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JP3484537B2 - Airship aggregate assembly method - Google Patents
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JP3484537B2 - Airship aggregate assembly method - Google Patents

Airship aggregate assembly method

Info

Publication number
JP3484537B2
JP3484537B2 JP2000133545A JP2000133545A JP3484537B2 JP 3484537 B2 JP3484537 B2 JP 3484537B2 JP 2000133545 A JP2000133545 A JP 2000133545A JP 2000133545 A JP2000133545 A JP 2000133545A JP 3484537 B2 JP3484537 B2 JP 3484537B2
Authority
JP
Japan
Prior art keywords
ring
aggregate
airship
shaped
aggregates
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
JP2000133545A
Other languages
Japanese (ja)
Other versions
JP2001315694A (en
Inventor
克治 海法
一樹 小林
潤一 杉本
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.)
Kawasaki Motors Ltd
Original Assignee
Kawasaki Jukogyo KK
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 Kawasaki Jukogyo KK filed Critical Kawasaki Jukogyo KK
Priority to JP2000133545A priority Critical patent/JP3484537B2/en
Publication of JP2001315694A publication Critical patent/JP2001315694A/en
Application granted granted Critical
Publication of JP3484537B2 publication Critical patent/JP3484537B2/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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Description

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

【0001】[0001]

【発明の属する技術分野】 本発明は、硬式の飛行船の
軟質の表面膜材を内側から支えて保形する骨材の組立に
関し、特に飛行船の防錐形となる機首部分,機尾部分の
骨材の組立に係る技術分野に属する。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to an assembly of an aggregate for supporting a soft surface film material of a rigid airship from the inside to retain the shape, and particularly to a nose portion and a stern portion of the airship that have a cone shape. It belongs to the technical field of assembling aggregates.

【0002】[0002]

【従来の技術】 一般に、硬式の飛行船の機首部分,機
尾部分では、飛行船の長さ方向と直交して周方向へ延び
るリング形骨材と、リング形骨材に直交し飛行船の長さ
方向へ湾曲して延びる湾曲骨材とを連結する骨材組立構
造が採用されている。
2. Description of the Related Art Generally, in the nose and aft of a rigid airship, a ring-shaped aggregate extending in the circumferential direction at right angles to the length of the airship and a length of the airship orthogonal to the ring-shaped aggregate. An aggregate assembly structure is used that connects curved aggregates extending in a direction.

【0003】従来、飛行船の骨材組立方法としては、例
えば、組立現場に骨材の全体を下支え,側支えする足場
(総足場)を構築して、リング形骨材,湾曲骨材等を連
結することが行われている。
Conventionally, as a method of assembling aggregates of an airship, for example, a scaffold (total scaffolding) that supports and side-supports the entire aggregate at an assembly site is constructed, and ring-shaped aggregates, curved aggregates, etc. are connected. Is being done.

【0004】[0004]

【発明が解決しようとする課題】 前述の従来の飛行船
の骨材組立方法では、飛行船が大型化すると、防錐形の
機首部分,機尾部分の足場が大規模化,複雑化してしま
うという問題点がある。
According to the above-described conventional method for assembling aggregates of an airship, when the airship becomes large, the scaffolding of the anti-cone type nose and stern becomes large and complicated. There is a problem.

【0005】特に、成層圏まで飛行する大型の無人の飛
行船では、骨材としてCFRP等の軽量材が使用され、
自重等で捻れ,歪みが生じやすいため、足場を大規模
化,複雑化させても精密な組立が不能になるという問題
点がある。
In particular, in large unmanned airships that fly to the stratosphere, lightweight materials such as CFRP are used as aggregates,
There is a problem in that precise assembly becomes impossible even if the scaffold is enlarged or complicated because it tends to be twisted or distorted due to its own weight or the like.

【0006】本発明は、このような問題点を考慮してな
されたもので、足場を大規模化,複雑化させることなく
精密な組立が可能な飛行船の骨材組立方法を提供するこ
とを課題とする。
The present invention has been made in view of the above problems, and an object thereof is to provide a method for assembling aggregates of an airship that can be precisely assembled without increasing the size and complexity of the scaffold. And

【0007】[0007]

【課題を解決するための手段】 前述の課題を解決する
ため、本発明に係る飛行船の骨材組立方法は、次のよう
な手段を採用する。
Means for Solving the Problems In order to solve the above-mentioned problems, an airship aggregate assembly method according to the present invention employs the following means.

【0008】即ち、請求項1では、飛行船の長さ方向と
直交して周方向へ延びるリング形骨材と、リング形骨材
に直交し飛行船の長さ方向へ湾曲して延びる湾曲骨材と
を連結する飛行船の骨材組立方法において、飛行船の長
さ方向に延びる軸中心線に対応する芯材を垂直に配設
し、芯材を中心としてリング形骨材を水平面で組付け、
芯材とリング形骨材との間に放射状に支持部材を掛渡し
た後、リング形骨材に湾曲骨材を連結することを特徴と
する。
That is, in claim 1, a ring-shaped aggregate extending in the circumferential direction orthogonal to the length of the airship, and a curved aggregate orthogonal to the ring-shaped aggregate and extending in the lengthwise direction of the airship. In the method of assembling an aggregate of an airship for connecting, a core material corresponding to an axial centerline extending in the length direction of the airship is arranged vertically, and a ring-shaped aggregate is assembled around the core material in a horizontal plane,
The present invention is characterized in that the support member is radially extended between the core member and the ring-shaped aggregate, and then the curved aggregate is connected to the ring-shaped aggregate.

【0009】この手段では、リング形骨材が水平面で組
付けられるため、リング形骨材の組付けの際の捻れ,歪
みが防止される。組付けられたリング形骨材は、芯材,
支持部材によって保形され、その後の捻れ,歪みも防止
される。
According to this means, since the ring-shaped aggregate is assembled on a horizontal plane, twisting and distortion at the time of assembling the ring-shaped aggregate can be prevented. The assembled ring-shaped aggregate is
The shape is retained by the support member, and subsequent twisting and distortion are prevented.

【0010】また、請求項2では、請求項1の飛行船の
骨材組立方法において、組付けられたリング形骨材を芯
材に沿って順次上昇させ、芯材の上方から下方へ向けて
間隔を介して順次径の大きくなるリング形骨材を積層す
ることを特徴とする。
According to a second aspect of the present invention, in the method for assembling aggregates for an airship according to the first aspect, the assembled ring-shaped aggregates are sequentially raised along the core material and are spaced from above the core material toward the lower side. It is characterized in that ring-shaped aggregates whose diameters are successively increased are laminated through.

【0011】この手段では、芯材を中心としてリング形
骨材,湾曲骨材により下向へ向けて広がる紡錘形が形成
される。
According to this means, a spindle-shaped body spreading downward is formed by the ring-shaped aggregate and the curved aggregate with the core as the center.

【0012】[0012]

【発明の実施の形態】 以下、本発明に係る飛行船の骨
材組立方法の実施の形態を図面に基づいて説明する。
BEST MODE FOR CARRYING OUT THE INVENTION Embodiments of an aggregate assembly method for an airship according to the present invention will be described below with reference to the drawings.

【0013】図1〜図4は、本発明に係る飛行船の骨材
組立方法の実施の形態(1)を示すものである。
1 to 4 show an embodiment (1) of an airship aggregate assembly method according to the present invention.

【0014】この実施の形態は、図1(A)に示すよう
に、飛行船の長さ方向に延びる軸中心線に対応するパイ
プ形の芯材1を垂直に配設し、芯材1を中心として最も
機首側,機尾側に位置するリング形骨材2を水平面で組
付けている。従って、リング形骨材2の組付けの際の捻
れ,歪みが防止される。
In this embodiment, as shown in FIG. 1 (A), a pipe-shaped core 1 corresponding to an axial center line extending in the lengthwise direction of an airship is vertically arranged, and the core 1 is centered. The ring-shaped aggregate 2 located on the nose side and the tail side is assembled in a horizontal plane. Therefore, twisting and distortion at the time of assembling the ring-shaped aggregate 2 are prevented.

【0015】そして、芯材1とリング形骨材2との間に
放射状にテグス,ワイヤ等からなる支持部材3をテンシ
ョンを掛けて掛渡している。従って、組付けられたリン
グ形骨材2は、芯材1,支持部材3によって保形され、
その後の捻れ,歪みも防止されることになる。
Then, a support member 3 made of tex, wire or the like is radially applied between the core 1 and the ring-shaped aggregate 2 by tension. Therefore, the assembled ring-shaped aggregate 2 is shaped by the core material 1 and the support member 3,
Later twisting and distortion will also be prevented.

【0016】この後、図1(B)に示すように、リング
形骨材2に対して、リング形骨材2よりも機首側,機尾
側に位置する湾曲骨材4が連結される。なお、リング形
骨材2同士やリング形骨材2,湾曲骨材4は、後述のよ
うな連結具5を使用して組付け,連結される(図5参
照)。連結されたリング形骨材2,湾曲骨材4の連結
は、芯材1,支持部材3の介在もあってかなり強固な剛
体となる。
Thereafter, as shown in FIG. 1 (B), the curved aggregates 4 located on the nose side and the aft side of the ring-shaped aggregate 2 are connected to the ring-shaped aggregate 2. . The ring-shaped aggregates 2 or the ring-shaped aggregates 2 and the curved aggregates 4 are assembled and connected using a connecting tool 5 as described later (see FIG. 5). The connected ring-shaped aggregate 2 and curved aggregate 4 are connected to each other by the core 1 and the support member 3 to form a rigid body.

【0017】続いて、図1(C)に示すように、芯材1
に第2の芯材1’が挿入され、先の芯材1が上方へスラ
イド上昇され一定の高さで固定される。このスライド上
昇には、クレーン等が使用される。
Subsequently, as shown in FIG. 1C, the core material 1
The second core material 1'is inserted into the above, and the above core material 1 is slid upward and fixed at a constant height. A crane or the like is used to raise the slide.

【0018】そして、第2の芯材1’を中心として機首
側,機尾側から2番目に位置するリング形骨材2’が水
平面で組付けられ、第2の芯材1’とリング形骨材2’
との間に放射状にテグス,ワイヤ等からなる支持部材
3’がテンションを掛けて掛渡され、両リング形骨材
2,2’に対して、両リング形骨材2,2’の間に位置
する湾曲骨材4’が連結される(図1(D)参照)。
Then, the ring-shaped aggregate 2'positioned second from the nose side and the aft side around the second core 1'is assembled in a horizontal plane, and the second core 1'and the ring are assembled. Shaped aggregate 2 '
A support member 3'comprising tex, wire, etc. is radially applied between and with respect to both ring-shaped aggregates 2, 2 ', and between both ring-shaped aggregates 2, 2'. The positioned curved aggregate 4'is connected (see FIG. 1D).

【0019】また、図2に示すように、剛性を高めるた
めに、両リング形骨材2,2’の間にも支持部材3,
3’が掛渡される。なお、リング形骨材2,2’を3段
以上に構成することも可能である。
Further, as shown in FIG. 2, in order to increase the rigidity, the supporting members 3, 3 are also provided between the ring-shaped aggregates 2, 2 '.
3'is handed over. It is also possible to configure the ring-shaped aggregates 2 and 2'in three or more stages.

【0020】この後、図3に示すように、組立てられた
紡錘形の機首部分A,機尾部分Bが横向きにされクレー
ン等で吊持ちされて、足場Dに搭載される。この足場D
には、機首部分A,機尾部分Bを繋ぐキール部Cが予め
搭載されている。なお、図3から明らかなように、この
実施の形態は半硬式である。
After that, as shown in FIG. 3, the assembled spindle-shaped nose portion A and tail portion B are laid sideways and hung by a crane or the like, and mounted on a scaffold D. This scaffold D
A keel portion C that connects the nose portion A and the tail portion B is mounted in advance on the vehicle. As is clear from FIG. 3, this embodiment is a semi-rigid type.

【0021】足場Dに搭載された機首部分A,機尾部分
B,キール部Cは、図4に示すように、補強材Eで強固
に繋ぎ連結される。
As shown in FIG. 4, the nose portion A, the aft portion B and the keel portion C mounted on the scaffold D are firmly connected and connected by a reinforcing material E, as shown in FIG.

【0022】この実施の形態によると、リング形骨材2
等に捻れ,歪みが生じないため、足場を大規模化,複雑
化させることなく、飛行船の紡錘形の機首部分A,機尾
部分Bの骨材を精密にしかも連続的な組立作業で組立て
ることができる。
According to this embodiment, the ring-shaped aggregate 2
Since there is no twist or distortion in the etc., the aggregates of the spindle-shaped nose A and tail B of the airship can be assembled accurately and continuously without increasing the size and complexity of the scaffold. You can

【0023】図5〜図8は、本発明に係る飛行船の骨材
組立方法の実施の形態(2)を示すものである。
5 to 8 show an embodiment (2) of the method for assembling aggregates for an airship according to the present invention.

【0024】この実施の形態では、図5に示すように、
支持部材3がリング形骨材2同士やリング形骨材2,湾
曲骨材4を組付け,連結する差込式の連結具5と芯材1
にスライド可能に嵌合されたリング6との間に掛渡され
ている。また、芯材1にスライド可能に嵌合された別の
リング6’と連結具5との間には、吊持形の支持部材
3”が掛渡されている。
In this embodiment, as shown in FIG.
The support member 3 assembles and connects the ring-shaped aggregates 2 or the ring-shaped aggregates 2 and the curved aggregates 4 with each other, and is a plug-in type connecting tool 5 and the core 1.
It is hung between the ring 6 and the ring 6 which is slidably fitted in. In addition, a suspension type support member 3 ″ is hung between another connecting member 5 and another ring 6 ′ which is slidably fitted to the core material 1.

【0025】そして、芯材1は、1本構成で比較的高さ
が長く設定されている。また、芯材1の周囲には、組立
足場7を構築してある。
The core material 1 has a single structure and a relatively high height. Further, an assembly scaffold 7 is built around the core material 1.

【0026】この実施の形態によると、図6に示すよう
に、リング6,6’を芯材1に沿って上昇させて、組付
けられたリング形骨材2を直ちに高い位置に設置するこ
とができる。このため、図7,図8に示すように、上段
のリング形骨材2,湾曲骨材4の連結作業と、下段のリ
ング形骨材2の組付作業やリング形骨材2’,湾曲骨材
4’の連結作業を同時進行させることができ、作業効率
が高くなる。
According to this embodiment, as shown in FIG. 6, the rings 6 and 6'are raised along the core 1 to immediately set the assembled ring-shaped aggregate 2 at a high position. You can Therefore, as shown in FIGS. 7 and 8, the work of connecting the upper ring-shaped aggregate 2 and the curved aggregate 4 and the work of assembling the lower ring-shaped aggregate 2 and the ring-shaped aggregate 2 ′, the curve The work of connecting the aggregates 4'can be simultaneously advanced, and the work efficiency is improved.

【0027】図9は、本発明に係る飛行船の骨材組立方
法の実施の形態(3)を示すものである。
FIG. 9 shows an embodiment (3) of the aggregate assembly method for an airship according to the present invention.

【0028】この実施の形態では、別の組立場所で組立
て吊持ちしたリング形骨材2,湾曲骨材4の芯材1を別
の第2の芯材1’の上端に継足すようにしている。
In this embodiment, the ring-shaped aggregate 2 and the core 1 of the curved aggregate 4 assembled and suspended at another assembly place are added to the upper end of another second core 1 '. There is.

【0029】この実施の形態によると、別の組立場所で
リング形骨材2,湾曲骨材4を組立てている際に、少な
くとも第2の芯材1’を中心としてリング形骨材2’を
組付け支持部材3’を掛渡す作業を行うことができ、作
業効率が高くなる。
According to this embodiment, when the ring-shaped aggregate 2 and the curved aggregate 4 are assembled at another assembly place, the ring-shaped aggregate 2'is centered around at least the second core 1 '. It is possible to carry out the work of hanging the assembly support member 3 ', and the work efficiency is improved.

【0030】以上、図示した実施の形態の外に、湾曲骨
材4,4’を3本以上のリング形骨材2,2’に連結す
ることも可能である。
As described above, in addition to the illustrated embodiment, the curved aggregates 4 and 4'can be connected to three or more ring-shaped aggregates 2 and 2 '.

【0031】[0031]

【発明の効果】 以上のように、本発明に係る飛行船の
骨材組立方法は、リング形骨材が水平面で組付けられ芯
材,支持部材によって保形されるため、リング形骨材等
に捻れ,歪みが生じないため、足場を大規模化,複雑化
させることなく精密な組立が可能になる効果がある。
As described above, in the method for assembling aggregates for an airship according to the present invention, since the ring-shaped aggregates are assembled in a horizontal plane and are retained by the core material and the supporting member, the ring-shaped aggregates are Since there is no twist or distortion, there is an effect that precise assembly can be performed without increasing the size or complexity of the scaffold.

【0032】さらに、請求項2として、芯材を中心とし
てリング形骨材,湾曲骨材により下向へ向けて広がる紡
錘形が形成されるため、連続的な組立に有効である効果
がある。
Further, according to a second aspect, since the spindle shape which spreads downward is formed by the ring-shaped aggregate and the curved aggregate centering on the core material, there is an effect that it is effective for continuous assembly.

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

【図1】 本発明に係る飛行船の骨材組立方法の実施の
形態(1)を示す工程斜視図であり、(A)〜(D)の
順に工程順が示されている。
FIG. 1 is a process perspective view showing an embodiment (1) of an airship aggregate assembly method according to the present invention, in which the process order is shown in the order of (A) to (D).

【図2】 図1(D)の拡大断面図である。FIG. 2 is an enlarged cross-sectional view of FIG.

【図3】 図1に続く工程の側面図である。FIG. 3 is a side view of a process following FIG.

【図4】 図3に続く工程の側面図である。FIG. 4 is a side view of a step following FIG.

【図5】 本発明に係る飛行船の骨材組立方法の実施の
形態(2)を示す要部の斜視図である。
FIG. 5 is a perspective view of a main part showing an embodiment (2) of an aggregate assembly method for an airship according to the present invention.

【図6】 図5の動作を示す側面図である。FIG. 6 is a side view showing the operation of FIG.

【図7】 図6に続く工程の側面図である。FIG. 7 is a side view of the step following FIG.

【図8】 図7に続く工程の側面図である。FIG. 8 is a side view of a step following FIG.

【図9】 本発明に係る飛行船の骨材組立方法の実施の
形態(3)を示す側面図である。
FIG. 9 is a side view showing an embodiment (3) of an aggregate assembly method for an airship according to the present invention.

【符号の説明】[Explanation of symbols]

1,1’ 芯材 2,2’ リング形骨材 3,3’,3” 支持部材 4,4’ 湾曲骨材 1,1 'core material 2,2 'ring-shaped aggregate 3,3 ', 3 "support member 4,4 'curved aggregate

───────────────────────────────────────────────────── フロントページの続き (56)参考文献 特開 平8−284255(JP,A) 特開 平7−253196(JP,A) 特開 平6−171596(JP,A) 実開 平4−116555(JP,U) 特許66015(JP,C2) (58)調査した分野(Int.Cl.7,DB名) B64B 1/08 B64F 5/00 ─────────────────────────────────────────────────── ─── Continuation of the front page (56) References JP-A-8-284255 (JP, A) JP-A-7-253196 (JP, A) JP-A-6-171596 (JP, A) Actual Kaihei 4- 116555 (JP, U) Patent 66015 (JP, C2) (58) Fields investigated (Int.Cl. 7 , DB name) B64B 1/08 B64F 5/00

Claims (2)

(57)【特許請求の範囲】(57) [Claims] 【請求項1】 飛行船の長さ方向と直交して周方向へ延
びるリング形骨材と、リング形骨材に直交し飛行船の長
さ方向へ湾曲して延びる湾曲骨材とを連結する飛行船の
骨材組立方法において、飛行船の長さ方向に延びる軸中
心線に対応する芯材を垂直に配設し、芯材を中心として
リング形骨材を水平面で組付け、芯材とリング形骨材と
の間に放射状に支持部材を掛渡した後、リング形骨材に
湾曲骨材を連結することを特徴とする飛行船の骨材組立
方法。
1. An airship that connects a ring-shaped aggregate that extends in the circumferential direction at right angles to the length of the airship and a curved aggregate that extends orthogonally to the ring-shaped aggregate and extends in the lengthwise direction of the airship. In the aggregate assembly method, a core material corresponding to an axial centerline extending in the length direction of the airship is vertically arranged, and the ring-shaped aggregate is assembled in a horizontal plane with the core material as a center. A method for assembling aggregates for an airship, characterized in that a curved aggregate is connected to the ring-shaped aggregate after radially arranging a support member between the aggregates.
【請求項2】 請求項1の飛行船の骨材組立方法におい
て、組付けられたリング形骨材を芯材に沿って順次上昇
させ、芯材の上方から下方へ向けて間隔を介して順次径
の大きくなるリング形骨材を積層することを特徴とする
飛行船の骨材組立方法。
2. The method of assembling aggregates for an airship according to claim 1, wherein the assembled ring-shaped aggregates are successively raised along the core material, and the diameters are sequentially increased from the upper part of the core material to the lower part thereof at intervals. A method for assembling aggregates for an airship, comprising stacking ring-shaped aggregates having a large size.
JP2000133545A 2000-05-02 2000-05-02 Airship aggregate assembly method Expired - Fee Related JP3484537B2 (en)

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JP3484537B2 true JP3484537B2 (en) 2004-01-06

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2021068457A1 (en) * 2019-10-10 2021-04-15 上海交通大学 Stratospheric airship of large-scale rigid and flexible integrated structure

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP3780336B2 (en) * 2001-12-07 2006-05-31 独立行政法人 宇宙航空研究開発機構 Pressure balloon
FR3098786B1 (en) * 2019-07-19 2021-08-06 Flying Whales "Method and system for manufacturing a rigid structure balloon, and heavy load carrying balloon thus manufactured"

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2021068457A1 (en) * 2019-10-10 2021-04-15 上海交通大学 Stratospheric airship of large-scale rigid and flexible integrated structure

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