KR20170073359A - Boarding Bridges apparatus to protect the sensors - Google Patents

Boarding Bridges apparatus to protect the sensors Download PDF

Info

Publication number
KR20170073359A
KR20170073359A KR1020150182163A KR20150182163A KR20170073359A KR 20170073359 A KR20170073359 A KR 20170073359A KR 1020150182163 A KR1020150182163 A KR 1020150182163A KR 20150182163 A KR20150182163 A KR 20150182163A KR 20170073359 A KR20170073359 A KR 20170073359A
Authority
KR
South Korea
Prior art keywords
sensor
bumper
canopy
cap head
aircraft
Prior art date
Application number
KR1020150182163A
Other languages
Korean (ko)
Other versions
KR101775972B1 (en
Inventor
조승상
주현수
이종호
조정수
양광호
Original Assignee
한국공항공사
에이지이(주)
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 한국공항공사, 에이지이(주) filed Critical 한국공항공사
Priority to KR1020150182163A priority Critical patent/KR101775972B1/en
Publication of KR20170073359A publication Critical patent/KR20170073359A/en
Application granted granted Critical
Publication of KR101775972B1 publication Critical patent/KR101775972B1/en

Links

Images

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F1/00—Ground or aircraft-carrier-deck installations
    • B64F1/30—Ground or aircraft-carrier-deck installations for embarking or disembarking passengers
    • B64F1/305—Bridges extending between terminal building and aircraft, e.g. telescopic, vertically adjustable
    • E—FIXED CONSTRUCTIONS
    • E01—CONSTRUCTION OF ROADS, RAILWAYS, OR BRIDGES
    • E01D—CONSTRUCTION OF BRIDGES, ELEVATED ROADWAYS OR VIADUCTS; ASSEMBLY OF BRIDGES
    • E01D18/00—Bridges specially adapted for particular applications or functions not provided for elsewhere, e.g. aqueducts, bridges for supporting pipe-lines

Abstract

A boarding device for protecting an aircraft sensor is disclosed. The boarding device for protecting the sensor may be configured such that when the boarding cap head and the aircraft are in contact, a part of the bumper of the cap head and a part of the bottom of the canopy slide away from the aircraft body.

Description

BACKGROUND OF THE INVENTION 1. Field of the Invention [0001] The present invention relates to a boarding bridge apparatus,

BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a boarding device for protecting an aircraft sensor and more particularly to a boarding device for protecting a sensor capable of sliding a bumper of a cab head and a part of a protective pad .

A boarding pass is a device that connects passengers of an airport to the aircraft at the gate of an airport passenger terminal for safe boarding and transportation of the aircraft. It is generally connected to a rotunda, a rotunda, Possible moving tunnels, cabs connected to the end of the moving tunnel and in contact with the aircraft body.

However, there is a problem in that the cab of the boarding school impacts the sensor mounted on the outside of the aircraft when the bottom portion and the side surface of the passenger are in contact with the aircraft.

A pitot tube, which is a sensor that can measure the flight speed of an aircraft, is usually installed on the side of the front of the aircraft. When the boarding bridge is connected to the aircraft, the cap head is connected to the Pitot tube It is important to ensure that the same sensor device is not damaged.

However, there is a problem in that the cap head part of the boarding bridge maintaining a constant width has interference between the cap head part and the aircraft sensor device when the pitot tube is located near the aircraft door on some aircraft types.

It is very time consuming for a boarding passenger to see a boarding bridge on a certain aircraft type so that the cap head of the boarding bridge does not come into contact with the sensor device of the aircraft. Sometimes the cap head of the boarding bridge causes the sensor of the aircraft to fail, .

Therefore, it is urgent to develop a device that does not impact the sensor mounted inside the aircraft when the cab of the boarding school is in direct contact with the aircraft.

SUMMARY OF THE INVENTION It is an object of the present invention to provide a boarding passageway device for protecting a sensor of an aircraft from damage when a phytot tube, which is a sensor for measuring the speed of an aircraft, .

It is another object of the present invention to provide a boarding passageway protecting a sensor that can shorten the time required to mount a boarding passageway on an aircraft.

A boarding device for protecting the sensor according to the embodiments of the present invention will be described.

The boarding device for protecting the sensor may be configured such that when the boarding cap head and the aircraft are in contact, a part of the bumper of the cap head and a part of the bottom of the canopy slide away from the aircraft body.

According to one aspect, a part of the bumper of the cap head part and a part of the canopy bottom part can be operated by a driving part driven by at least one of a screw jack, a hydraulic piston, and a motor.

According to one aspect, the driving portion can be driven by the operation of the button portion that controls the movement of the cap head portion.

According to one aspect, the driver can be driven by a pre-positioning or auto-docking function operation that controls the position of the moving tunnel in the boarding console according to the pre-input value

According to one aspect, a cushion portion is provided on the outside of the canopy bottom portion, and the cushion portion can be provided on the canopy bottom portion facing the airplane.

A boarding device for protecting the sensor according to the embodiments of the present invention will be described.

The boarding device for protecting the sensor includes a first bumper fixed to a cap head connected to a boarding bridge, a second bumper provided at a lower end of the first bumper, a second bumper movably disposed at a lower end of the second bumper, The canopy bottom, the second bumper, or a portion of the canopy bottom to form a separation distance from the aircraft fuselage.

According to one aspect, the second bumper or canopy bottom can be moved in a sliding manner.

According to one aspect of the present invention, the driving part is connected to the fixed part, one side of the fixing part is connected to the second bumper and the canopy bottom part, and the other side is connected to the driving part. The second bumper and the canopy bottom portion can be configured to draw a separation distance from the aircraft body, while the shaft length of the driving portion is shortened.

According to one aspect, the driving portion can be driven by at least one of a screw jack, a hydraulic piston, and a motor.

According to one aspect, the driving portion can be driven by the operation of the button portion that controls the movement of the cap head portion. According to one aspect, the driving unit can be driven by pre-positioning or auto-docking function operation in which the position of the moving tunnel is controlled by the boarding console in accordance with the pre-input value.

According to one aspect of the present invention, the cushion part is provided on the outside of the canopy bottom part, the cushion part is provided on the canopy bottom part facing the aircraft, and the cushion part is made of an elastic material.

A boarding device for protecting the sensor according to the embodiments of the present invention will be described.

In order to reduce the interference with the pitot tube sensor unit mounted on the front part of the aircraft, a part of the bumper of the cap head and a part of the bottom part of the canopy slide when the pitot tube sensor unit is contacted with the aircraft, Can be configured to be spaced apart.

According to one aspect, a part of the bumper of the cap head part and a part of the canopy bottom part can be operated by a driving part driven by at least one of a screw jack, a hydraulic piston, and a motor.

According to one aspect, the driving portion can be driven by the operation of the button portion that controls the movement of the cap head portion.

According to one aspect of the present invention, a cushion part is provided on the outer side of the canopy bottom part, and the cushion part can be provided on the canopy bottom part facing the pitot tube sensor part.

According to one aspect, the driver can be driven by a pre-positioning or auto-docking function operation that controls the position of the moving tunnel in the boarding console according to the pre-input value

According to the present invention, there is no damage to the sensor device of the aircraft when the boarding bridge is concealed, so that it is possible to shorten the time required to connect the boarding bridge to the aircraft.

1 is a view of a boarding bridge according to an embodiment of the present invention.
2 is a view of a sensor unit mounted inside an aircraft body according to an embodiment of the present invention.
FIG. 3 is a view showing the flight bridge cap head of FIG. 1 and the aircraft being engaged. FIG.
4 is a block diagram illustrating a driving operation of a boarding passageway for protecting a sensor according to an embodiment of the present invention.
5 is a side view of a cap head according to an embodiment of the present invention.
Figure 6 is a view of the second bumper and canopy floor of Figure 5 being slid.
FIG. 7 is a block diagram showing an operation sequence of a boarding device for protecting a sensor according to the present invention. FIG.

Hereinafter, embodiments will be described in detail with reference to exemplary drawings. It should be noted that, in adding reference numerals to the constituent elements of the drawings, the same constituent elements are denoted by the same reference symbols as possible even if they are shown in different drawings. In the following description of the embodiments, detailed description of known functions and configurations incorporated herein will be omitted when it may make the best of an understanding clear.

In describing the components of the embodiment, terms such as first, second, A, B, (a), and (b) may be used. These terms are intended to distinguish the constituent elements from other constituent elements, and the terms do not limit the nature, order or order of the constituent elements. When a component is described as being "connected", "coupled", or "connected" to another component, the component may be directly connected or connected to the other component, Quot; may be "connected,""coupled," or "connected. &Quot;

1 is a view of a boarding bridge according to an embodiment of the present invention. Referring to FIG.

The boarding school (1) is a system for connecting a boarding gate of an airport passenger terminal and an aircraft (10) to a passenger using an airplane (10) A moving tunnel 2 connected to the rotunda or movable in the center direction, a console 5 capable of boarding operation and control, and a cap head part 100 connected to the end of the moving tunnel and in contact with the aircraft body And the cap head portion 100 may be constituted by a canopy 245 of the bumper portion 230.

FIG. 2 is a view of a sensor unit mounted inside an aircraft body according to an embodiment of the present invention. FIG. 3 is a view showing the aircraft cap interposed between the flight bridge cap head of FIG. 1, 5 is a side view of the cap head according to an embodiment of the present invention, FIG. 6 is a side view of the second bumper and the canopy floor of FIG. 5, Fig. Referring to FIG.

The Pitot tube capable of measuring the flight speed of the airplane 10 is generally installed on the side surface of the front surface of the aircraft 10 so that when the boarding bridge is connected to the aircraft 10, It is important to prevent damage to the sensor unit 11 such as the Pitot tube mounted on the body of the battery 10.

The bumper 230 and a part of the canopy on the bottom surface side of the boarding cap head unit 100 of the present invention may be configured to be slid so as to be separated from the other side.

A part of the bumper 230 and the canopy bottom 240 disposed on the bottom surface side of the passenger cap head 100 can be connected to the driving unit 260. By the operation of the driving unit 260, 230 and the canopy bottom 240 slide.

Here, the driving unit 260 may be a screw jack, a hydraulic piston, and a button unit 50 for operating the driving unit 260 may be provided inside the boarding passageway 1. The button portion 50 can be mounted at any position where operation is possible.

The driver determines whether the sensor unit 11 mounted on the airplane 10 is operated and when the button unit 50 is pressed before the airplane 10 is connected to the airplane 10, The second bumper 220 and the canopy bottom portion 240 provided at the lower end of the second bumper 220 are driven so that the second bumper 220 and the canopy bottom portion 240 move from the existing position to the pitot tube 220. [ To move away from the body of the aircraft 10 to which it is attached.

The present invention is not limited to the manual configuration in which the driver presses the button unit 50 located on the console 5 but the height of the boarding bridge 1 by operating the console 5 in advance according to the type of the aircraft 10 to be connected Automatic operation in conjunction with an auto-docking method in which a pre-positioning system to set up a car and a boarding pass (1) to be automatically operated to the vicinity of a door of the aircraft 10 can be performed.

The cap head unit 100 includes a first bumper 210 fixed to a side surface of the cap head unit 100, a second bumper 220 provided at a lower end of the first bumper 210, A canopy bottom part 240 provided with a cushion part 241, a driving part 260 and a fixing part 270 provided at the lower end of the bumper 220.

The first bumper 210 may be fixed to the side of the cap head 100 and the second bumper 220 may be configured to be movable from the position of the first bumper 210.

The second bumper 220 may be positioned at the bottom of the cap head 100 and the can bottom 240 may be provided at the bottom of the second bumper 220. The canopy bottom portion 240 may be formed in a U-shape and a cushion portion 241 may be provided on a side portion thereof. The cushion portion 241 may be made of an elastic material so that when the canopy bottom portion 240 moves back and forth in a sliding manner, the cushion portion 241 is configured to slide back and forth together with the canopy bottom portion 240 .

Here, the sliding movement means that when the aircraft 10 and the cap head 100 are brought into contact with each other, the second bumper 220, the canopy bottom portion 240 and the cushion portion 241 are separated from the aircraft body 10 And may be in a reverse form to move away.

The second bumper 220 and the canopy bottom 240 can be simultaneously moved and the fixing portion 270 is provided to connect the driving unit 260 to the second bumper 220 and the canopy bottom 240 .

One side of the fixing part 270 can be connected to the driving part 260 and the other side can be connected to the second bumper 220 and the canopy bottom part 240.

The securing portion 270 may be configured to guide the second bumper 220 and the canopy bottom 240 away from the aircraft 10 body. Here, the fixing portion 270 may be a sliding guide.

For example, the upper end of the fixing portion 270 is connected to the second bumper 220 by the bolts 280, and the central portion of the fixing portion 270 is connected to the driving portion 260 by the bolts 280 And the lower end of the fixing part 270 may be connected to the canopy bottom part 240 by bolts 280. [

The second bumper 220 and the canopy bottom 240 can be pulled while the distance of the moving part 271 is reduced according to the driving of the screw 260, A portion of the cap head portion 100 may be operated to move away from the aircraft 10.

The first guiding portion 272 and the second guiding portion 273 connected to the moving portion 271 are formed so that the length of the moving portion 271 connected to the axis of the driving portion 260 becomes shorter according to the operation of the driving portion 260, The second bumper 220 and the canopy bottom 240 can be configured to be pulled toward the driving unit 260 while being inclined.

This is because when the Pitot tube which is the sensor unit 11 for measuring the speed and the like is installed in the vicinity of the door of the aircraft 10 and the boarding bridge 1 is connected to the specific aircraft 10, A part of the surface is separated by a width of about 1 m and a width of about 20 cm so that it can be constructed to reduce the interference with the Pitot tube mounted on the body of the aircraft 10.

The cap head portion 100 contacting the body of the airplane 10 when the airplane 10 is contacted according to the operation of the button portion 50 moves the second bumper 220 and the canopy bottom portion 240 toward the airplane 10, Even if the cap head portion 100 is positioned near the entrance of the airplane 10, the space does not interfere with the Pitot tube, which is the sensor portion 11 of the airplane 10, It is possible to shorten the time required to connect the bridge to the aircraft 10 and to prevent a contact accident between the boarding bridge and the aircraft.

The driving unit 260 may be driven by a pre-positioning or an auto-docking function that controls the position of the moving tunnel in the boarding console according to the pre-input value.

FIG. 7 is a block diagram showing an operation sequence of a boarding device for protecting a sensor according to the present invention. FIG. Referring to FIG.

The pitot tubes for measuring the flight speed of the aircraft are installed on the front side of the aircraft. When the boarding bridge is connected to the aircraft (S310), the manager confirms whether the aircraft sensor protection required model is present (S320) (S340). In step S340, the controller controls the button unit to operate the button unit in step S340. In step S340, the controller controls the second bumper and the canopy bottom of the cap head unit And may be configured to retract from the aircraft body.

 On the other hand, if it is not the aircraft sensor protection required model, the second bumper and canopy bottom of the cap head portion may be configured to perform a fixed general mode of operation from the cap head portion (S360).

This is because, in the case of aircraft sensor protection required type, the cap head portion contacting the aircraft body at the time of aircraft connection is spaced apart from the aircraft body by the second bumper and the canopy bottom to form a space of about 20 cm-1 m, It is possible to shorten the time required for the boarding bridge to be connected to the aircraft because it does not interfere with the Pitot tube which is the sensor part of the aircraft.

Although the present invention has been described in connection with what is presently considered to be the most practical and preferred embodiment, it is to be understood that the invention is not limited to the disclosed embodiments. In addition, the present invention is not limited to the above-described embodiments, and various modifications and changes may be made thereto by those skilled in the art to which the present invention belongs. Therefore, the spirit of the present invention should not be construed as being limited to the above-described embodiments, and all of the equivalents or equivalents of the claims, as well as the following claims, are included in the scope of the present invention.

1: Boarding school 3: Rotunda
5: Console 10: Aircraft
11: sensor part 50: button part
100: cap head part 200: boarding device for protecting the sensor
230: bumper part 210: first bumper
220: second bumper 240: canopy bottom
241: Cushion part 260: Driving part
270: Fixing portion 280: Bolt

Claims (19)

Wherein a part of the bumper of the cap head part and a part of the bottom part of the canopy slide when the aircraft cap is connected with the cap head part to protect the sensor configured to be separated from the aircraft body. The method according to claim 1,
Wherein a part of the bumper of the cap head and a part of the bottom of the canopy protect a sensor operated by a driving part driven by at least one of a screw jack, a hydraulic piston, and a motor. 3. The method of claim 2,
And the driving unit protects the sensor driven by the operation of the button unit that controls the movement of the cap head unit. 3. The method of claim 2,
Wherein the driving unit protects the sensor that is automatically driven by operation of a console that controls movement of the cap head unit. The method according to claim 1,
Wherein a cushion portion is provided on an outer side of the canopy bottom portion, and the cushion portion protects a sensor provided on the canopy bottom portion facing the aircraft. A first bumper fixed to the cap head connected to the boarding bridge;
A second bumper provided at a lower end of the first bumper and movable;
A canopy bottom provided at a lower end of the second bumper and simultaneously moving with the second bumper;
A driver connected to the second bumper or a portion of the canopy bottom to form a separation distance from the aircraft body;
And a sensor for protecting the sensor. The method according to claim 6,
Wherein the second bumper or the bottom of the canopy protects the sensor moving in a sliding manner. The method according to claim 6,
Wherein the driving part is connected to the fixed part, one side of the fixing part is connected to the second bumper and the bottom part of the canopy, and the other side protects the sensor connected to the driving part. The method according to claim 6,
Wherein the moving part connected to the shaft of the driving part pulls the second bumper and the canopy bottom part while the shaft length of the driving part is shortened by the operation of the driving part so that the second bumper and the canopy bottom part A boarding device for protecting a sensor configured to form a separation distance. The method according to claim 6,
Wherein the driving unit protects a sensor driven by at least one of a screw jack, a hydraulic piston, and a motor. The method according to claim 6,
And the driving unit protects the sensor driven by the operation of the button unit that controls the movement of the cap head unit. The method according to claim 6,
Wherein the driving unit protects the sensor that is automatically driven by operation of a console that controls movement of the cap head unit. The method according to claim 6,
Wherein a cushion portion is provided on an outer side of the canopy bottom portion, and the cushion portion protects a sensor provided on the canopy bottom portion facing the aircraft. 14. The method of claim 13,
The cushion unit protects the sensor, which is an elastic material. A portion of the bumper of the cap head and a part of the bottom portion of the canopy slide so as to be spaced apart from the pitot tube sensor portion in order to reduce interference with the pitot tube sensor portion mounted on the front portion of the aircraft, Boarding device. 16. The method of claim 15,
Wherein a part of the bumper of the cap head and a part of the bottom of the canopy protect a sensor operated by a driving part driven by at least one of a screw jack, a hydraulic piston, and a motor. 17. The method of claim 16,
And the driving unit protects the sensor driven by the operation of the button unit that controls the movement of the cap head unit. 16. The method of claim 15,
Wherein the cushion unit includes a cushion unit on the outside of the canopy bottom part, and the cushion unit protects the sensor provided on the canopy bottom part facing the pythot tube sensor unit. 17. The method of claim 16,
Wherein the driving unit protects the sensor that is automatically driven by operation of a console that controls movement of the cap head unit.
KR1020150182163A 2015-12-18 2015-12-18 Boarding Bridges apparatus to protect the sensors KR101775972B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
KR1020150182163A KR101775972B1 (en) 2015-12-18 2015-12-18 Boarding Bridges apparatus to protect the sensors

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
KR1020150182163A KR101775972B1 (en) 2015-12-18 2015-12-18 Boarding Bridges apparatus to protect the sensors

Publications (2)

Publication Number Publication Date
KR20170073359A true KR20170073359A (en) 2017-06-28
KR101775972B1 KR101775972B1 (en) 2017-09-07

Family

ID=59280587

Family Applications (1)

Application Number Title Priority Date Filing Date
KR1020150182163A KR101775972B1 (en) 2015-12-18 2015-12-18 Boarding Bridges apparatus to protect the sensors

Country Status (1)

Country Link
KR (1) KR101775972B1 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109211301A (en) * 2018-09-21 2019-01-15 华德宝机械（昆山）有限公司 The abnormity diagnostic system and Aerobridge control system of sensor on a kind of connecting bridge

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6691361B2 (en) 2001-03-30 2004-02-17 Dew Engineering And Development Limited Extensible platform on an extensible passenger loading bridge
US6725488B2 (en) 2002-02-06 2004-04-27 Britt C. Hinkle Loading bridge control system and method
US6802096B2 (en) * 2002-06-14 2004-10-12 Dew Engineering And Development Limited Retractable floor assembly for a passenger loading bridge

Also Published As

Publication number Publication date
KR101775972B1 (en) 2017-09-07

Similar Documents

Publication Publication Date Title
CN106458514B (en) Elevator shaft dimension measuring device and measuring method thereof
KR101176491B1 (en) Working vehicle for monorail
EP2327630A2 (en) Boarding bridge with a minute approaching device and a shock absorbing part and operation method thereof
JP2006521234A (en) Slide step
KR20100011871A (en) Cable railway system
CN105946882A (en) Self-adaptive telescopic footboard device for train platform
JP6001128B1 (en) Train arrival and departure control system, on-board equipment and ground equipment
CN110696841A (en) Railway track train and train door entrance step structure thereof
KR102513737B1 (en) Bogie for car crash test and car crash simulator
AU2017213560A1 (en) Intelligent step for BRT platform
CN107867408A (en) Couple the bottom plate of module
US20100251617A1 (en) Open/close device for pit cover
KR101775972B1 (en) Boarding Bridges apparatus to protect the sensors
US6725488B2 (en) Loading bridge control system and method
WO2018096773A1 (en) Passenger boarding bridge
JP4324605B2 (en) Boarding bridge
KR101762737B1 (en) Stopper apparatus for train stops at the correct position
CN209739381U (en) passenger boarding vehicle with automatic telescopic sliding door
ITMI20121549A1 (en) METHOD OF CONTROL OF A ROPE TRANSPORTATION SYSTEM AND ROPE TRANSPORT SYSTEM
CN107499294B (en) Control method, system and the vehicle of vehicle
JP2021049973A (en) Boarding bridge
CN113682490B (en) Autonomous stopping device, control method thereof, machine receiving platform and aviation food vehicle
KR20050009439A (en) Safety landing apparatus for airplane
JP2013124024A (en) Vehicle for airport
US11932289B2 (en) External sliding threshold assembly for vehicle doors

Legal Events

Date Code Title Description
A201 Request for examination
E902 Notification of reason for refusal
AMND Amendment
E601 Decision to refuse application
AMND Amendment
X701 Decision to grant (after re-examination)
GRNT Written decision to grant