JP2693177B2 - Aircraft work equipment - Google Patents

Aircraft work equipment

Info

Publication number
JP2693177B2
JP2693177B2 JP63128030A JP12803088A JP2693177B2 JP 2693177 B2 JP2693177 B2 JP 2693177B2 JP 63128030 A JP63128030 A JP 63128030A JP 12803088 A JP12803088 A JP 12803088A JP 2693177 B2 JP2693177 B2 JP 2693177B2
Authority
JP
Japan
Prior art keywords
workbench
tunnel
aircraft
air
aircraft body
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
JP63128030A
Other languages
Japanese (ja)
Other versions
JPH01297396A (en
Inventor
順二 森野
和司 小林
昭夫 山本
Original Assignee
株式会社大氣社
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Filing date
Publication date
Application filed by 株式会社大氣社 filed Critical 株式会社大氣社
Priority to JP63128030A priority Critical patent/JP2693177B2/en
Publication of JPH01297396A publication Critical patent/JPH01297396A/en
Application granted granted Critical
Publication of JP2693177B2 publication Critical patent/JP2693177B2/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B05SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
    • B05BSPRAYING APPARATUS; ATOMISING APPARATUS; NOZZLES
    • B05B13/00Machines or plants for applying liquids or other fluent materials to surfaces of objects or other work by spraying, not covered by groups B05B1/00 - B05B11/00
    • B05B13/005Machines or plants for applying liquids or other fluent materials to surfaces of objects or other work by spraying, not covered by groups B05B1/00 - B05B11/00 mounted on vehicles or designed to apply a liquid on a very large surface, e.g. on the road, on the surface of large containers
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B05SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
    • B05BSPRAYING APPARATUS; ATOMISING APPARATUS; NOZZLES
    • B05B14/00Arrangements for collecting, re-using or eliminating excess spraying material
    • B05B14/30Arrangements for collecting, re-using or eliminating excess spraying material comprising enclosures close to, or in contact with, the object to be sprayed and surrounding or confining the discharged spray or jet but not the object to be sprayed

Description

【発明の詳細な説明】 〔産業上の利用分野〕 本発明は、航空機ボディーの塗装作業等に用いる航空
機用作業設備に関し、詳しくは、航空機ボディーの長手
方向に延びる作業台を航空機ボディーの周面に沿って上
下複数断設置する航空機用作業設備に関する。
Description: BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to work equipment for aircraft used for painting work on an aircraft body, and more specifically, a workbench extending in the longitudinal direction of the aircraft body is provided on a peripheral surface of the aircraft body. The present invention relates to work equipment for aircraft that is installed in a plurality of vertical sections along a line.

〔従来の技術〕[Conventional technology]

従来は、第6図及び第7図に示すように、各作業台
(2)上の作業空間を開空間とし、そして、作業台
(2)を設置した建屋(1)内の各所に換気装置の給気
部(7a)及び排気部(7b)を分散配置していた。
Conventionally, as shown in FIG. 6 and FIG. 7, the work space on each workbench (2) is made into an open space, and the ventilation device is installed at each place in the building (1) in which the workbench (2) is installed. The air supply part (7a) and the exhaust part (7b) were distributed.

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

しかし、各作業台上の作業空間は、最も重要な換気対
象域であるにもかかわらず、上下の作業台、及び航空機
ボディーにより三方を囲まれていることから換気効率が
悪く、その点、各作業台上の作業環境を良好に保つ上で
改善の余地があった。
However, even though the work space on each workbench is the most important ventilation target area, ventilation efficiency is poor because it is surrounded on three sides by the workbench above and below and the aircraft body. There was room for improvement in maintaining a good work environment on the workbench.

又、建屋内の各所に分散配置した給気部からの換気空
気吹出し、及び、排気部からの排気をもって各作業台上
の作業空間を換気するには極めて大きな換気風量が必要
であり、そのために、換気装置に大型のものが必要とな
って設備コストが高く付くとともにランニングコストを
嵩むといった経済面での問題もあり、 更には、作業に伴い発生した塵埃(特に塗装作業にあ
っては塗料ミストや溶剤ガス)が建屋内の全体に広が
り、建屋内全体の作業環境の悪化を招くといった問題も
あった。
In addition, a very large ventilation air volume is required to ventilate the work space on each workbench by blowing out ventilation air from the air supply parts distributed throughout the building and exhausting air from the exhaust part. In addition, there is an economic problem that a large ventilation device is required, resulting in high equipment cost and running cost, and dust generated during work (especially paint mist in painting work). There is also a problem that the work environment of the entire building is deteriorated due to the fact that solvent and gas) spread throughout the building.

本発明の目的は合理的な改良により上述問題を解消す
る点にある。
An object of the present invention is to solve the above problems by making a reasonable improvement.

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

本発明による航空機用作業設備の特徴構成は、航空機
ボディーの長手方向に延びる作業台を航空機ボディーの
周面に沿って上下複数段設置する構成において、 前記作業台夫々の巾方向端部のうち航空機ボディーと
は反対側の端部どうしにわたる隔壁を、前記作業台の長
手方向にわたらせて張設し、 上下の前記作業台、航空機ボディー、及び、前記隔壁
で囲まれる作業用のトンネル状制限空間に対する給気口
と排気口とを、そのトンネル状制限空間の長手方向に振
り分け配置し、 前記給気口から前記トンネル状制限空間の内部へ換気
空気を流入させるとともに、前記排気口から前記トンネ
ル状制限空間の内部空気を排出する換気装置を設けてあ
ることにあり、その作用・効果は次の通りである。
The characteristic configuration of the work equipment for an aircraft according to the present invention is a configuration in which a workbench extending in a longitudinal direction of an aircraft body is installed in a plurality of upper and lower stages along a peripheral surface of the aircraft body. A partition wall extending between the opposite ends of the body is stretched in the longitudinal direction of the workbench, and the workbench above and below, the aircraft body, and a tunnel-shaped restricted space for work surrounded by the partition The air supply port and the exhaust port are distributed in the longitudinal direction of the tunnel-shaped restriction space, and ventilation air is introduced from the air supply port into the tunnel-shaped restriction space, and the tunnel-shaped restriction space is provided from the exhaust port. There is a ventilator that discharges the air inside the space, and its actions and effects are as follows.

〔作 用〕(Operation)

つまり、上述構成によれば、上下の作業台、航空機ボ
ディー、及び、隔壁で囲まれる作業用のトンネル状制限
空間(すなわち、作業台上の作業空間)は、外部に対し
遮断された状態で、給気口から排気口へかけてトンネル
状制限空間の内部をその長手方向(すなわち、作業台や
航空機ボディーの長手方向)に流通する換気空気により
集中的に換気される。
That is, according to the above-mentioned configuration, the upper and lower workbench, the aircraft body, and the tunnel-shaped restricted space for work surrounded by the partition wall (that is, the work space on the workbench) are isolated from the outside, Ventilation air that flows in the longitudinal direction of the tunnel-shaped restricted space from the air supply port to the exhaust port (that is, the longitudinal direction of the workbench or the aircraft body) is intensively ventilated.

〔発明の効果〕〔The invention's effect〕

その結果、従来、換気効率が悪かった作業台上の作業
空間を効率良く確実に換気できるようになり、各作業台
上の作業環境を従前に比して大巾に改善し得るに至っ
た。
As a result, it has become possible to efficiently and reliably ventilate the work space on the workbench, which has conventionally been poor in ventilation efficiency, and to greatly improve the work environment on each workbench as compared with the conventional work environment.

又、作業用制限空間を換気空気の内部流通により集中
的に換気するものであるから、少量の換気風量で効果的
な換気を行うことができ、換気風量の少量化により換気
装置を小型化し得て設備コスト及びランニングコストを
従前に比して低減し得る。
Moreover, since the restricted space for work is intensively ventilated by the internal circulation of ventilation air, effective ventilation can be performed with a small amount of ventilation air, and the ventilation device can be downsized by reducing the amount of ventilation air. The equipment cost and running cost can be reduced as compared with the past.

しかも、作業台上での作業に伴い発生する塵埃、又、
塗装作業に伴い発生する塗装ミストや溶剤ガスが建屋内
に広がることは隔壁により確実に阻止されるから、建屋
内の作業環境悪化も防止できる。
In addition, dust generated during work on the workbench,
The partition walls reliably prevent the spread of paint mist and solvent gas generated during the painting work inside the building, so that the working environment inside the building can be prevented from deteriorating.

尚、隔壁を透明材で形成すれば、採光が可能となると
共に、トンネル状作業用制限空間内での作業状況を外部
から監視できて、管理面、並びに、安全面で有効であ
る。
If the partition wall is made of a transparent material, it is possible to illuminate and it is possible to monitor the working condition in the tunnel-shaped restricted working space from the outside, which is effective in terms of management and safety.

又、隔壁を人為破断可能なシート材で形成すれば、ト
ンネル状作業用制限空間内で万一事故が発生した場合に
作業者はシート材の破断により迅速に外部へ退避でき、
安全面でより一層有効である。
In addition, if the partition wall is formed of a sheet material that can be artificially ruptured, in the unlikely event that an accident occurs in the restricted space for tunnel-like work, the operator can quickly escape to the outside by rupturing the sheet material,
It is even more effective in terms of safety.

〔実施例〕〔Example〕

次に実施例を説明する。 Next, an embodiment will be described.

第1図ないし第5図は航空機ボディーの塗装に用いる
作業設備を示し、建屋(1)内に収容した塗装対象航空
機の両側において、航空機ボディー(A)の長手方向に
延びる作業台(2)を航空機ボディー(A)の周面に沿
って上下複数段設置してある。
1 to 5 show work equipment used for painting an aircraft body, and a workbench (2) extending in the longitudinal direction of the aircraft body (A) is provided on both sides of the painting target aircraft housed in the building (1). A plurality of upper and lower stages are installed along the peripheral surface of the aircraft body (A).

航空機ボディー(A)の両側夫々の作業台(2)群は
天井クレーン(3)により航空機ボディー(A)から離
れた退避位置と航空機ボディー(A)に近接する使用位
置とにわたって移動操作されるものである。
The workbench (2) group on each side of the aircraft body (A) is moved and operated by an overhead crane (3) between a retracted position away from the aircraft body (A) and a use position close to the aircraft body (A). Is.

各作業台(2)の巾方向端縁のうち航空機ボディー
(A)側の端縁部(2a)は航空機ボディー(A)に対す
る遠近方向に摺動自在としており、この摺動調整により
各作業台(2)を航空機ボディー(A)の周面に対して
適切にセッティングする。
Of the widthwise edges of each workbench (2), the edge portion (2a) on the aircraft body (A) side is slidable in the perspective direction with respect to the aircraft body (A). (2) is properly set on the peripheral surface of the aircraft body (A).

又、各作業台群においては、上下夫々の作業台(2)
の巾方向端部のうち航空機ボディー(A)とは反対側の
端部どうしにわたる隔壁(4)を作業台(2)のほぼ全
長にわたって張設してあり、各作業台(2)上の塗装作
業空間を、上下の作業台(2)、航空機ボディー
(A)、及び、隔壁(4)に囲まれたトンネル状の制限
空間(5)としてある。
Further, in each workbench group, the workbench (2) for each of the upper and lower
A partition wall (4) extending across the widthwise ends of the workbench (A) from the side opposite to the aircraft body (A) is stretched over substantially the entire length of the workbench (2). The work space is a tunnel-shaped restricted space (5) surrounded by the upper and lower workbench (2), the aircraft body (A), and the partition wall (4).

図中(6)は最上段の作業台(2)について上述と同
様のトンネル状制限空間(5)を形成すための天井であ
る。
In the figure, (6) is a ceiling for forming the tunnel-shaped restricted space (5) similar to the above with respect to the uppermost workbench (2).

一方、塗装作業空間であるトンネル状制限空間(5)
の夫々を換気するための構成としては、各トンネル状制
限空間(5)の長手方向中央部に隔壁(4)の不存部を
一部設け、この隔壁不存部を各制限空間(5)の内部へ
換気空気を取り入れるための給気口(7A)にしてある。
On the other hand, the tunnel-shaped restricted space (5), which is the painting work space
As a configuration for ventilating each of the above, each of the tunnel-shaped restricted spaces (5) is provided with a part of an absent part of the partition wall (4) at the central part in the longitudinal direction, and the partition wall absent part is provided in each restricted space (5). It has an air supply port (7A) for taking in ventilation air inside the.

また、各トンネル状制限空間(5)の長手方向両端部
には排気口(7B)を設け、そして、トンネル状制限空間
(5)に対する換気装置として排気ファン(8)を、排
気風路(9)を介して上記の各排気口(7B)に接続して
ある。
Further, exhaust ports (7B) are provided at both longitudinal ends of each tunnel-shaped restricted space (5), and an exhaust fan (8) is provided as a ventilation device for the tunnel-shaped restricted space (5) and an exhaust air duct (9). ) Is connected to each of the above exhaust ports (7B).

つまり、上記の排気ファン(8)は、給気口(7A)か
ら各トンネル状制限空間(5)の内部へ換気空気を流入
させるとともに、排気口(7B)から各トンネル状制限空
間(5)の内部空気を排出する換気装置を構成するもの
であり、この排気ファン(8)により、トンネル状制限
空間(5)の夫々を、その長手方向で給気口(7A)から
排気口(7B)へ向け換気空気を内部流通させて集中的に
換気する。
That is, the exhaust fan (8) causes ventilation air to flow from the air supply port (7A) into each tunnel-shaped restricted space (5), and also through the exhaust port (7B) to each tunnel-shaped restricted space (5). This exhaust fan (8) is used to construct a ventilation device for exhausting the internal air of each of the tunnel-shaped restricted spaces (5) in the longitudinal direction from the air supply port (7A) to the exhaust port (7B). Ventilation air is internally circulated toward and is intensively ventilated.

排気風路(9)には、制限空間(5)からの排気空気
に含まれる塗料ミストのうち比較的粒径の大きいものを
捕捉するペーパーフィルター(10)、及び、細粒径のも
のを捕捉するための除塵ユニット(11)を介装してあ
り、除塵ユニット(11)は塗料ミスト捕捉用のプレフィ
ルター(11a)及び中性能バグフィルター(11b)と共に
前記の排気ファン(8)を内装する構成としてある。
In the exhaust air passage (9), a paper filter (10) that captures a relatively large particle size of the paint mist contained in the exhaust air from the restricted space (5) and a fine particle size The dust removal unit (11) for removing the dust is contained in the dust removal unit (11) together with the pre-filter (11a) for catching the paint mist and the medium performance bag filter (11b). It is as a configuration.

除塵ユニット(11)を通過した排気空気は、制限空間
(5)内での塗装に伴い発生した溶剤ガスとともに屋外
に廃棄される。
The exhaust air that has passed through the dust removal unit (11) is discarded outdoors together with the solvent gas generated by the coating in the restricted space (5).

尚、排気空気中に含まれる溶剤ガスを適宜後処理する
ようにしても良い。
The solvent gas contained in the exhaust air may be appropriately post-treated.

(12)は浄化空気をトンネル状制限空間(5)の給気
口(7A)に向けて吹出す給気ユニットであり、給気ファ
ン(12a)、プレフィルター(12b)、中性能フィルター
(12c)を内装するものである。
(12) is an air supply unit that blows the purified air toward the air supply port (7A) of the tunnel-shaped restricted space (5). The air supply fan (12a), the pre-filter (12b), and the medium-performance filter (12c). ) Is the interior.

つまり、吹出し浄化空気を換気空気として給気口(7
A)から制限空間(5)内へ取込ませることにより、塗
面に対する塵埃付着を防止して塗装品質を向上させるよ
うにしてある。
In other words, blown purified air is used as ventilation air for the air inlet (7
By taking it from A) into the restricted space (5), it is possible to prevent dust from adhering to the coated surface and improve the coating quality.

又、(13)は給気風路(14)を介して各制限空間
(5)の給気口(7A)付近に温調空気を供給する空調器
であり、夏場や冬場には、この温調空気供給によりトン
ネル状制限空間(5)を冷暖房する。
In addition, (13) is an air conditioner that supplies temperature-controlled air to the vicinity of the air supply port (7A) of each restricted space (5) via the air supply air passage (14). The air is supplied to heat and cool the tunnel-shaped restricted space (5).

(15)は塗料タンク、(16)は塗料供給ポンプであ
り、塗料は固定供給管(17)、及び、作業者の移動を許
す螺旋状伸縮ホース(18)を介して、各作業者が持つス
プレーガン(19)に供給される。又、(18′)は作業者
の移動を許すスプレー用圧縮空気供給ホースである。
(15) is a paint tank, (16) is a paint supply pump, and the paint is held by each worker through a fixed supply pipe (17) and a spiral telescopic hose (18) that allows the worker to move. Supplied to the spray gun (19). Further, (18 ') is a compressed air supply hose for spraying which allows the operator to move.

隔壁(4)は、不燃性、耐溶剤性を有するとともに帯
電性を有しない材質で、かつ、透明ないし半透明で、し
かも、人為破断が可能なシート材で形成してあり、隔壁
(4)を、透明ないし半透明とすることでトンネル状制
限空間(5)内を明るく保ち、又、人為的破断が可能な
シート材とすることで事故の際には隔壁(4)を破って
迅速に脱出できるようにしてある。
The partition wall (4) is made of a non-combustible, solvent-resistant and non-chargeable material, and is transparent or translucent, and is formed of a sheet material that can be artificially broken. Is transparent or semi-transparent to keep the tunnel-shaped restricted space (5) bright, and by using a sheet material that can be artificially ruptured, the partition wall (4) is ruptured quickly in the event of an accident. I am able to escape.

最下段の作業台(2)においては、航空機ボディー
(A)の周面における塗装不要部分のマスキング、並び
に、航空機ボディー(A)の周面と作業台(2)との間
のシーリングを兼ねるシート部材(20)を作業台(2)
の全長にわたって貼設してある。
In the workbench (2) at the lowermost stage, a sheet that also serves as a mask for the unpainted portion on the peripheral surface of the aircraft body (A) and as a sealing between the peripheral surface of the aircraft body (A) and the workbench (2). Workbench (2) with member (20)
Is affixed over the entire length of.

図中(21)は航空機ボディー(A)のうち垂直尾翼を
塗装するために上下複数段に設置した作業台群であり、
この作業台群においても隔壁(22)を設けて前述とほぼ
同形式の制限空間内換気を実施するようにしてある。
In the figure, (21) is a workbench group installed in a plurality of upper and lower stages for painting the vertical tail of the aircraft body (A),
Also in this workbench group, a partition wall (22) is provided to perform ventilation in the restricted space of substantially the same type as described above.

又、(23)は航空機ボディー(A)の下部周面に対す
る階段状の塗装作業台である。
Further, (23) is a stair-shaped painting workbench on the lower peripheral surface of the aircraft body (A).

〔別実施例〕(Another embodiment)

次に別実施例を説明する。 Next, another embodiment will be described.

トンネル状制限空間(5)の長手方向において給気口
(7A)と排気口(7B)とをどのように振り分け配置する
かは種々の構成変更が可能であり、例えば、トンネル状
制限空間(5)の長手方向中央部に排気口(7B)を配置
し、かつ、長手方向両端部に給気口(7A)を配置しても
よく、また、トンネル状制限空間(5)の長手方向一端
部に排気口(7B)を配置し、かつ、長手方向他端部に給
気口(7A)を配置してもよい。
Various arrangement changes can be made as to how to arrange the air supply port (7A) and the exhaust port (7B) in the longitudinal direction of the tunnel-shaped restricted space (5), for example, the tunnel-shaped restricted space (5). ), The exhaust port (7B) may be arranged at the center in the longitudinal direction, and the air supply ports (7A) may be arranged at both ends in the longitudinal direction, and one end in the longitudinal direction of the tunnel-shaped restricted space (5). The exhaust port (7B) may be arranged at the same time, and the air supply port (7A) may be arranged at the other end in the longitudinal direction.

給気口(7A)からの換気空気の流入と排気口(7B)か
らの内部空気排出とによるトンネル状制限空間(5)の
換気形態、及び、この流入と排出を行う換気装置の形態
としては、排気口(7B)からの強制排気と給気口(7A)
からの自然給気とによりトンネル状制限空間(5)を換
気するものとしてもよく、また、排気口(7B)からの強
制排気と給気口(7A)からの強制給気とによりトンネル
状制限空間(5)を換気するものとしてもよく、さらに
また、給気口(7A)からの強制給気と排気口(7B)から
の自然排気とによりトンネル状制限空間(5)を換気す
るものとしてもよい。
The ventilation form of the tunnel-shaped restricted space (5) by the inflow of ventilation air from the air supply port (7A) and the exhaust of internal air from the exhaust port (7B), and the form of the ventilation device that performs this inflow and outflow are , Forced exhaust from the exhaust port (7B) and air supply port (7A)
The tunnel-shaped restriction space (5) may be ventilated by natural air supply from the, and tunnel-shaped restriction by forced exhaust from the exhaust port (7B) and forced air supply from the air supply port (7A). The space (5) may be ventilated, and furthermore, the tunnel-shaped restricted space (5) is ventilated by forced air supply from the air supply port (7A) and natural exhaust from the air exhaust port (7B). Good.

隔壁(4)はシート材であっても良く、又、板材であ
っても良く、材質も種々のものを適用できる。
The partition wall (4) may be a sheet material or a plate material, and various materials can be applied.

本発明による航空機用作業設備は塗装作業用に限定さ
れるものではなく、航空機ボディーに対する種々の作業
に適用できる。
The aircraft work equipment according to the present invention is not limited to painting work, but can be applied to various works on an aircraft body.

尚、特許請求の範囲の項に図面との対照を便利にする
為に符号を記すが、該記入により本発明は添付図面の構
造に限定されるものではない。
In the claims, reference numerals are provided for convenience of comparison with the drawings, but the present invention is not limited to the structure shown in the attached drawings.

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

第1図ないし第5図は本発明の実施例を示し、第1図は
全体構成を示す概略斜視図、第2図は、断面図、第3図
は拡大断面図、第4図は平面視拡大断面図、第5図は側
面視拡大断面図である。第6図及び第7図は従来例を示
す平面図と正面、図である。 (2)……作業台、(4)……隔壁、(5)……制限空
間、(7A)……給気口、(7B)……排気口、(8)……
換気装置、(A)……航空機ボディー。
1 to 5 show an embodiment of the present invention, FIG. 1 is a schematic perspective view showing the entire structure, FIG. 2 is a sectional view, FIG. 3 is an enlarged sectional view, and FIG. 4 is a plan view. An enlarged sectional view and FIG. 5 are enlarged side sectional views. 6 and 7 are a plan view, a front view, and a view showing a conventional example. (2) ... Workbench, (4) ... Partition, (5) ... Restricted space, (7A) ... Air inlet, (7B) ... Exhaust, (8) ...
Ventilator, (A) ... Aircraft body.

Claims (3)

(57)【特許請求の範囲】(57) [Claims] 【請求項1】航空機ボディー(A)の長手方向に延びる
作業台(2)を航空機ボディー(A)の周面に沿って上
下複数段設置する航空機用作業設備であって、 前記作業台(2)夫々の巾方向端部のうち航空機ボディ
ー(A)とは反対側の端部どうしにわたる隔壁(4)
を、前記作業台(2)の長手方向にわたらせて張設し、 上下の前記作業台(2)、航空機ボディー(A)、及
び、前記隔壁(4)で囲まれる作業用のトンネル状制限
空間(5)に対する給気口(7A)と排気口(7B)とを、
そのトンネル状制限空間(5)の長手方向に振り分け配
置し、 前記給気口(7A)から前記トンネル状制限空間(5)の
内部へ換気空気を流入させるとともに、前記排気口(7
B)から前記トンネル状制限空間(5)の内部空気を排
出する換気装置(8)を設けてある航空機用作業設備。
1. A work equipment for an aircraft, wherein workbench (2) extending in a longitudinal direction of an aircraft body (A) is installed in a plurality of upper and lower stages along a peripheral surface of the aircraft body (A), said workbench (2). ) A partition wall (4) extending between the ends of the respective widthwise ends opposite to the aircraft body (A).
Is stretched over the longitudinal direction of the workbench (2) and is surrounded by the workbench (2) above and below, the aircraft body (A), and the partition wall (4), and is a tunnel-shaped restricted space for work. The air supply port (7A) and exhaust port (7B) for (5)
The tunnel-shaped restricted space (5) is arranged in the longitudinal direction so that ventilation air flows from the air supply port (7A) into the tunnel-shaped restricted space (5) and the exhaust port (7).
Aircraft work equipment provided with a ventilation device (8) for discharging the internal air of the tunnel-shaped restricted space (5) from B).
【請求項2】前記隔壁(4)が透明材から成る請求項1
記載の航空機用作業設備。
2. The partition (4) is made of a transparent material.
Aircraft work equipment as described.
【請求項3】前記隔壁(4)が人為破断可能なシート材
から成る請求項1又は2記載の航空機用作業設備。
3. The aircraft work facility according to claim 1, wherein the partition wall (4) is made of a sheet material that can be artificially ruptured.
JP63128030A 1988-05-25 1988-05-25 Aircraft work equipment Expired - Fee Related JP2693177B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP63128030A JP2693177B2 (en) 1988-05-25 1988-05-25 Aircraft work equipment

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP63128030A JP2693177B2 (en) 1988-05-25 1988-05-25 Aircraft work equipment

Publications (2)

Publication Number Publication Date
JPH01297396A JPH01297396A (en) 1989-11-30
JP2693177B2 true JP2693177B2 (en) 1997-12-24

Family

ID=14974769

Family Applications (1)

Application Number Title Priority Date Filing Date
JP63128030A Expired - Fee Related JP2693177B2 (en) 1988-05-25 1988-05-25 Aircraft work equipment

Country Status (1)

Country Link
JP (1) JP2693177B2 (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7922272B2 (en) * 2008-04-11 2011-04-12 The Boeing Company Method for application and accurate positioning of graphics on a surface
LU92367B1 (en) * 2014-01-29 2015-07-30 Cti Systems S A Device suspended from the top of a vertical stabilizer of an aerial vehicle

Also Published As

Publication number Publication date
JPH01297396A (en) 1989-11-30

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