounted object 3 is suspended under the main umbrella 4 thus opened via the suspension belt 10 and the pallet 1, and descends in the air. It is designed to land on the ground.

【0013】次に、緩衝材18およびその装着構造につ
いて述べる。上述した着地時の落下衝撃から搭載物3を
防護するため緩衝材18が装着されているが、この装着
構造は、次の緩衝材18,保持材19,ワイヤ20等の
引張手段,位置決め手段21等を有してなる。
Next, the cushioning material 18 and its mounting structure will be described. The cushioning material 18 is attached to protect the mounting object 3 from the above-described drop impact at the time of landing. This attachment structure has the following cushioning material 18, holding material 19, tension means for the wire 20, etc., and positioning means 21. And so on.

【0014】これらについて詳述すると、緩衝材18
は、まず航空機7内等では、車輌2等の搭載物3の引き
出し方向の後端付近の準備位置Aに保持され(図2,図
3等参照)、又、落下途中の空中においては、パレット
1の底面側の緩衝位置Bに保持され(図6等参照)、着
地時の落下衝撃にて潰れやすい構造よりなる。すなわち
緩衝材8は、軽量で潰れやすい例えばペーパー製のハニ
カムコアやエアマットよりなると共に、図示例ではシー
トパック方式にて包装されている。つまり図7に示した
ように、この緩衝材18は、4個等の複数個に区画,分
割されたものが用いられると共に、2枚のシート22間
に、各縫目23を介し間隔を存しつつ一連にパックされ
ている。そして緩衝材18は、準備位置Aでは図7の
(1)図中において想像線にて示したように、間隔部分
のシート22が折り込まれて縦に積み重ねられ、又、緩
衝位置Bでは図7の(1)図中において実線にて示さ
れ、更に図7の(2)図に示されたように、横に間隔を
存しつつ一連に展開される。
More specifically, the cushioning material 18
Is first held in the preparation position A near the rear end of the loading object 3 such as the vehicle 2 in the airplane 7 or the like (see FIGS. 2 and 3), and in the air during the fall, the pallet It is held at a buffer position B on the bottom side of 1 (see FIG. 6 etc.) and has a structure that is easily crushed by a drop impact at the time of landing. That is, the cushioning material 8 is made of a lightweight and crushable material such as a honeycomb core made of paper or an air mat, and is packaged in a sheet pack system in the illustrated example. That is, as shown in FIG. 7, this cushioning material 18 is used by being divided and divided into a plurality of pieces such as four pieces, and at the same time, there is a space between each of the two sheets 22 through each stitch 23. While being packed in a series. The cushioning material 18 is vertically stacked at the preparation position A as shown by the imaginary line in FIG. 7 (1), and the cushioning material 18 is vertically stacked at the cushioning position B. 7 (1), it is shown in solid lines, and as shown in FIG. 7 (2), it is developed in series with a lateral gap.

【0015】次に、保持材19について述べる。保持材
19は、準備位置Aにある緩衝材18と搭載物3やパレ
ット1との間に介裝され、緩衝材18を準備位置Aに保
持する。すなわち図2中に示した例では、このような保
持材19として包帯状の紐が用いられており、このよう
な保持材19が、積み重ねられて準備位置Aをとる各緩
衝材18と車輌2との間を各々縛着すると共に、後述に
よりワイヤ20にて引張力が加わった際には、上側のも
のから順次切断可能で、準備位置Aにおける緩衝材18
の保持を順次解除して行くようになっている。
Next, the holding material 19 will be described. The holding material 19 is interposed between the cushioning material 18 in the preparation position A and the mounting object 3 or the pallet 1, and holds the cushioning material 18 in the preparation position A. That is, in the example shown in FIG. 2, a band-shaped cord is used as such a holding material 19, and such a holding material 19 is stacked and each cushioning material 18 at the preparation position A and the vehicle 2 are used. When the tensile force is applied by the wire 20 as will be described later, they can be sequentially cut from the upper side, and the cushioning material 18 at the preparation position A
It is designed to release the holding of the.

【0016】次に、ワイヤ20等の引張手段について述
べる。この引張手段は、準備位置Aにある緩衝材18に
対しパレット1の底面を介し連結されたワイヤ20を備
え、落下途中の空中において、ワイヤ20にて緩衝材1
8に引張力を加えることが可能であり、もって、保持材
19による保持を解除すると共に、緩衝材18を準備位
置Aから緩衝位置Bへと廻り込ませて保持するようにな
っている。すなわち図示例では、準備位置Aに積み重ね
られた緩衝材18について、図7等に示したように、こ
れらをパックしたシート22の下端側がパレット1の後
端にフレキシブルな取付材Hにて取り付けられ、かつ図
2等に示したように、上端側にワイヤ20の一端が止着
されると共に、ワイヤ20の他端が主傘4の懸吊帯10
に止着されている。そして、このようなワイヤ20は複
数本用いられ、各々パレット1の底面に沿って平行に後
側から前側へと配されており、パレット1の底面におけ
る通し方としては、パレット1を機内で滑走させるロー
ラ間を利用する方式や、パレット1の底面に溝を設けこ
れを利用する方式、等々が考えられる。
Next, the pulling means for the wire 20 and the like will be described. This pulling means is provided with a wire 20 connected to the cushioning material 18 at the preparation position A via the bottom surface of the pallet 1, and the cushioning material 1 is connected to the cushioning material 18 by the wire 20 in the air while falling.
It is possible to apply a tensile force to 8, so that the holding by the holding member 19 is released, and the cushioning member 18 is held from the preparation position A to the cushioning position B by being wound around. That is, in the illustrated example, as for the cushioning material 18 stacked at the preparation position A, as shown in FIG. 7 and the like, the lower end side of the sheet 22 in which these are packed is attached to the rear end of the pallet 1 by the flexible attachment material H. As shown in FIG. 2 and the like, one end of the wire 20 is fixed to the upper end side, and the other end of the wire 20 is attached to the suspension band 10 of the main umbrella 4.
Is fastened to. A plurality of such wires 20 are used and are arranged in parallel along the bottom surface of the pallet 1 from the rear side to the front side. As a way of passing the bottom surface of the pallet 1, the pallet 1 is slid inside the machine. A method of using the space between the rollers, a method of providing a groove on the bottom surface of the pallet 1 and using the groove, and the like are possible.

【0017】更に、この引張手段のワイヤ20は、主傘
4が開傘した際に張られた懸吊帯10にて引張られるに
足る長さに設定されており、緩衝材18に対し、主傘4
の開傘張力を利用して、2トンから7トン程度の引張力
を加えることが可能となっている。そして、このような
引張力により、保持材19による緩衝材18の保持が順
次切断,解除され、図5の(1)図,(2)図中そして
図1の(2)図,(3)図中に示したように、緩衝材1
8が、準備位置Aから緩衝位置Bへと順次廻り込み、図
6,図7や図1の(4)図中に示したように、すべてが
緩衝位置Bにて保持されるようになっている。このよう
に図示例の引張手段では、ワイヤ20にて緩衝材18に
対し引張力を生じさせるため、主傘4の懸吊帯10にワ
イヤ20の他端を止着する方式が採用されているが、ワ
イヤ20に引張力を生じさせる方式は勿論これに限定さ
れるものではなく、例えば、ワイヤ20の他端を別途付
設される巻取装置のリールに止着し、そのスプリング等
を利用した巻取力を利用して、ワイヤ20を巻き取る方
式も考えられる。
Further, the wire 20 of the pulling means is set to have a length long enough to be pulled by the suspension belt 10 stretched when the main umbrella 4 is opened, and the wire 20 is Umbrella 4
It is possible to apply a pulling force of about 2 tons to 7 tons by utilizing the opening umbrella tension. Then, due to such a pulling force, the holding of the cushioning material 18 by the holding material 19 is sequentially cut and released, and in FIGS. 5 (1) and 5 (2) and FIGS. 1 (2) and 3 (3). As shown in the figure, the cushioning material 1
8 sequentially wraps around from the preparation position A to the buffer position B, and as shown in FIGS. 6, 7 and (4) of FIG. 1, all are held at the buffer position B. There is. As described above, in the pulling means of the illustrated example, in order to generate the pulling force on the cushioning material 18 by the wire 20, the method of fixing the other end of the wire 20 to the suspension band 10 of the main umbrella 4 is adopted. However, the method of generating a tensile force on the wire 20 is not limited to this, of course, and, for example, the other end of the wire 20 is fixed to a reel of a winding device additionally provided and its spring or the like is used. A method of winding the wire 20 by utilizing the winding force is also conceivable.

【0018】次に、位置決め手段21について述べる。
位置決め手段21は、緩衝位置Bにある緩衝材18とパ
レット1との間に介裝され、緩衝材18を緩衝位置Bに
安定的に位置決めするものである。図示例では、このよ
うな位置決め手段21としてマグネット方式が採用され
ており、図6中に示したように、パレット1の底面内に
はマグネット粉よりなる位置決め手段21が配されると
共に、対応して緩衝材18の上部内にはマグネット板よ
りなる位置決め手段21が配されている。位置決め手段
21として、図示例ではこのようにマグネット力を利用
して、緩衝位置Bの緩衝材18をパレット1の底面に吸
着せしめる方式が採用されているが、位置決め手段21
は勿論これに限定されるものではなく、マジックテープ
を利用する方式、その他各種の方式の採用が可能であ
る。
Next, the positioning means 21 will be described.
The positioning means 21 is interposed between the cushioning material 18 at the cushioning position B and the pallet 1, and stably positions the cushioning material 18 at the cushioning position B. In the illustrated example, a magnet system is adopted as the positioning means 21, and as shown in FIG. 6, the positioning means 21 made of magnet powder is arranged in the bottom surface of the pallet 1 and the positioning means 21 corresponds thereto. Positioning means 21 made of a magnet plate is arranged in the upper portion of the cushioning material 18. As the positioning means 21, in the illustrated example, a method is used in which the cushioning material 18 at the cushioning position B is attracted to the bottom surface of the pallet 1 by utilizing the magnetic force as described above.
Of course, the present invention is not limited to this, and a method using a magic tape and various other methods can be adopted.

【0019】本発明は、以上のようになっている。そこ
で以下のようになる。この緩衝材18の装着構造では、
緩衝材18を、搭載物3の後端付近の準備位置Aとパレ
ット1下の緩衝位置Bとに変位可能とすると共に、緩衝
材18を、機内では保持材19にて準備位置Aに保持
し、空中でワイヤ20を備えた引張手段にて変位させ、
位置決め手段21にて緩衝位置Bに位置決めして、着地
するようになっている。
The present invention is as described above. Then it becomes as follows. In this mounting structure of the cushioning material 18,
The cushioning material 18 is displaceable between a preparation position A near the rear end of the mounted object 3 and a cushioning position B under the pallet 1, and the cushioning material 18 is held in the preparation position A by a holding member 19 in the machine. , Displaced in the air by a pulling means equipped with a wire 20,
The positioning means 21 is positioned at the buffer position B to land.

【0020】そしてまず、航空機7内への搭載時におい
て、車輌2等の搭載物3は、畳まれた落下傘つまり主傘
4付のパレット1上に直接取り付けられており、緩衝材
18は、保持材19により搭載物3の後端付近の準備位
置Aに保持され、又、引張手段のワイヤ20は、緩衝材
18にパレット1の底面を介し連結されている(図2参
照)。そして着地地点の上空において、搭載物3は、主
傘4付のパレット1と共に航空機7内から引き出され
て、空中に投下され(図3,図4,図5および図1の
(1)図,(2)図,(3)図等参照)、もって搭載物
3は、パレット1を介し開傘した主傘4下に吊り下げら
れる(図6,図1の(4)図参照)。そしてその際、引
張手段のワイヤ20が引かれ、ワイヤ20にて緩衝材1
8に引張力が加えられることにより、緩衝材18は、保
持材19による保持が解除され、落下途中の空中におい
て、準備位置Aから緩衝位置Bに向け廻り込むように変
位せしめられる。そして緩衝材18は、ワイヤ20と取
付材Hにて両端が引張られ、パレット1の底面側の緩衝
位置Bに保持されると共に、空気抗力等により外れない
ように、位置決め手段21により緩衝位置Bに安定的に
位置決めされる。
First, at the time of mounting on the aircraft 7, the mounting object 3 such as the vehicle 2 is directly mounted on the pallet 1 with the folded parachute, that is, the main umbrella 4, and the cushioning material 18 is held. The material 19 is held at the preparation position A near the rear end of the mounting object 3, and the wire 20 of the pulling means is connected to the cushioning material 18 via the bottom surface of the pallet 1 (see FIG. 2). Then, in the sky above the landing point, the mounted object 3 is pulled out from the inside of the aircraft 7 together with the pallet 1 with the main umbrella 4 and dropped into the air (Fig. 3, Fig. 4, Fig. 5 and Fig. 1 (1) diagram, (2), (3), etc.), so that the mounted object 3 is suspended below the opened main umbrella 4 via the pallet 1 (see (4) in FIGS. 6 and 1). Then, at that time, the wire 20 of the pulling means is pulled, and the buffer material 1 is pulled by the wire 20.
By applying a tensile force to 8, the buffer material 18 is released from the holding by the holding material 19, and is displaced so as to wrap around from the preparation position A to the buffer position B in the air during the fall. Both ends of the cushioning material 18 are pulled by the wire 20 and the mounting material H, are held at the cushioning position B on the bottom surface side of the pallet 1, and are positioned by the positioning means 21 so as not to come off due to air drag or the like. Is stably positioned.

【0021】さてこのように、車輌2等の搭載物3は、
そのパレット1下の緩衝位置Bに緩衝材18が位置決め
保持された状態で、空中を降下し地上に着地する。そこ
で搭載物3は、着地時の落下衝撃により緩衝材18が潰
れ落下衝撃が吸収されることにより、落下衝撃から防護
される。そして、このような着地,降着後に、車輌2等
の搭載物3は、パレット1上から取り外され,解脱され
て、発進,使用,展開等される。さてそこで、この緩衝
材18の装着構造によると、次の第1,第2,第3,第
4,第5のようになる。
In this way, the mounted object 3 such as the vehicle 2 is
The cushioning material 18 is positioned and held at the cushioning position B under the pallet 1 and descends in the air to land on the ground. Therefore, the mounted object 3 is protected from the drop impact by the cushioning material 18 being crushed by the drop impact at the time of landing and the drop impact being absorbed. Then, after such landing and landing, the mounted object 3 such as the vehicle 2 is removed from the pallet 1 and released to be started, used and deployed. Now, according to the mounting structure of the cushioning material 18, the following first, second, third, fourth and fifth are provided.

【0022】まず第1に、車輌2等の搭載物3は、パレ
ット1上に直接接した状態で着地されるので、図8に示
したこの種従来例のように、着地時にパレット1上から
浮き上がり、例えば車輌2の車輪6がパレット1上に着
かないような事態は発生しない。従って、車輌2等の搭
載物3は、着地後におけるジャッキアップや緩衝材18
の抜き取り等の作業を要せず、パレット1上から簡単容
易に取り外され,解脱される。第2に、そこで着地,降
着後において、車輌2等の搭載物3は、直ちに発進,使
用,展開等できるようになる。
First of all, since the mounted object 3 such as the vehicle 2 is landed on the pallet 1 in a state of being directly in contact with the pallet 1, the pallet 1 is landed on the pallet 1 at the time of landing like the conventional example of this kind shown in FIG. It does not occur that the wheels 6 of the vehicle 2 float up and the wheels 6 of the vehicle 2 do not reach the pallet 1, for example. Therefore, the mounted object 3 such as the vehicle 2 is jacked up and the cushioning material 18 after landing.
It can be easily and easily removed from the pallet 1 and released without the need for work such as removing. Secondly, after landing and landing there, the mounted object 3 such as the vehicle 2 can be immediately started, used and deployed.

【0023】第3に、更に航空機7への搭載時におい
て、緩衝材18は、搭載物3の後端付近の準備位置Aに
縦に保持されている。そこで、図8に示したこの種従来
例に比し、搭載物3やパレット1の全体的高さが低くな
り、機内の制限高さに対し空間的なゆとりが生じる。第
4に、着地時において、パレット1下の緩衝位置Bに緩
衝材18が位置決め保持されているので、着地時の落下
衝撃からパレット1も防護される。第5に、しかもこれ
らは、従来よりの車輌2等の搭載物3,パレット1,主
傘4等の落下傘等々をそのまま利用すると共に、所定の
緩衝材18,保持材19,ワイヤ20等の引張手段,位
置決め手段21等を設けるだけでよく、簡単な構造によ
り実現される。
Thirdly, the cushioning material 18 is vertically held at the preparation position A near the rear end of the mounting object 3 when it is mounted on the aircraft 7. Therefore, as compared with the conventional example of this type shown in FIG. 8, the overall height of the mounting object 3 and the pallet 1 is reduced, and a spatial allowance is generated with respect to the height limit inside the machine. Fourthly, since the cushioning material 18 is positioned and held at the cushioning position B below the pallet 1 at the time of landing, the pallet 1 is also protected from the drop impact at the time of landing. Fifthly, in addition to these, the conventional mount 2, such as the vehicle 2, the pallet 1, the parachute such as the main umbrella 4, etc. can be used as they are, and the predetermined cushioning material 18, holding material 19, wire 20, etc. can be pulled. It suffices to provide the means, the positioning means 21, etc., and is realized by a simple structure.

【0024】[0024]

【発明の効果】本発明に係る緩衝材の装着構造は、以上
説明したように、緩衝材を、端付近の準備位置とパレッ
ト下の緩衝位置とに変位可能とすると共に、緩衝材を機
内では保持材にて準備位置に保持し、空中でワイヤを備
えた引張手段にて変位せしめ、位置決め手段にて緩衝位
置に位置決めして、着地するようにしたことにより、次
の第1,第2,第3,第4,第5の効果を発揮する。
As described above, the shock-absorbing member mounting structure according to the present invention allows the shock-absorbing member to be displaced between the preparation position near the end and the shock-absorbing position under the pallet. By holding the material in the preparation position with the holding material, displacing it with the tension means equipped with the wire in the air, positioning it in the buffer position with the positioning means, and landing, the following first, second, and The third, fourth and fifth effects are exhibited.

【0025】第1に、着地後における車輌等の搭載物の
ジャッキアップ、緩衝材の抜き取り等の煩雑で面倒な作
業を要せず、着地後における搭載物のパレット上からの
取り外し,解脱作業が、簡単容易化される。第2に、そ
こで着地、降着後において、搭載物が迅速に使用,展開
できるようになる。例えば、着地,降着後において、搭
載物である車輌を直ちに発進でき、迅速な空挺行動が可
能となる。
First, it is possible to remove and dismount the loaded article from the pallet after landing without the need for complicated and troublesome work such as jacking up of the loaded article such as a vehicle after the landing and removing the cushioning material. Facilitated, easy. Secondly, the loaded object can be used and deployed quickly after landing and landing. For example, after landing and landing, the vehicle, which is the loaded object, can be immediately started, and swift airborne action can be performed.

【0026】第3に、航空機への搭載時において、機内
の制限高さに対し空間的なゆとりがあり、余裕を持って
機内作業を行うことができるようになる。第4に、着地
時におけるパレットの破損も防止される。第5に、しか
もこれらは簡単な構造により実現され、コスト面にも優
れている。このように、この種従来例に存した問題点が
一掃される等、本発明の発揮する効果は、顕著にて大な
るものがある。
Thirdly, when mounted on an aircraft, there is a spatial allowance with respect to the height limit inside the aircraft, and it becomes possible to perform work inside the aircraft with a margin. Fourth, damage to the pallet during landing is also prevented. Fifth, and moreover, these are realized by a simple structure and are excellent in cost. Thus, the effects of the present invention are remarkably great, such as the problems existing in this type of conventional example are eliminated.

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

【図1】本発明に係る緩衝材の装着構造の実施例を示す
側面概略図であり、(1)図は、抽出傘が開傘した段階
を、(2)図は、搭載物等が引き出された段階を、
(3)図は、抽出傘と主傘が分離された段階を、(4)
図は、主傘が開傘し搭載物等が吊り下げられた段階を示
す。
FIG. 1 is a schematic side view showing an embodiment of a cushioning material mounting structure according to the present invention. FIG. 1 (1) is a stage when an extraction umbrella is opened, and FIG. The stage
(3) The figure shows the stage when the extraction umbrella and the main umbrella are separated (4)
The figure shows the stage when the main umbrella is opened and the mounted objects are hung.

【図2】同実施例における航空機内の側面図である。FIG. 2 is a side view of the inside of the aircraft in the embodiment.

【図3】同実施例において、抽出傘が開傘した段階の側
面図である。
FIG. 3 is a side view of the stage in which the extraction umbrella is opened in the embodiment.

【図4】同実施例において、搭載物等が引き出される途
中の段階の側面図である。
FIG. 4 is a side view showing a stage in the middle of pulling out a mounted object in the embodiment.

【図5】同実施例の側面図であり、(1)図は、搭載物
等が引き出された段階を示し、(2)図は、抽出傘と主
傘が分離された段階を示す。
FIG. 5 is a side view of the embodiment, FIG. 1 (1) shows a stage in which a mounted object is pulled out, and FIG. 5 (2) shows a stage in which an extraction umbrella and a main umbrella are separated.

【図6】同実施例において、主傘が開傘し搭載物等が吊
り下げられた段階の側面図である。
FIG. 6 is a side view of the embodiment in which the main umbrella is opened and the mounted object is hung.

【図7】同実施例における緩衝材のシートパック構造を
示し、(1)図は側面説明図、(2)図は斜視説明図で
ある。
7A and 7B show a sheet pack structure of a cushioning material in the embodiment, FIG. 1A is a side view and FIG. 2B is a perspective view.

【図8】従来例に係る緩衝材の装着構造を示し、主傘が
開傘し搭載物等が吊り下げられた段階の側面図である。
FIG. 8 is a side view showing a cushioning material mounting structure according to a conventional example, in a stage in which a main umbrella is opened and a mounted object or the like is suspended.

【符号の説明】[Explanation of symbols]

1 パレット 2 車輌 3 搭載物 4 主傘(落下傘) 7 航空機 18 緩衝材 19 保持材 20 ワイヤ(引張手段) 21 位置決め手段 A 準備位置 B 緩衝位置 DESCRIPTION OF SYMBOLS 1 pallet 2 vehicle 3 loading object 4 main umbrella (parachute) 7 aircraft 18 cushioning material 19 holding material 20 wire (pulling means) 21 positioning means A preparation position B buffer position

Claims (1)

【特許請求の範囲】[Claims] 【請求項1】 落下傘付のパレット上に直接取り付けら
れた車輌等の搭載物を、航空機から空中に投下し、落下
途中の空中において該搭載物を該パレットを介し開傘し
た該落下傘の下に吊り下げて、着地させる際に用いら
れ、着地時の落下衝撃から該搭載物を防護する緩衝材の
装着構造であって、 該航空機内等では該搭載物の端付近の準備位置に保持さ
れ、又、落下途中の空中においては該パレットの底面側
の緩衝位置に保持され、着地時の落下衝撃にて潰れやす
い構造よりなる緩衝材と、 上記準備位置にある該緩衝材と該搭載物やパレットとの
間に介裝され、該緩衝材を上記準備位置に保持する保持
材と、 上記準備位置にある該緩衝材に対し該パレットの底面を
介し連結されたワイヤを備え、落下途中の空中におい
て、該ワイヤにて該緩衝材に引張力を加えることが可能
であり、該保持材による保持を解除すると共に、該緩衝
材を上記準備位置から緩衝位置へと廻り込ませて保持す
る引張手段と、 上記緩衝位置にある該緩衝材と該パレットとの間に介裝
され、該緩衝材を上記緩衝位置に安定的に位置決めする
位置決め手段と、を有してなることを特徴とする緩衝材
の装着構造。
1. A loaded article such as a vehicle directly mounted on a pallet with a parachute is dropped from an aircraft into the air, and the article is placed under the parachute opened through the pallet in the air during the fall. A structure for mounting a cushioning material that is used for suspending and landing and protecting the mounted object from a drop impact at the time of landing, and is held at a preparation position near the end of the mounted object in the aircraft or the like, In addition, in the midst of falling, the cushioning material having a structure that is held at the cushioning position on the bottom side of the pallet and is easily crushed by a drop impact at the time of landing, the cushioning material in the above-mentioned preparation position, the mounted object and the pallet. And a wire that is interposed between the buffer material and the buffer material at the preparation position and a wire that is connected to the buffer material at the preparation position via the bottom surface of the pallet. , The buffer with the wire It is possible to apply a tensile force to the material, release the holding by the holding material, and to hold the material by wrapping around the buffer material from the preparatory position to the buffer position and holding the member at the buffer position. A cushioning material mounting structure, comprising: a positioning means interposed between the cushioning material and the pallet and stably positioning the cushioning material at the cushioning position.
JP03947193A 1993-02-03 1993-02-03 Mounting structure of cushioning material Expired - Fee Related JP3190470B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP03947193A JP3190470B2 (en) 1993-02-03 1993-02-03 Mounting structure of cushioning material

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP03947193A JP3190470B2 (en) 1993-02-03 1993-02-03 Mounting structure of cushioning material

Publications (2)

Publication Number Publication Date
JPH06227496A true JPH06227496A (en) 1994-08-16
JP3190470B2 JP3190470B2 (en) 2001-07-23

Family

ID=12553986

Family Applications (1)

Application Number Title Priority Date Filing Date
JP03947193A Expired - Fee Related JP3190470B2 (en) 1993-02-03 1993-02-03 Mounting structure of cushioning material

Country Status (1)

Country Link
JP (1) JP3190470B2 (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2010221983A (en) * 2009-03-25 2010-10-07 Ihi Aerospace Co Ltd Method and apparatus for launching rocket
JP2014091414A (en) * 2012-11-02 2014-05-19 Ihi Aerospace Co Ltd Attitude stabilization device of air-launching system
JP2016527117A (en) * 2013-05-29 2016-09-08 ザ クック ファウンデーション Air drop system
JP2020190463A (en) * 2019-05-22 2020-11-26 東日本旅客鉄道株式会社 Inclination measuring instrument to be installed on slope, and method for installing measuring instrument on slope
CN114987771A (en) * 2022-08-05 2022-09-02 西安羚控电子科技有限公司 Unmanned aerial vehicle and carrier buffering separator

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2010221983A (en) * 2009-03-25 2010-10-07 Ihi Aerospace Co Ltd Method and apparatus for launching rocket
JP2014091414A (en) * 2012-11-02 2014-05-19 Ihi Aerospace Co Ltd Attitude stabilization device of air-launching system
JP2016527117A (en) * 2013-05-29 2016-09-08 ザ クック ファウンデーション Air drop system
JP2020190463A (en) * 2019-05-22 2020-11-26 東日本旅客鉄道株式会社 Inclination measuring instrument to be installed on slope, and method for installing measuring instrument on slope
CN114987771A (en) * 2022-08-05 2022-09-02 西安羚控电子科技有限公司 Unmanned aerial vehicle and carrier buffering separator
CN114987771B (en) * 2022-08-05 2022-11-01 西安羚控电子科技有限公司 Unmanned aerial vehicle and carrier buffering separator

Also Published As

Publication number Publication date
JP3190470B2 (en) 2001-07-23

Similar Documents

Publication Publication Date Title
US11273919B2 (en) Parachute architecture for low-altitude VTOL aircraft
US10717537B2 (en) Parachute tow and release system with canopy extraction controlled by drag surface
JPH0624483A (en) Expanding type container for aircraft transportation and its assembly method
CA1258057A (en) Methods of deploying parachutes
US11180261B2 (en) Attached rocket parachute deployment system
US3690604A (en) Parachute stowage and deployment
US20190112057A1 (en) Parachute deployment system using decoupled tow and release lines
CA2104581C (en) Lightweight sealed parachute and harness assembly
JPH06227496A (en) Installation structure for buffer member
US2702679A (en) Means for the deployment of parachutes at high speeds
US10053221B2 (en) Multi-staged suspension line length parachutes
CN107600433B (en) Parachute canopy protective sleeve by means of back-pull method and mounting method thereof
US6776374B2 (en) Parachute pack for powered parachute
US2749066A (en) Aid to packing, deployment, and initial inflation of parachutes
US3137465A (en) Load recovery parachute system
US2718369A (en) Pilot chute
US4445654A (en) Aircraft recovery chute
CN211711077U (en) Wheeled vehicle air-drop system without cargo bed
US10625870B1 (en) Secured lines for ballistic recovery system
US2439318A (en) Parachute pack
JP3005861B1 (en) Large airship recovery system and airship recovery method using the same
US2625404A (en) Apparatus for laying hose lines from moving vehicles
US2979294A (en) Parachute combination and ejection device
US3511458A (en) Aerial recovery system
US3429531A (en) Deployment bag and method of packing

Legal Events

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