JPH059280Y2 - - Google Patents

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Publication number
JPH059280Y2
JPH059280Y2 JP1989018678U JP1867889U JPH059280Y2 JP H059280 Y2 JPH059280 Y2 JP H059280Y2 JP 1989018678 U JP1989018678 U JP 1989018678U JP 1867889 U JP1867889 U JP 1867889U JP H059280 Y2 JPH059280 Y2 JP H059280Y2
Authority
JP
Japan
Prior art keywords
closure
contact
fuselage
aircraft
boarding bridge
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
JP1989018678U
Other languages
Japanese (ja)
Other versions
JPH02109799U (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 JP1989018678U priority Critical patent/JPH059280Y2/ja
Publication of JPH02109799U publication Critical patent/JPH02109799U/ja
Application granted granted Critical
Publication of JPH059280Y2 publication Critical patent/JPH059280Y2/ja
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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  • Seal Device For Vehicle (AREA)
  • Vehicle Waterproofing, Decoration, And Sanitation Devices (AREA)
  • Body Structure For Vehicles (AREA)

Description

【考案の詳細な説明】 (産業上の利用分野) 本考案は、乗り物の乗降口に接続するボーデイ
ングブリツジのクロージヤに関する。
[Detailed Description of the Invention] (Industrial Field of Application) The present invention relates to a closure for a boarding bridge connected to a vehicle entrance/exit.

(従来の技術) 空港の適宜の位置に停止した航空機と空港ビル
とを連結するボーデイングブリツジとして、空港
ビルに基端を連結した基部通路体と先端部の機体
連結用キヤブとの間に中間通路体を設け、この中
間通路体と上記基部通路体、並びに上記機体連結
用キヤブとを、それぞれ基端側と先端側の両円形
室を介して水平回動可能に連結した構造のものは
一般に知られている(例えば、特公昭61−5952号
公報参照)。
(Prior art) As a boarding bridge that connects an aircraft stopped at an appropriate location at an airport and an airport building, a boarding bridge is installed between a base passage body whose base end is connected to the airport building and a cab for connecting the aircraft at its tip. A structure in which an intermediate passage body is provided, and this intermediate passage body, the base passage body, and the cab for connecting the fuselage are horizontally rotatably connected through circular chambers on both the base end side and the distal side, respectively. It is generally known (for example, see Japanese Patent Publication No. 61-5952).

かかるボーデイングブリツジの上記機体連結用
キヤブには、機体への連結口の周縁に機体に当接
せしめて、この機体連結用キヤブと機体との間を
シールするクロージヤが設けられている。クロー
ジヤは、ナイロン製のターポリン(防水帆布)を
利用してベローズ状に形成されていて、機体連結
用キヤブのフロアを機体に当接せしめた状態でベ
ローズの伸縮を利用して前方に倒し、機体の乗降
口の上縁及び両側縁にクロージヤの当接口部を当
接せしめるようになされている。
The fuselage connecting cab of such a boarding bridge is provided with a closure around the periphery of the connecting port to the fuselage, which abuts against the fuselage and seals between the fuselage connecting cab and the fuselage. The closure is formed into a bellows shape using a nylon tarpaulin (waterproof canvas).With the floor of the cabin connecting the aircraft in contact with the aircraft, the closure is folded forward using the expansion and contraction of the bellows, and the aircraft is The contact opening portion of the closure is brought into contact with the upper edge and both side edges of the entrance/exit door.

また、実開昭62−56400号公報には、可撓性フ
レーム部材の前面に取り付けられた緩衝材と、該
緩衝材を覆う外装シートとの間にバネ板とゴム板
とからなる当板を介在させ、該当板を緩衝材とは
接合せずに、外装シート材に接合し、外装シート
材が機体の湾曲に沿つて湾曲するようにしたもの
が記載されている。
Furthermore, Japanese Utility Model Application Publication No. 62-56400 discloses that a plate made of a spring plate and a rubber plate is installed between a cushioning material attached to the front surface of a flexible frame member and an exterior sheet covering the cushioning material. It is described that the relevant plate is not joined to the cushioning material but is joined to the exterior sheet material so that the exterior sheet material curves along the curvature of the aircraft body.

すなわち、このものは、緩衝材の前面を単に外
装シート材によつて覆つただけでは、機体に当接
させた際に緩衝材の前面が機体の当接面よりも小
さな曲率半径で湾曲して収縮した状態になり、そ
のために、例えば外装シート材の左右方向の両端
は機体に当接して中央部は当接しない、あるいは
外装シート材にしわ寄りを生じて隙間を生ずると
いう問題を解決するものである。つまり、外装シ
ート材が緩衝材前面の湾曲に伴つて弛むことをそ
の背面の当板によつて防止しようとするものであ
る。
In other words, if the front surface of the cushioning material is simply covered with an exterior sheet material, the front surface of the cushioning material will curve with a smaller radius of curvature than the contact surface of the aircraft body when it comes into contact with the aircraft. This is to solve the problem that the outer sheet material is in a contracted state, and as a result, for example, both ends of the exterior sheet material in the left and right direction come into contact with the aircraft body but the center part does not, or the exterior sheet material wrinkles and creates a gap. It is. That is, the purpose is to prevent the exterior sheet material from loosening due to the curvature of the front surface of the cushioning material, by means of the backing plate.

(考案が解決しようとする課題) しかし、上述の如き当板によつて外装シート材
の弛みを防止するものでは、新品のときには効果
があるが、その使用回数が多くなつてくると、外
装シート材自体が可撓性を有し且つ伸縮性を有す
る関係で、雨水の影響により、また機体との接触
によつて伸び、その結果、この外装シート材にし
わが常時寄つた状態になり易い。このため、外装
シート材と機体との密着性が低下し、上記しわに
よつて生ずる隙間から雨や風が機体ないしは機体
連結用キヤブの内部に浸入してくることがある。
(Problem to be solved by the invention) However, the above-mentioned backing plate that prevents the exterior sheet material from loosening is effective when it is new, but as the number of times it is used increases, the Since the material itself is flexible and stretchable, it stretches due to the influence of rainwater and contact with the aircraft body, and as a result, the exterior sheet material tends to be wrinkled all the time. As a result, the adhesion between the exterior sheet material and the fuselage is reduced, and rain and wind may infiltrate into the fuselage or the fuselage connection cab through the gaps created by the wrinkles.

すなわち、本考案の課題は、上記クロージヤの
シール性を簡単な構造で高くできるようにするこ
とにある。
That is, an object of the present invention is to improve the sealing performance of the closure with a simple structure.

(課題を解決するための手段) 本考案は、このような課題に対して、上記クロ
ージヤの機体への当接面にこの当接面を構成する
上記ターポリンのような防水シートよりも曲がり
難いシール部材を設けることにより、クロージヤ
のシール性の向上を図ろうとするものである。
(Means for Solving the Problems) In order to solve these problems, the present invention provides a seal that is more difficult to bend than the waterproof sheet such as the tarpaulin that constitutes the contact surface of the closure to the fuselage. By providing the member, the sealing performance of the closure is improved.

すなわち、その手段は、乗り物への連結口の周
縁に前後方向へ伸縮可能なクロージヤが設けら
れ、このクロージヤの乗り物への当接口部が防水
シートにて構成されたボーデイングブリツジにお
いて、上記当接口部の少なくとも上縁部分には前
方に突出し且つこの当接口部の縁に沿つて延び上
記乗り物に当接せしめられる突条のシール部材が
設けられていて、このシール部材はその曲げ強度
が上記防水シートよりも高く設定されていること
を特徴とするボーデイングブリツジのクロージヤ
である。
That is, this means is provided in a boarding bridge in which a closure that is extendable and retractable in the front and back direction is provided on the periphery of the connection port to the vehicle, and the contact port of the closure to the vehicle is constructed of a waterproof sheet. At least the upper edge portion of the abutting portion is provided with a sealing member having a protruding strip that projects forward, extends along the edge of the abutting port, and comes into contact with the vehicle, and this sealing member has a bending strength as described above. This is a boarding bridge closure characterized by being set higher than the tarpaulin.

(作用) 上記クロージヤにおいては、シール部材が機体
に当接することによつてボーデイングブリツジと
機体との間のシールがなされるが、このシール部
材は機体への当接口部を構成する防水シートより
も曲げ強度が高いから、それ自身にしわを生じ難
いとともに、このシール部材が上記当接口部のし
わ寄りを防止する補強リブとして機能する。
(Function) In the closure described above, a seal is created between the boarding bridge and the fuselage by the sealing member coming into contact with the fuselage. Since the sealing member has higher bending strength than the sealing member, it is difficult to wrinkle itself, and the sealing member functions as a reinforcing rib to prevent the abutment opening from wrinkling.

(考案の効果) 従つて、本考案によれば、クロージヤの当接口
部にこの当接口部を構成する防水シートよりも曲
げ強度が高い突条のシール部材を設けたから、こ
のシール部材をその全長にわたつて乗り物に確実
に当接せしめて、この乗り物とボーデイングブリ
ツジとの間のシール性の向上を図ることができる
とともに、上記当接面のしわ寄りを防止してその
耐久性の向上を図ることができるようになる。
(Effects of the invention) Therefore, according to the invention, since a protruding seal member having higher bending strength than the waterproof sheet constituting the abutment opening of the closure is provided, this sealing member can be extended over its entire length. The contact surface can be brought into reliable contact with the vehicle over a period of time, thereby improving the sealing performance between the vehicle and the boarding bridge, and preventing the contact surface from wrinkling to improve its durability. You will be able to aim for

(実施例) 以下、本考案の実施例を図面に基づいて説明す
る。
(Example) Hereinafter, an example of the present invention will be described based on the drawings.

第1図にはボーデイングブリツジ1の全体構造
が示されている。すなわち、このボーデイングブ
リツジ1は、基部通路体2と中間通路体4と航空
機の機体に対する連結口3aを有する機体連結用
キヤブ3とが順に設けられてなる。上記基部通路
体2と中間通路体4とは基端側円形室5を介して
駆動手段(図示省略)により水平回動可能に連結
され、上記中間通路体4と機体連結用キヤブ3と
は先端側円形室6を介して同じく駆動手段(図示
省略)により水平回動可能に連結されている。そ
して、上記先端側円形室6には機体連結用キヤブ
3に対する連通口7を開閉するシヤツター8が設
けられている。
FIG. 1 shows the overall structure of a boarding bridge 1. As shown in FIG. That is, this boarding bridge 1 is provided with a base passage body 2, an intermediate passage body 4, and a fuselage connection cab 3 having a connection port 3a to the aircraft fuselage in this order. The base passage body 2 and the intermediate passage body 4 are horizontally rotatably connected by a driving means (not shown) via the base-side circular chamber 5, and the intermediate passage body 4 and the cab 3 for connecting the fuselage are connected at the tip. They are also horizontally rotatably connected via a side circular chamber 6 by a drive means (not shown). A shutter 8 for opening and closing the communication port 7 to the cab 3 for connecting the fuselage is provided in the circular chamber 6 on the distal end side.

上記基部通路体2は、空港ビルに連結されるも
ので、路上に支柱9にて支持されている。中間通
路体4は、内筒4aと外筒4bとを伸縮可能に嵌
合してなる。この場合、内筒4aは上記基端側円
形室5に対して上下動可能に連なり、外筒4bは
上下伸縮可能な走行脚10に支持されていて、上
記先端側円形室6に連なつている。そして、上記
機体連結用キヤブ3の機体への連結口3aの周縁
には、機体に当接せしめてこの機体連結用キヤブ
3と機体との間をシールするクロージヤ11が設
けられており、このクロージヤ11に上記シール
性を高めるための前方に突出した突条のシール部
材12が設けられている。
The base passage body 2 is connected to an airport building, and is supported on the road by pillars 9. The intermediate passage body 4 is formed by fitting an inner tube 4a and an outer tube 4b so that they can expand and contract. In this case, the inner cylinder 4a is vertically movably connected to the proximal circular chamber 5, and the outer cylinder 4b is supported by vertically extendable running legs 10, and is connected to the distal circular chamber 6. There is. A closure 11 is provided on the periphery of the connection port 3a of the aircraft connection cab 3 to the aircraft body, and is brought into contact with the aircraft body to seal between the aircraft connection cab 3 and the aircraft body. 11 is provided with a seal member 12 in the form of a protrusion protruding forward in order to improve the sealing performance.

すなわち、クロージヤ11は、上記連結口3a
の上縁及び左右の両側縁に設けられていて、第2
図に示す如く、前後方向に伸縮可能なベローズ状
になつている。そして、フロア13の前端を機体
Wの乗降口下縁に当接した状態で、クロージヤ1
1の機体Wへの当接口部11aを前方に倒し、機
体Wの乗降口の上縁及び両側縁に当接するように
なされている。
That is, the closure 11 is connected to the connection port 3a.
The second
As shown in the figure, it has a bellows shape that can be expanded and contracted in the front and rear directions. Then, with the front end of the floor 13 in contact with the lower edge of the entrance/exit of the aircraft W, the closure 1
The abutting port 11a for the body W of No. 1 is tilted forward so as to come into contact with the upper edge and both side edges of the entrance/exit of the body W.

しかして、上記クロージヤ11は、そのベロー
ズ部14が門型に成形したばね鋼による複数のフ
レームと、このフレームに被せたナイロン製ター
ポリンによるベローズカバー15とにより構成さ
れている。そして、上記機体Wへの当接口部11
aは、上記ターポリンによるカバーを設けた当接
体16と、この当接体16の当接面に設けた上述
のシール部材12とにより構成されている。
The closure 11 is comprised of a plurality of spring steel frames whose bellows portions 14 are formed into a gate shape, and a bellows cover 15 made of a nylon tarpaulin placed over the frames. Then, the abutment port 11 to the body W
A is composed of the abutting body 16 provided with the above-mentioned tarpaulin cover, and the above-mentioned sealing member 12 provided on the abutting surface of this abutting body 16.

上記ベローズカバー15は、第3図に示す如
く、上記機体連結用キヤブ3の連結口3aの角部
に当たる部分にこのカバー15を門型に折り曲げ
るための菱形孔17が形成されている。そして、
このベローズカバー15の端縁に上記当接体16
のカバー18が一体に連なつている。この当接体
カバー18にも門型に折り曲げるための三角形状
の切欠き19が形成されている。なお、上記菱形
孔17及び切欠き19は門型に折り曲げた状態で
はミシン掛けして塞がれるものである。
As shown in FIG. 3, the bellows cover 15 has a diamond-shaped hole 17 formed at a corner of the connecting port 3a of the cab 3 for connecting the aircraft body to allow the cover 15 to be bent into a gate shape. and,
The abutting body 16 is attached to the edge of this bellows cover 15.
The covers 18 are integrally connected. This abutting body cover 18 is also formed with a triangular notch 19 for bending into a gate shape. Note that the diamond-shaped hole 17 and the notch 19 are closed by sewing with a sewing machine in the state of being bent into a gate shape.

上記当接体16は、第4図に示す如く、上記当
接体カバー18にてウレタンフオームによるクツ
シヨン材20を覆つてなる。そして、この当接体
カバー18の表面(当接面)に上記シール部材1
に機体連結用キヤブ3の連結口3aの上縁から両
側縁の上部にわたつて、この連結口3aの縁に沿
つて設けられている。
As shown in FIG. 4, the abutting body 16 is formed by covering a cushion material 20 made of urethane foam with the abutting body cover 18. Then, the seal member 1 is placed on the surface (contact surface) of this contact body cover 18.
It is provided along the edge of the connection port 3a of the cab 3 for connecting the fuselage, extending from the upper edge of the connection port 3a to the upper portions of both side edges.

すなわち、このシール部材12は、ゴム製であ
つて、平板状の基部12aと、この基部12aの
幅方向の中央部に一体に設けられていて機体Wに
当接せしめる半円弧状の当て部12bとにより構
成された閉断面構造のものであり、上記当接体カ
バー18よりもその曲げ強度が高くなつている。
そして、上記基部12bの両側部が上記当接体カ
バー18にミシン掛けにより固定されている。こ
の場合、第5図に示す如く、上記シール部材12
は、上記連結口3aの上縁においては、その中央
から両側縁に向かつて下降傾斜して設けられてい
る。
That is, this sealing member 12 is made of rubber, and includes a flat base 12a and a semicircular arc-shaped abutting part 12b that is integrally provided at the center of the base 12a in the width direction and abuts against the body W. It has a closed cross-sectional structure, and its bending strength is higher than that of the abutting body cover 18.
Both sides of the base portion 12b are fixed to the abutting body cover 18 by sewing. In this case, as shown in FIG.
are provided at the upper edge of the connecting port 3a, slanting downward from the center toward both side edges.

従つて、上記構造のクロージヤ11において
は、ボーデイングブリツジ1を運転して機体Wの
乗降口の下縁に機体連結用キヤブ3のフロア13
に当接し、クロージヤ11の当接口部11aをベ
ローズ部14の伸縮を利用して前方に倒し、機体
Wの乗降口の上縁及び両側縁に当接せしめること
になる。この場合、連結口3aの上縁と両側縁の
上部においては、主として上記シール部材12が
当接し、上記両側縁の下部においては上記当接体
16が当接することになる。
Therefore, in the closure 11 having the above structure, the boarding bridge 1 is operated and the floor 13 of the cab 3 for connecting the fuselage is attached to the lower edge of the entrance/exit of the fuselage W.
The contact opening portion 11a of the closure 11 is brought forward by utilizing the expansion and contraction of the bellows portion 14, and brought into contact with the upper edge and both side edges of the entrance/exit of the aircraft body W. In this case, the seal member 12 mainly contacts the upper edge of the connecting port 3a and the upper portions of both side edges, and the contact body 16 contacts the lower portions of the both side edges.

そうして、シール部材12は当接体カバー18
よりも曲げ強度が高いから、それ自身にしわを生
じ難く、その全長にわたつて機体Wに確実に当接
して、この機体Wと機体連結用キヤブ3との間の
シール性を高めることになる。また、このシール
部材12は上記当接体カバー18の補強リブとし
て機能し、この当接体カバー18のしわ寄りを防
止してその外観を維持するとともに、その耐久性
の向上を図ることになる。
Then, the sealing member 12 is attached to the abutting body cover 18.
Since the bending strength is higher than that of the fuselage, it is difficult to wrinkle itself, and it reliably contacts the fuselage W over its entire length, improving the sealing performance between the fuselage W and the fuselage connection cab 3. . Furthermore, this sealing member 12 functions as a reinforcing rib for the abutting body cover 18, preventing the abutting body cover 18 from wrinkling, maintaining its appearance, and improving its durability. .

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

図面は本考案の実施例を示し、第1図はボーデ
イングブリツジの斜視図、第2図はクロージヤを
示す一部断面にした側面図、第3図はベローズ部
及び当接体のカバーとシール部材とを示す一部省
略した展開図、第4図はクロージヤの当接部の縦
断面図、第5図はクロージヤを示す一部省略した
正面図である。 1……ボーデイングブリツジ、3a……連結
口、11……クロージヤ、11a……当接口部、
12……シール部材、18……当接体カバー(防
水シート)、W……機体(乗り物)。
The drawings show an embodiment of the present invention, in which Fig. 1 is a perspective view of the boarding bridge, Fig. 2 is a partially sectional side view showing the closure, and Fig. 3 shows the bellows part and the cover of the abutting body. FIG. 4 is a longitudinal sectional view of the abutting portion of the closure, and FIG. 5 is a partially omitted front view showing the closure. 1... Boarding bridge, 3a... Connection port, 11... Closure, 11a... Contact port,
12... Seal member, 18... Contact body cover (waterproof sheet), W... Body (vehicle).

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] 乗り物への連結口の周縁に前後方向へ伸縮可能
なクロージヤが設けられ、このクロージヤの乗り
物への当接口部が防水シートにて構成されたボー
デイングブリツジにおいて、上記当接口部の少な
くとも上縁部分には前方に突出し且つこの当接口
部の縁に沿つて延び上記乗り物に当接せしめられ
る突条のシール部材が設けられていて、このシー
ル部材はその曲げ強度が上記防水シートよりも高
く設定されていることを特徴とするボーデイング
ブリツジのクロージヤ。
In a boarding bridge in which a closure that is expandable and retractable in the front and back direction is provided around the periphery of a connection port to the vehicle, and the contact port portion of the closure to the vehicle is made of a waterproof sheet, at least the upper edge of the contact port portion. The portion is provided with a sealing member having a protrusion that projects forward and extends along the edge of the abutment opening portion so as to come into contact with the vehicle, and the bending strength of this sealing member is set higher than that of the waterproof sheet. A boarding bridge closure characterized by:
JP1989018678U 1989-02-20 1989-02-20 Expired - Lifetime JPH059280Y2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP1989018678U JPH059280Y2 (en) 1989-02-20 1989-02-20

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP1989018678U JPH059280Y2 (en) 1989-02-20 1989-02-20

Publications (2)

Publication Number Publication Date
JPH02109799U JPH02109799U (en) 1990-09-03
JPH059280Y2 true JPH059280Y2 (en) 1993-03-08

Family

ID=31233539

Family Applications (1)

Application Number Title Priority Date Filing Date
JP1989018678U Expired - Lifetime JPH059280Y2 (en) 1989-02-20 1989-02-20

Country Status (1)

Country Link
JP (1) JPH059280Y2 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2014147656A1 (en) * 2013-03-18 2014-09-25 新明和工業株式会社 Aircraft aircraft boarding and deboarding connection apparatus

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6256400B2 (en) * 1980-02-19 1987-11-25 Hitachi Ltd

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0330240Y2 (en) * 1985-09-28 1991-06-26

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6256400B2 (en) * 1980-02-19 1987-11-25 Hitachi Ltd

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2014147656A1 (en) * 2013-03-18 2014-09-25 新明和工業株式会社 Aircraft aircraft boarding and deboarding connection apparatus
JP5736510B2 (en) * 2013-03-18 2015-06-17 新明和工業株式会社 Aircraft boarding / exiting connection device

Also Published As

Publication number Publication date
JPH02109799U (en) 1990-09-03

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