JPH0447040Y2 - - Google Patents

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Publication number
JPH0447040Y2
JPH0447040Y2 JP1988158745U JP15874588U JPH0447040Y2 JP H0447040 Y2 JPH0447040 Y2 JP H0447040Y2 JP 1988158745 U JP1988158745 U JP 1988158745U JP 15874588 U JP15874588 U JP 15874588U JP H0447040 Y2 JPH0447040 Y2 JP H0447040Y2
Authority
JP
Japan
Prior art keywords
refueling
aircraft
vehicle
wing body
light
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
Application number
JP1988158745U
Other languages
Japanese (ja)
Other versions
JPH0278498U (en
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 filed Critical
Priority to JP1988158745U priority Critical patent/JPH0447040Y2/ja
Publication of JPH0278498U publication Critical patent/JPH0278498U/ja
Application granted granted Critical
Publication of JPH0447040Y2 publication Critical patent/JPH0447040Y2/ja
Expired legal-status Critical Current

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  • Vehicle Cleaning, Maintenance, Repair, Refitting, And Outriggers (AREA)
  • Indicating And Signalling Devices For Elevators (AREA)

Description

【考案の詳細な説明】 〔産業上の利用分野〕 本考案は、空港ターミナルにおける航空機の給
油を行う為の航空機給油用車両に関するものであ
る。
[Detailed Description of the Invention] [Industrial Application Field] The present invention relates to an aircraft refueling vehicle for refueling aircraft at an airport terminal.

〔従来の技術〕 大規模な空港の多くは、航空機が駐機されるス
ポツトの地上に、ハイドラントピツトと呼ばれる
給油口を有しており、ここから航空機用燃料が供
給されるものである。
[Prior Art] Many large-scale airports have fueling ports called hydrant pits on the ground at spots where aircraft are parked, from which aircraft fuel is supplied.

この航空機の給油には、翼体下面に設けられて
いる給油口に給油用ホースを取り付ける必要があ
り、地上から数メートルの高さにある翼体への取
り付け作業が必要である。
To refuel this aircraft, it is necessary to attach a refueling hose to the refueling port provided on the underside of the wing body, which requires installation work to the wing body several meters above the ground.

また、ハイドラントピツチには、貯蔵タンクか
ら高圧がかけられた航空機用燃料が供給されてお
り、例えば、150psi程度の圧力が与えられている
為、このままの圧力で航空機に給油を行うと、航
空機の燃料タンクを破損する恐れがある。
In addition, the hydrant pit is supplied with highly pressurized aircraft fuel from a storage tank, for example at a pressure of about 150 psi, so if you refuel an aircraft at this pressure, the aircraft will There is a risk of damaging the fuel tank.

よつて、減圧装置を用いて、45〜50psi程度の
圧力に減圧して給油を行う必要がある。
Therefore, it is necessary to supply oil by reducing the pressure to about 45 to 50 psi using a pressure reducing device.

この為、航空機の給油には、航空機の給油口に
接続される給油用ホースを備え、上面には昇降可
能な作業用エレベータデツキを有し、減圧装置、
圧力計、流量計、給油用フイルタセパレータ、シ
ヨツクアブソーバ等を具備する給油用車両が利用
されるものである。
For this reason, the aircraft refueling system is equipped with a refueling hose connected to the aircraft's fuel tank, a work elevator deck that can be raised and lowered on the top, a pressure reducing device,
A refueling vehicle equipped with a pressure gauge, a flow meter, a refueling filter separator, a shock absorber, etc. is used.

即ち、この給油用車両の作業用エレベータデツ
キが航空機の翼体下面にある給油口の真下になる
ように配置し、エレベータデツキを上昇させて、
作業者が給油口をカバーしているアクセスドアを
開き、給油ホースを給油口に取り付けるととも
に、給油ホースの他端をハイドラントピツトに連
結して給油を行うものである。
That is, the working elevator deck of this refueling vehicle is placed directly below the refueling port on the lower surface of the wing body of the aircraft, and the elevator deck is raised.
The operator opens the access door covering the fuel filler port, attaches the fuel hose to the fuel filler port, and connects the other end of the fuel hose to the hydrant pit to supply fuel.

〔考案が解決しようとする課題〕[The problem that the idea attempts to solve]

このような航空機給油用車両では、エレベータ
デツキの位置が、航空機の翼体下面の給油口真下
になるように移動させる必要があり、エレベータ
デツキの位置が給油口とずれている場合には、ア
クセスドアの開閉や給油用ホースの着脱が困難と
なる。この為、運転者以外の作業員が誘導を行
つ、適切な位置にこの車両を停止させることが行
われるが、運転者以外の作業者を必要とし、作業
者の安全性の確保や人件費等の問題点を内包する
ものであつた。
In such aircraft refueling vehicles, it is necessary to move the elevator deck so that it is directly below the refueling port on the underside of the aircraft wing. If the elevator deck is out of alignment with the refueling port, access It becomes difficult to open and close the door and to attach and detach the refueling hose. For this reason, a worker other than the driver guides the vehicle and stops the vehicle at an appropriate location, but this requires a worker other than the driver, ensuring worker safety and reducing labor costs. This included problems such as:

そこで、このような問題点を解決するために、
実開昭60−49099号公報には、航空機の給油口ま
たは給油口付近の目標の影像を受けるための受像
装置と、該受像装置で受けた影像を運転台に設け
た影像装置に伝達するための光伝達装置を設けて
なる給油位置の確認装置が、また、実開昭62−
138700号公報には、給油車の作業台の略直上方向
を撮影可能にテレビカメラを配設し、該テレビカ
メラで撮影された映像を伝送ケーブルを会して運
転席内に配設されたテレビ受像装置等に受像せし
めるように構成してなる給油位置の確認装置が記
載されている。
Therefore, in order to solve such problems,
Japanese Utility Model Application No. 60-49099 discloses an image receiving device for receiving an image of a target at or near an aircraft refueling port, and a device for transmitting the image received by the image receiving device to an image device installed in a driver's cab. A refueling position confirmation device equipped with an optical transmission device was also developed in 1982.
Publication No. 138700 discloses that a television camera is installed so as to be able to take pictures almost directly above the workbench of a refueling vehicle, and the images taken by the television camera are connected to a transmission cable and installed on a television set in the driver's seat. A refueling position confirmation device configured to have an image received by an image receiving device or the like is described.

なるほどこれらの考案によれば、給油用車両の
運転席に座つたままで航空機の給油口付近の映像
を見ることはできるものの、給油口と車両との相
対位置を直接確認するものではなく、前記映像を
もとに運転者が給油車を適宜移動させるものであ
るから、例えば、受像装置そして反射鏡を用いた
場合、この反射鏡の角度が狂うと給油車と供給口
との相対位置の確認は困難となり、また、この受
像装置としての反射鏡やテレビカメラの視野が広
角の場合、比較的離れた位置から給油口を確認で
きるため、ある程度給油口の近くまで給油車を接
近させることは容易であるが、視野が広いために
最終的な正確な位置合わせは困難であり、また反
対に、受像装置の視野が狭い場合には、ある程度
給油車が給油口に接近した後であれば位置合わせ
には有利なものの、そのような位置にまで接近す
る間は給油口を確認できないという難点があり、
実際には、これらの装置では給油車を正しい位置
に停止させることは必ずしも容易でなかつた。
Indeed, according to these ideas, it is possible to view images of the vicinity of the aircraft refueling port while sitting in the driver's seat of the refueling vehicle, but it is not possible to directly confirm the relative position between the refueling port and the vehicle; Since the driver moves the refueling vehicle appropriately based on the image, for example, if an image receiving device and a reflector are used, if the angle of the reflector is incorrect, it will be difficult to confirm the relative position of the refueling vehicle and the supply port. In addition, if the field of view of the reflector or television camera used as the image receiving device is wide-angle, the refueling port can be seen from a relatively distant position, so it is easy to approach the refueling vehicle to some extent close to the refueling port. However, final accurate positioning is difficult due to the wide field of view, and conversely, if the field of view of the image receiving device is narrow, positioning may be difficult after the refueling vehicle has approached the refueling port to some extent. Although this is an advantage, it has the disadvantage that the refueling port cannot be seen while approaching such a position.
In reality, it has not always been easy to stop the refueling vehicle at the correct position with these devices.

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

本考案は上記のような航空機の給油時の問題点
を鑑み、少なくとも、給油用ホースと、作業用エ
レベータデツキとを有し、前記作業用エレベータ
を利用して、空港の地上に設けられたハイドラン
トピツトと航空機の給油口を前記給油ホースによ
つて連結して給油を行う航空機給油用車両におい
て、前記航空機の翼体下面を照射し、車両が給油
作業に適切な位置にあるときに、航空機の翼体下
面の所定位置に光点が位置するように設定してな
る収束性を有する停止位置検出用投光手段と、前
記翼体下面を照射する投光手段の光点の位置を運
転席から視認可能な視認手段とを設けてなる航空
機給油用車両を提供せんとするものである。
In view of the above-mentioned problems when refueling an aircraft, the present invention has at least a refueling hose and a working elevator deck, and uses the working elevator to install a hydrant on the ground of an airport. In an aircraft refueling vehicle that refuels by connecting a pit and an aircraft refueling port with the refueling hose, the lower surface of the wing body of the aircraft is irradiated, and when the vehicle is in an appropriate position for refueling, the aircraft A stop position detection light projecting means with convergence is set so that a light point is located at a predetermined position on the lower surface of the wing body, and the position of the light point of the light projecting means that illuminates the lower surface of the wing body is determined by It is an object of the present invention to provide an aircraft refueling vehicle equipped with a visual recognition means that can be visually recognized from the vehicle.

前記の視認手段としては、ミラー、又はテレビ
カメラおよびテレビ受像装置からなるものを利用
することができる。
As the visual confirmation means, a mirror or a television camera and a television receiver can be used.

〔作用〕[Effect]

本考案に係る航空機給油用車両は上記のように
構成してなり、航空機の翼体下面を照射する投光
手段の光点位置を、ミラーやテレビカメラ等を利
用した視認手段で確認しながら、前記光点が翼体
の所定に位置にくるように車両を移動させて行
き、光点が当該所定の位置にきたときに車両を停
止させ、この位置で給油作業を行う。
The aircraft refueling vehicle according to the present invention is constructed as described above, and while confirming the light spot position of the light projecting means that illuminates the lower surface of the wing body of the aircraft using visual means such as a mirror or a television camera, The vehicle is moved so that the light spot is at a predetermined position on the wing body, and when the light spot is at the predetermined position, the vehicle is stopped, and the refueling operation is performed at this position.

〔実施例〕〔Example〕

以下、本考案の詳細を図示した実施例に基づい
て説明する。
Hereinafter, details of the present invention will be explained based on illustrated embodiments.

第1図および第2図は、本考案に係る航空機給
油用車両の実施例を示す説明用斜視図、第3図は
その側面図である。
1 and 2 are explanatory perspective views showing an embodiment of an aircraft refueling vehicle according to the present invention, and FIG. 3 is a side view thereof.

図中符号1は、本考案の航空機給油用車両本体
であり、2は、空港の駐機スポツトの地上に設け
られたハイドラントポツト3に着脱可能な端部を
有する給油用ホースで、4は、航空機5の翼体6
の下面に設けられた給油口7に着脱可能な端部を
有する給油用ホースであり、前記給油用ホース
2,4は、車両本体1内部に設けられる減圧装置
等を介して連続しており、ハイドラントピツト3
から航空機5に給油可能にされてなるものであ
る。
In the figure, reference numeral 1 is the aircraft refueling vehicle body of the present invention, 2 is a refueling hose having an end that can be attached to and detached from a hydrant pot 3 provided on the ground at an airport parking spot, and 4 is Wing body 6 of aircraft 5
It is a refueling hose having an end that is detachable from a refueling port 7 provided on the lower surface of the vehicle, and the refueling hoses 2 and 4 are connected to each other via a pressure reducing device or the like provided inside the vehicle main body 1. hydrant pit 3
It is possible to refuel the aircraft 5 from there.

8は、車両本体1の上面に設けられる作業用エ
レベータデツキであり、航空機5の翼体6下面の
作業が可能な高さに昇降可能にされてなるもので
あり、このエレベータデツキ8には、折り畳み式
の防護壁9と流量計等の計器類(図示せず)、昇
降装置10および作業者用昇降手段11等が設け
られており、給油作業に際しては、防護壁9を立
起させ、作業可能な高さにエレベータデツキ8を
上昇させて、作業者昇降手段11を利用してエレ
ベータデツキ8に搭乗して作業を行うものであ
る。
Reference numeral 8 denotes a working elevator deck provided on the upper surface of the vehicle body 1, which can be raised and lowered to a height that allows work on the lower surface of the wing body 6 of the aircraft 5. A foldable protective wall 9, instruments such as a flow meter (not shown), a lifting device 10, a lifting means 11 for workers, etc. are provided, and during refueling work, the protective wall 9 is erected and the work is carried out. The elevator deck 8 is raised to a possible height, and the worker uses the elevating means 11 to board the elevator deck 8 and perform work.

そして、符号12として示すものが、収束性の
あるライトからなる停止位置検出用投光手段であ
り、航空機5の翼体6下面を照射するように、上
方に向けて投光を行うものであり、本実施例で
は、給油用車両を給油に際して正しい位置に停止
させた場合に、投光手段12の光点が翼体6下面
のアクセスドア14に位置するように設定してな
る。この投光手段12は、エレベータデツキ8の
上面に設けることもできるが、エレベータデツキ
8の昇降に伴う、電源またはコード類の昇降を考
慮する必要があるので、図示したものは、エレベ
ータデツキ8の前面に取り付け、垂直よりやや後
方に傾斜して投光するように設定されている。
What is indicated by reference numeral 12 is a stop position detection light projecting means made of a convergent light, which projects light upward so as to illuminate the lower surface of the wing body 6 of the aircraft 5. In this embodiment, the light point of the light projecting means 12 is set to be located at the access door 14 on the lower surface of the wing body 6 when the refueling vehicle is stopped at the correct position for refueling. The light projecting means 12 can be provided on the upper surface of the elevator deck 8, but it is necessary to take into account the raising and lowering of the power supply or cords as the elevator deck 8 goes up and down. It is mounted on the front and is set to emit light at a slight angle backwards from the vertical direction.

13は、視認用ミラーであり、投光用手段12
によつて照射される航空機5の翼体6下面を車両
の運転席から視認可能とするものである。
13 is a viewing mirror, and the light projecting means 12
The lower surface of the wing body 6 of the aircraft 5 illuminated by the light beam is made visible from the driver's seat of the vehicle.

尚、この車両には、前記の他に、減圧装置、燃
料中の水分をチエツクする為の給油用フイルタセ
パレータ、流量計、圧力ゲージ、シヨツクアブソ
ーバ等が設けられており、前記流量計、圧力計等
の計器類はエレベータデツキ8上で目視できるよ
うに設置されている。
In addition to the above, this vehicle is also equipped with a pressure reducing device, a refueling filter separator for checking moisture in the fuel, a flow meter, a pressure gauge, a shock absorber, etc. Instruments such as the above are installed on the elevator deck 8 so that they can be visually observed.

上記のような本考案に係る航空機給油用車両
は、投光手段12によつて上方に投光して航空機
5の翼体6下面にその光点をあてる。これを運転
車は、視認用ミラー13によつて確認しながら車
両を移動させ、投光手段12の光点が翼体6下面
のアクセスドア14に位置した時に車両を停止さ
せる。この場合、前記投光手段12は、エレベー
タデツキ8の前方に設置され、かつ垂直よりやや
後方に投光しているので、光点がアクセスドア1
4上にある時に、エレベータデツキ8がアクセス
ドア14の直下になるように設定されてなるもの
である。
The aircraft refueling vehicle according to the present invention as described above projects light upward by the light projecting means 12 to illuminate the lower surface of the wing body 6 of the aircraft 5 with the light spot. The driving vehicle moves the vehicle while confirming this using the viewing mirror 13, and stops the vehicle when the light spot of the light projecting means 12 is located at the access door 14 on the lower surface of the wing body 6. In this case, the light projecting means 12 is installed in front of the elevator deck 8 and projects light slightly backward from the vertical direction, so that the light spot is directed toward the access door 1.
4, the elevator deck 8 is set directly below the access door 14.

このように、本考案に係る航空機給油用車両に
よれば、運転者が運転席に座つたままで視認用ミ
ラー13を通して投光手段12によつて照射させ
る翼体6下面の光点を確認しながら車両を移動さ
せることによつて、車両を適切な給油位置に停止
させることが可能となり、人手を省くことが可能
となるとともに、前記投光手段12の光点を翼体
6下面の所定位置に合わせることで、給油用車両
の停止位置を正確にすることができる。
As described above, according to the aircraft refueling vehicle according to the present invention, the driver can check the light spot on the lower surface of the wing body 6 illuminated by the light projection means 12 through the viewing mirror 13 while sitting in the driver's seat. By moving the vehicle while moving the vehicle, it becomes possible to stop the vehicle at an appropriate refueling position, save manpower, and direct the light point of the light projecting means 12 to a predetermined position on the lower surface of the wing body 6. By matching this, the stopping position of the refueling vehicle can be made accurate.

尚、上記の実施例では、翼体6下面に照射され
る投光手段12の光点を視認するための視認手段
としてミラーを用いているが、このミラーのかわ
りに、テレビカメラおよびその受像装置といつた
具合に、視認手段としては給油用車両の運転席か
ら航空機5の翼体6下面を視認しうるものであれ
ば、どのようなものでもよい。
Incidentally, in the above embodiment, a mirror is used as a viewing means for visually recognizing the light spot of the light projecting means 12 that is irradiated onto the lower surface of the wing body 6, but instead of this mirror, a television camera and its image receiving device are used. As such, any visual recognition means may be used as long as the lower surface of the wing body 6 of the aircraft 5 can be visually recognized from the driver's seat of the refueling vehicle.

〔考案の効果〕[Effect of idea]

以上の如く本考案に係る航空機給油用車両によ
れば、停止位置検出用投光手段の光点の位置を運
転席から視認手段で確認しながら当該光点が航空
機の翼体下面の所定位置にくるように車両を移動
させてゆくだけで、給油用車両を給油作業に適切
な位置に停車させることを簡単、かつ確実に行う
ことができ、また、前記作業は運転車が単独で行
うことができることから、それ以外の余分な作業
人員を配置する必要がなく、作業者の安全確保の
問題や人件費等の問題も解消しうるものである。
As described above, according to the aircraft refueling vehicle according to the present invention, while checking the position of the light spot of the stop position detection light projecting means from the driver's seat using the visual confirmation means, the light spot is positioned at a predetermined position on the lower surface of the wing body of the aircraft. By simply moving the vehicle in the same direction, the refueling vehicle can be easily and reliably stopped at an appropriate position for refueling work, and the driver vehicle can perform the work alone. Because it can be done, there is no need to allocate extra workers, and problems such as ensuring worker safety and personnel costs can be resolved.

【図面の簡単な説明】[Brief explanation of the drawing]

第1図、第2図は本考案に係る航空機給油用車
両の1実施例を示す説明用斜視図、第3図は前記
航空機給油用車両の説明用側面図である。 1……航空機給油用車両本体、2……給油用ホ
ース、3……ハイドラントピツト、4……給油用
ホース、5……航空機、6……翼体、7……給油
口、8……エレベータデツキ、9……防護壁、1
0……昇降手段、11……作業者用昇降手段、1
2……投光手段、13……視認用ミラー、14…
…アクセスドア。
FIGS. 1 and 2 are explanatory perspective views showing one embodiment of an aircraft refueling vehicle according to the present invention, and FIG. 3 is an explanatory side view of the aircraft refueling vehicle. 1...Aircraft refueling vehicle body, 2...Refueling hose, 3...Hydrant pit, 4...Refueling hose, 5...Aircraft, 6...Wing body, 7...Refueling port, 8... Elevator deck, 9...protective wall, 1
0... Lifting means, 11... Lifting means for workers, 1
2... Light projecting means, 13... Viewing mirror, 14...
...access door.

Claims (1)

【実用新案登録請求の範囲】 1 少なくとも、給油用ホースと、作業用エレベ
ータデツキとを有し、前記作業用エレベータを
利用して、空港の地上に設けられたハイドラン
トピツトと航空機の給油口を前記給油ホースに
よつて連結して給油を行う航空機給油用車両に
おいて、前記航空機の翼体下面を照射し、車両
が給油作業に適切な位置にあるときに、航空機
の翼体下面の所定位置に光点が位置するように
設定してなる収束性を有する停止位置検出用投
光手段と、前記翼体下面を照射する投光手段の
光点の位置を運転席から視認可能な視認手段と
を設けてなる航空機給油用車両。 2 視認手段として、ミラーを利用してなる実用
新案登録請求の範囲第1項記載の航空機給油用
車両。 3 視認手段として、テレビカメラおよびテレビ
受像装置からなるものを利用してなる実用新案
登録請求の範囲第1項記載の航空機給油用車
両。
[Claims for Utility Model Registration] 1. A method having at least a refueling hose and a working elevator deck, and using the working elevator to connect a hydrant pit provided on the ground of an airport and an aircraft refueling port. In the aircraft refueling vehicle connected by the refueling hose for refueling, the lower surface of the wing body of the aircraft is irradiated, and when the vehicle is in an appropriate position for refueling work, the vehicle is irradiated at a predetermined position on the lower surface of the aircraft wing body. A light projecting means for detecting a stop position having convergence and configured such that a light spot is located; and a visual confirmation means that allows the position of the light spot of the light projecting means that illuminates the lower surface of the wing body to be visually recognized from the driver's seat. Aircraft refueling vehicle. 2. An aircraft refueling vehicle according to claim 1, which utilizes a mirror as a visual recognition means. 3. The aircraft refueling vehicle according to claim 1, which utilizes a television camera and a television receiver as visual recognition means.
JP1988158745U 1988-12-06 1988-12-06 Expired JPH0447040Y2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP1988158745U JPH0447040Y2 (en) 1988-12-06 1988-12-06

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP1988158745U JPH0447040Y2 (en) 1988-12-06 1988-12-06

Publications (2)

Publication Number Publication Date
JPH0278498U JPH0278498U (en) 1990-06-15
JPH0447040Y2 true JPH0447040Y2 (en) 1992-11-06

Family

ID=31439350

Family Applications (1)

Application Number Title Priority Date Filing Date
JP1988158745U Expired JPH0447040Y2 (en) 1988-12-06 1988-12-06

Country Status (1)

Country Link
JP (1) JPH0447040Y2 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2589878Y2 (en) * 1992-06-24 1999-02-03 昭和飛行機工業株式会社 Refueling car

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6049099U (en) * 1983-09-14 1985-04-06 昭和飛行機工業株式会社 Refueling position confirmation device for refueling vehicles
JPS62138700U (en) * 1986-02-27 1987-09-01

Also Published As

Publication number Publication date
JPH0278498U (en) 1990-06-15

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