JPH0735838Y2 - Aircraft boarding bridge movable floor device - Google Patents

Aircraft boarding bridge movable floor device

Info

Publication number
JPH0735838Y2
JPH0735838Y2 JP1985082987U JP8298785U JPH0735838Y2 JP H0735838 Y2 JPH0735838 Y2 JP H0735838Y2 JP 1985082987 U JP1985082987 U JP 1985082987U JP 8298785 U JP8298785 U JP 8298785U JP H0735838 Y2 JPH0735838 Y2 JP H0735838Y2
Authority
JP
Japan
Prior art keywords
movable
bracket
floor
fender
aircraft
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 - Lifetime
Application number
JP1985082987U
Other languages
Japanese (ja)
Other versions
JPS61198200U (en
Inventor
忠尚 烏谷
Original Assignee
尾部工業株式会社
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 尾部工業株式会社 filed Critical 尾部工業株式会社
Priority to JP1985082987U priority Critical patent/JPH0735838Y2/en
Publication of JPS61198200U publication Critical patent/JPS61198200U/ja
Application granted granted Critical
Publication of JPH0735838Y2 publication Critical patent/JPH0735838Y2/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Description

【考案の詳細な説明】 産業上の利用分野 この考案は、航空機乗降口床面と可動床防舷部が常に平
行に接舷することができる航空機搭乗橋可動床装置に関
するものである。
TECHNICAL FIELD The present invention relates to an aircraft boarding bridge movable floor device in which an aircraft entrance / exit floor surface and a movable floor fender can always come in parallel.

従来の技術 従来は固定床の一部分を折り曲げ、又、一部分床の可動
を行なって部分的に航空機床面に合致しようとするもの
であるが、各航空機には機種により床面にレベル差があ
り、航空機乗降口床と可動橋先端円形室との間に約10〜
12°程度の傾斜角が付く状態である。この様な条件下に
於て、安全に乗客を乗降せしむる為、航空機搭乗橋可動
床装置に於て、先端円形室の連接部近傍の固定床はその
一部を切欠状となし、該切欠部には先端部を端縁部材と
連結した複数の骨部材及びこれら骨部材上に貼着した可
撓性床板より成る可動床を配置し、捩り状に昇降しうる
ようにしたものが知られている(例えば実開昭59-16050
0号公報参照)。
Conventional technology Conventionally, a part of a fixed floor is bent, and a part of the floor is moved to try to partially match the aircraft floor surface, but each aircraft has a level difference on the floor surface depending on the model. Approximately 10 ~
It is in a state with an inclination angle of about 12 °. In order to safely get on and off passengers under such conditions, in the movable boarding device for an aircraft boarding bridge, the fixed floor in the vicinity of the connecting part of the tip circular chamber has a part notched, It is known that a movable floor composed of a plurality of bone members whose front ends are connected to edge members and a flexible floor plate attached to these bone members is arranged in the cutout portion so that the movable floor can be lifted and lowered in a torsional manner. (For example, the actual exploitation Sho 59-16050
No. 0).

考案が解決しようとする問題点 しかし、各種航空機は前述のように乗降口には何れの場
合においてもレベル差があって、航空機の接舷時、航空
機乗降口の床面と可動橋先端円形室床との間に傾斜面を
生じて接舷に支障を来すのみでなく、機種によっては航
空機扉が可動橋先端円形室床面に接触する為、両床面に
段差を付けて運用していた。これは、航空機体と傾斜角
が大きい程高い段差が必要と成り、乗客によっては介添
えを要し、安全性が十分でないと云う問題点があった。
又一部床補正した場合も床面自体に段差を生じ不十分で
あった。
Problems to be solved by the invention However, as described above, the various aircraft have different levels at the entrances and exits in each case, and when the aircraft is berthing, the floor of the entrance and exit of the aircraft and the circular room at the tip of the movable bridge Not only does it cause an incline between the floor and the hull, but depending on the model, the aircraft door contacts the floor of the circular room at the tip of the movable bridge, so there are steps on both floors for operation. It was This requires a higher step as the inclination angle increases with respect to the aircraft body, and some passengers need to intervene, resulting in a problem that safety is not sufficient.
In addition, even if the floor was partially corrected, a step was generated on the floor itself, which was insufficient.

そこで、本考案は、このような従来の問題点に着目して
なされたものであって、可動床における航空機への接舷
時、常に航空機床面に段差なく平行と成る様接舷し、可
動床全面が、傾斜角に適合して、変形する様考案された
ものである。先端防舷部と平行に配置した多数の可動棒
を固定ブラケット側と可動ブラケット側の運動により、
安全かつ滑らかな全面変形した可動床面を作ることによ
り、上記問題点を解決することを目的としている。
Therefore, the present invention has been made by paying attention to such a conventional problem, and when porting to an aircraft on a movable floor, the port is always parallel to the floor of the aircraft without any step, and the mobile floor is movable. It is designed so that the entire surface of the floor will be deformed according to the inclination angle. A large number of movable rods arranged in parallel with the tip fender are moved by the fixed bracket side and the movable bracket side,
The purpose is to solve the above problems by creating a safe and smooth movable floor surface that is completely deformed.

問題点を解決するための手段 上記目的を達成するために、本考案における航空機搭乗
橋可動床装置は、前記記載事項と共に通路としての歩行
性を重視し、部分変形に見るわずかな通路面段差を生じ
る事なきよう防舷部に対し平行に配列して可動棒を複数
設け、複数の可動棒よりなる床面を足型が直交する方向
の歩行が出来る様にして、歩行しやすくした可動床を含
むものである。そしてこの可動棒の両側方に少なくとも
2ヶ所以上のブラケットを設け、一方の固定ブラケット
位置を基準点として可動棒に貫通架設して接舷するよう
になし、他方のブラケットは可動とし、該可動ブラケッ
トを可動棒に貫通して支承し、該可動ブラケットを任意
駆動機構により作動して可動床の昇降運動を行い、可動
床全面を傾斜角に合せ、自在に変形し、該床面の先端の
防舷部を航空機床に平行に接舷するように連接してなる
ものである。
Means for Solving the Problems In order to achieve the above-mentioned object, the aircraft boarding bridge movable floor device according to the present invention attaches importance to the walkability as a passage together with the above-mentioned items, and a slight passage surface step seen in partial deformation is provided. To prevent this from happening, the movable bar is arranged in parallel with the fender and a plurality of movable bars are provided. It is a waste. Then, at least two or more brackets are provided on both sides of the movable rod so that the movable rod is pierced through the movable rod with one fixed bracket position as a reference point so that the other bracket is movable. Is pierced through the movable rod, and the movable bracket is operated by an arbitrary drive mechanism to elevate and lower the movable floor, and the entire movable floor is adjusted to the inclination angle and freely deformed to prevent the tip of the floor surface from being deformed. It is formed by connecting the port side so that the port side is parallel to the aircraft floor.

作用 航空機床面に対し、可動床の先端の防舷部が傾斜した場
合、先づ固定ブラケットの位置を基準点として接舷し、
次に駆動部(3c)の歯車(6)の回転により作動用ブラ
ケット(3a)を介して可動ブラケット(3)を昇降操作
する。そして可動ブラケット(3)が昇降すると、可動
床面を構成する複数の可動棒に微少ながら段差を生じ可
動床全面が自在に変形しながら平滑な可動床面が形成さ
れるので、該可動床面上にマットを敷設する。この場
合、前記駆動装置の操作により可動床の先端防舷部が航
空機の床面と全く平行に接舷することができると共に通
路面として局部的な段差を生じない滑らかな歩路面が出
来る。
Action When the fender at the tip of the movable floor inclines with respect to the aircraft floor, first attach the fixed bracket as the reference point,
Next, the movable bracket (3) is moved up and down through the operation bracket (3a) by the rotation of the gear (6) of the drive unit (3c). Then, when the movable bracket (3) moves up and down, a plurality of movable rods forming the movable floor surface are formed with slight steps, and the entire movable floor is freely deformed to form a smooth movable floor surface. Lay the mat on top. In this case, by operating the drive device, the tip fender of the movable floor can be brought into contact with the floor surface of the aircraft in a completely parallel manner, and a smooth walkway surface that does not cause a local step difference can be formed as a passage surface.

実施例 実施例について図面を参照して説明する。Examples Examples will be described with reference to the drawings.

第1図〜第6図において(1)は可動棒であって、先端
縁に設けた防舷部(5)に対し、平行に床面として多数
配列する。(2)は可動床であって、複数の可動棒を平
行に配列して形成され、その可動床面にマットを敷設し
て緩衝床面を形成する。(3)は可動ブラケットであっ
て、床を形成する裏側に配列した前記可動棒(1)の一
側方に前記可動ブラケット(3)を該可動棒に直交貫通
し、該貫通したブラケット(3)の先端を軸支した作動
用ブラケット(3a)を先端部より基端部方向に傾斜させ
て延長し、該作動用ブラケット(3a)に、可動ブラケッ
ト(3)の基端部に軸支した支持ブラケット(3b)を垂
下させて前記作動用ブラケット(3a)に接続固着し、そ
の固着部を交点として外部に突出させた作動用ブラケッ
ト(3a)の外端部を駆動部(3c)に形成し、該駆動部
(3c)に駆動装置(6)を接触させる。この場合、前記
駆動部(3c)は例えば、ラックギアに形成し、駆動装置
(6)は例えば歯車に形成して、ラックギアと歯車とを
噛み合せて駆動機構を構成し、正逆回転により可動床を
昇降させる。(4)は固定ブラケットであって、可動ブ
ラケット(3)とは反対側に設けて基準機能を有するよ
う固定ブラケット(4)にて可動棒(1)を貫通して防
舷部(5)にて連絡し、下面に固定ブラケット(4)と
殆んど同長のブラケットを平行に設けて固定ブラケット
(4)の両端を縦杆及び可動橋床(7)に連結して固定
枠に構成する。この固定ブラケット(4)の位置を基準
点として航空機に対し接舷するとき、可動ブラケット
(3)を作動用ブラケット(3a)を介して駆動装置によ
り昇降作用を行い、可動床の防舷部は平行に航空機床に
接舷して可動床を形成し、該可動床は可動橋床(7)に
接続しており通路に連続している。
In FIGS. 1 to 6, (1) is a movable rod, and a large number of the rods are arranged in parallel as a floor surface with respect to the fender (5) provided at the tip edge. (2) is a movable floor, which is formed by arranging a plurality of movable rods in parallel, and a mat is laid on the movable floor surface to form a buffer floor surface. (3) is a movable bracket, and the movable bracket (3) is orthogonally penetrated to one side of the movable bar (1) arranged on the back side forming the floor, and the penetrating bracket (3) ), The operation bracket (3a) pivotally supporting the tip of the movable bracket (3a) is extended to the operation bracket (3a) by inclining toward the base end direction from the tip end. The support bracket (3b) is hung down to connect and fix to the operating bracket (3a), and the outer end of the operating bracket (3a) protruding outward with the fixed portion as an intersection is formed on the drive section (3c). Then, the drive unit (6) is brought into contact with the drive unit (3c). In this case, the drive unit (3c) is formed, for example, in a rack gear, the drive unit (6) is formed, for example, in a gear, and the rack gear and the gear are meshed with each other to form a drive mechanism. Raise and lower. (4) is a fixed bracket, which is provided on the side opposite to the movable bracket (3) and penetrates the movable rod (1) by the fixed bracket (4) to form a fender (5). Then, a fixed bracket (4) and a bracket having almost the same length as the fixed bracket (4) are provided in parallel on the lower surface, and both ends of the fixed bracket (4) are connected to the vertical rod and the movable bridge deck (7) to form a fixed frame. . When the fixed bracket (4) is used as a reference point for porting to the aircraft, the movable bracket (3) is moved up and down by the drive device through the operation bracket (3a), and the fender of the movable floor is Parallel to the aircraft floor, a movable floor is formed, which is connected to the movable bridge floor (7) and is continuous with the passage.

第5図、第6図は従来の可動床を含む可動橋床を示すも
のであって、(8)は固定床部、(9)は斜線床部であ
って、前記固定床部(8)と斜線床部(9)とは切り離
されてユニバーサルジョイントにて連絡している。
5 and 6 show a movable bridge deck including a conventional movable floor, in which (8) is a fixed floor portion, (9) is a diagonal floor portion, and the fixed floor portion (8) is shown. And the slanted floor (9) are separated and are connected by a universal joint.

考案の効果 本考案は、上述のように構成されているので、次に記載
する効果を奏する。
Effect of the Invention Since the present invention is configured as described above, it has the following effects.

可動床の先端に取付けた防舷部に平行して内部に複数の
可動棒を密着配列し、該可動棒の一側方に固定ブラケッ
トを貫通させて支持固定し、他側方には可動ブラケット
(3)を貫通させ、可動ブラケットの両端をピン可動構
造にて先端と基端とに夫々ブラケットを取りつけ、該ブ
ラケットのうち、先端部に軸支した作動用ブラケット
(3a)を基端方向に可動ブラケット(3)に対し傾斜延
長し、基端部に軸支した支持ブラケット(3b)は前記作
動用ブラケット(3a)に直交させて固着し、該ブラケッ
トの延長端を駆動部に形成し該駆動部に駆動機構を作動
状態に構成しているので、航空機床面に対し、可動床先
端部が傾斜した場合、固定ブラケット位置を基準点とし
て接舷し、前記駆動部を駆動装置にて作動することによ
り航空機乗降口の床面と可動床の防舷部が平行に接舷す
ることができ、さらにマットを可動床面上に敷くことに
より全面が円滑変形した凹凸のない歩行に安全な床面と
なり乗客の昇降に当り足をくじいたり、何等の支障がな
く極めて簡単なる構造で接舷が容易である。また、航空
機の乗降口扉の開閉による段差を必要とすることなく円
滑に扉の開閉もでき安全なる通路の構成が出来る実益が
ある。
A plurality of movable rods are closely arranged in parallel with the fender attached to the tip of the movable floor, and a fixed bracket is passed through one side of the movable rod to support and fix the movable rod, and a movable bracket is provided on the other side. (3) is penetrated, and both ends of the movable bracket are attached to the tip and the base end by a pin movable structure, and the operation bracket (3a) pivotally supported on the tip of the bracket in the base end direction. A support bracket (3b), which extends obliquely with respect to the movable bracket (3) and is axially supported at the base end, is fixed orthogonally to the operating bracket (3a), and the extended end of the bracket is formed as a drive unit. Since the drive mechanism is configured to operate in the drive unit, when the tip of the movable floor inclines with respect to the aircraft floor surface, the fixed bracket position is used as the reference point to operate the drive unit with the drive device. The floor of the aircraft entrance / exit The fenders of the movable floor can be sewn in parallel, and by placing a mat on the movable floor, the entire surface is smoothly deformed, making it a safe floor for walking without unevenness, and ascending and descending passengers It is easy to berth with a very simple structure without any problems. In addition, there is a practical benefit that the door can be smoothly opened and closed without the need for a step due to the opening and closing of the entrance door of the aircraft, and a safe passage can be configured.

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

第1図は本考案可動床の取付状態を示す一部切除した斜
視図、第2図は、本考案可動床の可動棒とブラケットと
の取付状態を示す一部切欠平面図、第3図は第2図A−
A線における作動及び可動ブラケット取付構造を示す断
面図、第4図は第2図B−B線における固定ブラケット
の構造を示す断面図、第5図は従来の可動橋床の平面
図、第6図は従来の同上の正面図である。 1……可動棒、2……可動床 3……可動ブラケット、3a……作動用ブラケット 3b……支持ブラケット、3c……駆動部 4……固定ブラケット、5……防舷部 6……駆動装置
FIG. 1 is a partially cutaway perspective view showing a movable floor of the present invention, showing a mounting state, FIG. 2 is a partially cutaway plan view showing a mounting state of a movable rod and a bracket of the movable floor of the present invention, and FIG. Fig. 2 A-
Sectional drawing which shows the operation | movement in A line and a movable bracket attachment structure, FIG. 4 is sectional drawing which shows the structure of the fixed bracket in FIG. 2 BB line, FIG. 5 is a top view of the conventional movable bridge deck, 6th. The figure is a conventional front view of the same. 1 ... Movable rod, 2 ... Movable floor 3 ... Movable bracket, 3a ... Operating bracket 3b ... Support bracket, 3c ... Drive part 4 ... Fixed bracket, 5 ... Fender part 6 ... Drive apparatus

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] 【請求項1】防舷部(5)に対し平行に複数の可動棒
(1)を配列された航空機搭乗可動床装置の可動床
(2)において、前記可動棒(1)の一方には固定ブラ
ケット(4)を貫通させ、可動橋床(7)と防舷部
(5)との間に固定支承して接舷基準点とし、前記基準
点を介在させた前記可動棒の他方には可動ブラケット
(3)を貫通させ、前記可動ブラケットの基端部を可動
橋床(7)に枢支し、前記可動ブラケットの先端部を防
舷部(5)内に枢着するとともに、前記可動ブラケット
の先端部に作動用ブラケット(3a)を枢着し、前記作動
用ブラケットの他端を基端部方向に傾斜延長し、さら
に、前記作動用ブラケットの基端部に前記可動ブラケッ
トの基端部より垂下させた支持ブラケット(3b)を接続
固着し、固着部を交点として外方に突出させた駆動部
(3c)を駆動装置(6)に接触し、前記作動用ブラケッ
トを昇降運動させることにより可動床全面を自在に変形
して上下動或は傾斜角に適合させ、前記防舷部を航空機
床に平行に接舷することができるようにしたことを特徴
とする航空機搭乗橋可動床装置。
1. A movable floor (2) of an aircraft boarding movable floor device in which a plurality of movable rods (1) are arranged in parallel to a fender (5) and fixed to one of the movable rods (1). The bracket (4) is penetrated and fixedly supported between the movable bridge deck (7) and the fender (5) to serve as a fender reference point, and the movable rod is movable to the other side of the reference point. The bracket (3) is penetrated, the base end of the movable bracket is pivotally supported on the movable bridge deck (7), and the tip of the movable bracket is pivotally attached to the fender (5), and the movable bracket is The operation bracket (3a) is pivotally attached to the tip end of the movable bracket, the other end of the operation bracket is inclined and extended toward the base end, and the base end of the movable bracket is attached to the base end of the operation bracket. Connect and fix the hanging support bracket (3b) to the outside with the fixed part as the intersection. The projecting drive part (3c) is brought into contact with the drive device (6), and the operating bracket is moved up and down to freely deform the entire movable floor to match the vertical movement or the inclination angle, and the fender. An aircraft boarding bridge movable floor device, characterized in that the section can be ported parallel to the aircraft floor.
JP1985082987U 1985-06-01 1985-06-01 Aircraft boarding bridge movable floor device Expired - Lifetime JPH0735838Y2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP1985082987U JPH0735838Y2 (en) 1985-06-01 1985-06-01 Aircraft boarding bridge movable floor device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP1985082987U JPH0735838Y2 (en) 1985-06-01 1985-06-01 Aircraft boarding bridge movable floor device

Publications (2)

Publication Number Publication Date
JPS61198200U JPS61198200U (en) 1986-12-11
JPH0735838Y2 true JPH0735838Y2 (en) 1995-08-16

Family

ID=30631206

Family Applications (1)

Application Number Title Priority Date Filing Date
JP1985082987U Expired - Lifetime JPH0735838Y2 (en) 1985-06-01 1985-06-01 Aircraft boarding bridge movable floor device

Country Status (1)

Country Link
JP (1) JPH0735838Y2 (en)

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS59160500U (en) * 1983-04-13 1984-10-27 新明和工業株式会社 Joint movable floor device in boarding bridge

Also Published As

Publication number Publication date
JPS61198200U (en) 1986-12-11

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