CN103085988B - Connecting channel - Google Patents
Connecting channel Download PDFInfo
- Publication number
- CN103085988B CN103085988B CN201210484588.3A CN201210484588A CN103085988B CN 103085988 B CN103085988 B CN 103085988B CN 201210484588 A CN201210484588 A CN 201210484588A CN 103085988 B CN103085988 B CN 103085988B
- Authority
- CN
- China
- Prior art keywords
- frame
- flexible frame
- flexible
- actuator
- stereoplasm
- 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.)
- Active
Links
Landscapes
- Tents Or Canopies (AREA)
- Power-Operated Mechanisms For Wings (AREA)
Abstract
The invention provides a connecting channel. The connecting channel comprises a telescopic bridge body channel and an awning device, wherein the awning device comprises a door-shaped frame and a docking frame; the docking frame comprises a hard frame and a flexible frame; retraction mechanisms and an energy storage device are connected between the door-shaped frame and the hard frame; the hard frame and the flexible frame are respectively hinged to a non-telescopic floor; the flexible frame is hinged to the front end of the floor, and two side ends of the front end of the floor and two side branches of the flexible frame are respectively provided with distance measuring instruments; a plurality of actuators are connected between the hard frame and the flexible frame; and hinged joints of the actuators on each side branch of the flexible frame and mounting points of the distance measuring instruments are vertically crosswise arranged. By a boarding bridge provided by the invention, the tightness and the security are improved.
Description
Technical field
The present invention relates to a kind of interface channel, be specifically related to a kind of connecting bridge comprising awning device, particularly relate to a kind of be included in dock with aircraft before just can have the connecting bridge of the docking framework of the profile of coincideing with aircraft surfaces radian adaptively.
Background technology
Boarding bridge is the airfield equipment that a modern passenger aircraft usually uses, and they are used as the entrance of boarding, can enter passenger plane inside for passenger from terminal.This connecting bridge all has an awning device in its end usually, and it is connected across in the space between connecting bridge and aircraft, thus boarding personnel can be protected not to be subject to the impact of adverse weather condition.
Patent documentation CN100355628C discloses a kind of birdman's gangway or boarding bridge sealing arrangement, comprise one and be stretched in vestibule diaphragm above a connection floor, wherein said vestibule diaphragm has a flexible frame on one open end, be arranged at its other end place on a door-shaped frame be used for fixing on birdman's gangway or boarding bridge, wherein said flexible frame is fitted on airplane skin when described vestibule diaphragm stretches out, and be wherein provided with one for the operating control of described vestibule diaphragm, to launch or to close up described vestibule diaphragm, wherein said operating control comprises wind2 and by energy storage equipment, the brake ac-tuating mechanism that multi link is formed.Patent documentation CN100528688C discloses a kind of shelter device, for the connecting bridge of aircraft, comprises flexible frame, is arranged on an open end of this shelter device, for fitting to the shell of this aircraft when this shelter device launches; Door-shaped frame, is arranged on another open end of this awning device, for being connected to this connecting bridge; Extensible folding paulin, be connected across between this flexible frame and this door-shaped frame, and be connected to top and the both sides of this flexible cross-over connection and this door-shaped frame, also comprise at least two steering units independent of each other, for driving this shelter device launch and/or close up, described steering unit is made up of wind2 and single energy storage equipment.Patent documentation CN101910001A discloses a kind of kiss connection device for portable connecting bridge, comprising: charging portion, and it is attached to the end of the shelter of described portable connecting bridge and can injects air; And padded coaming, it is arranged in described charging portion, even and if described padded coaming still keeps solid shape when discharging air from described charging portion.Patent documentation US5267368A discloses a kind of boarding bridge awning device, and it uses actuator to promote collapsible docking framework and realizes and the docking of aircraft door.
Therefore can find out, prior art all have employed energy storage equipment usually when realizing awning device and docking with fuselage, and such as gas spring etc. and wind2 are with the use of, or hydraulic actuator, and document CN100355628C also uses multiple connecting rod or cantilever design; And in order to make docking framework fit tightly fuselage as far as possible, and the injury that minimizing awning device may cause for aircraft fuselage cover, adopt flexible frame more than docking framework of the prior art, especially document CN101910001A also adopts the gas filled device with padded coaming.But, the difference each other of aircraft is now all comparatively large, and the Curvature varying of its outline is also all comparatively large, particularly sometimes also there is very large bent angle in prow transitional region, make existing boarding bridge awning device be difficult to accurately fit on airplane skin, and then retain gap.These gaps are totally unfavorable under severe conditions, particularly sleety weather, are easy to cause moisture enter interior of aircraft or drench passenger, also may cause wet and slippery risk at connecting bridge or fuselage interior.By energy storage equipment or actuator in aforementioned documents, such as gas spring, hydraulic actuator promote the top of docking flexible frame, awning device is made to fit to fuselage cover, due in such cases, docking framework passive is pushed on fuselage, actuating structure is comparatively complicated on the one hand, and flexible frame is when in the face of multiple curvature thereof on the other hand, is usually also difficult to very closely fit on fuselage cover.Moreover in order to realize fitting tightly, gas spring, hydraulic actuator generally also need to provide comparatively high thrust, therefore unavoidable fuselage cover to be caused damage.
Document CN202379091U discloses a kind of boarding bridge pickup range finding sensing device, comprise the buffering sebific duct being arranged on front edge of airport pickup port end, described buffering sebific duct is provided with range finding sensing device, the side of described buffering sebific duct has exploration hole, and the sensor probe of described range finding sensing device and described exploration hole are just to setting.It is mainly used in the deformation extent reacting buffering sebific duct, and notice control system sends speed-slackening signal in time, prevents from causing greater impact to fuselage.But the deployed configuration that it adopts still belongs to conventional prior art, and it also cannot solve the problem.Document CN101287649B disclose a kind of by connecting bridge automatic butt to the method on hatch door, it adopts laser rangefinder and Computer Control Unit to realize the automatic butt of connecting bridge and aircraft door.Above-mentioned two sections of documents are still more single for the using method of laser rangefinder.
Therefore, column defects under connecting bridge ubiquity of the prior art: due to energy storage equipment or the actuator point of application single, flexible frame is difficult to adapt to various aircraft surfaces curvature, and alerting ability and leak tightness are all poor; And in order to fuselage cover that flexible frame is closely fitted, the power of usual applying is all larger, easy infringement fuselage cover, in addition because energy storage equipment or actuator are just started working usually after awning device touches fuselage cover, therefore easily because faults itself or system error cause overload, heavy damage fuselage cover; Lack passenger's boarding process to detect in real time and alarm device, there is potential safety hazard.
Summary of the invention
In order to overcome the problems referred to above, the invention provides a kind of connecting bridge comprising awning device, particularly relate to a kind of be included in dock with aircraft before just can have the connecting bridge of the docking framework of the profile of coincideing with aircraft surfaces radian adaptively.Connecting bridge comprises scalable bridge body passageway and awning device, described awning device comprises door-shaped frame and docking framework, described docking framework comprises stereoplasm frame and flexible frame, jack and energy storage equipment is connected with between door-shaped frame and stereoplasm frame, stereoplasm frame and flexible frame are articulated with non-telescoping floor respectively, wherein flexible frame is articulated with ground front edge of board, and two, floor layer front end side end and flexible frame both sides branch are also respectively arranged with apomecometer; Be connected with multiple actuator between stereoplasm frame and flexible frame, the actuator hinge-point in the every side branch of flexible frame and apomecometer attachment point in the vertical direction should interlock and come.
Preferably, flexible frame is made up of plastic material.
Preferably, described apomecometer is laser rangefinder or ultrasonic range finder, infrared ambulator.
Preferably, awning is connected with between stereoplasm frame and flexible frame and between stereoplasm frame and door-shaped frame.
Preferably, the controller receiving apomecometer signal and control actuator is also comprised.
Connecting bridge tool according to the present invention has the following advantages: (1) multiple apomecometer and actuator carry out yielding flexibility framework because the present invention utilizes, therefore, it is possible to adapt to various different aircraft surfaces curvature well, and can possess good leak tightness; (2) because docking framework of the present invention completed distortion before touching fuselage cover, therefore, it is possible to prevent actuator from transshipping due to faults itself or system error; (3) distance measuring sensor of the present invention can detect docking situation in real time, and gives the alarm, therefore safer.
Accompanying drawing explanation
Fig. 1 partially show the longitdinal cross-section diagram according to connecting bridge of the present invention.
Fig. 2 schematically simulates the mode of texturing of the flexible frame of the awning device in the present invention.
Detailed description of the invention
With reference to accompanying drawing 1, it partially show according to connecting bridge of the present invention, and the connecting bridge in the present invention is a kind of retractable boarding bridge comprising roller.It comprises bridge body passageway and awning device 1, and this awning device 1 comprises door-shaped frame 2 and docking framework 3, and docking framework 3 is directly used in and realizes docking of awning device 1 and aircraft fuselage cover.The flexible frame 5 that docking framework 3 comprises stereoplasm frame 4 and directly will contact with fuselage cover, flexible frame 5 is made up of flexible material, but the ductility of this material is poor, such as plastics.Flexible frame surrounding also can comprise padded coaming, inflatable packer or elastic variable pipe etc. further.Door-shaped frame 2 is fixedly connected on floor layer 6.Described floor layer is the non-telescoping formula flaggy regularly that cannot change shape.Stereoplasm frame 4 is articulated with the floor layer 6 of awning device 1 pivotally, and uses energy storage equipment between door-shaped frame 2 and stereoplasm frame 6 and reclaim winding mechanism 8, and energy storage equipment can be such as gas spring 7.Flexible frame can be articulated with the front end on floor, but selects as a kind of, also can be fixedly installed on floor.In order to be added to open area, preferably, stereoplasm frame 4 and flexible frame also can be arranged on the lateral surface of floor layer.On each side, multiple actuator is connected with (in order to various fuselage surface curvature can be adapted between stereoplasm frame 4 and flexible frame 5, can accept in scope at cost, the quantity of actuator is preferably The more the better), such as hydraulic actuator 9, considers for simplification, in the present embodiment, the number of hydraulic actuator is three, and on even keel is arranged between stereoplasm frame 4 and flexible frame 5 respectively.These three actuators are preferably distributed on every side of flexible frame dispersedly, but the preferably the rarest top being arranged on every side branch of flexible frame in multiple actuator, be beneficial to the laminating of flexible frame and fuselage cover.Actuator one end and flexible frame 5 carry out hinged, and the other end is then hinged with stereoplasm frame 4.Two, floor layer front end side end (floor and flexible frame hinge-point below) and flexible frame 5 both sides branch are also respectively arranged with distance measuring sensor 10, this apomecometer can be such as ultrasonic range finder, infrared ambulator or laser rangefinder, prioritizing selection laser rangefinder in the present embodiment.The installation of apomecometer on flexible frame can adopt well-known conventional means, the form of support such as can be adopted to be arranged on flexible frame, and this laser rangefinder also can be arranged among the perforate on flexible frame 5, apomecometer can deflect along with flexible frame flexural deformation.Apomecometer quantity on flexible frame can identical from actuator quantity also can be different.The set laser rangefinder of floor layer front end can be arranged in the boring of floor layer front end.In an initial condition, distance measuring sensor 10 in the vertical direction that floor layer front end and flexible frame 5 are arranged should be alignment, and that is they should be arranged on same vertical straight line.Certainly, for the object of protection apomecometer, their edges slightly should retreat the edge in flexible frame or floor layer front end, can not cause shock like this when docking to apomecometer.Apomecometer in each branch of flexible frame is crisscross arranged relative to actuator, specifically, apomecometer should be tried one's best and is arranged at dispersedly on flexible frame, but should avoid being in very near the hinge-point of actuator on flexible frame, this use for apomecometer is very favourable, therefore described hinge-point often suffers stress, this is unsafe for apomecometer, consider it is also favourable from installing space in addition, simultaneously because they stagger installation, the infringement therefore for flexible frame is also less.The periphery in stereoplasm frame, space between flexible frame and door-shaped frame is equipped with awning.Awning device 1 also comprises the controller (not shown) being arranged on door-shaped frame 3 upper back, for receiving the signal and the operation of hydraulic control actuator 9 and winding mechanism 8 that laser rangefinder obtains, going back controller in addition and also controlling a warning device.Therefore this controller can have following function: when causing connecting bridge to tremble relative to airplane skin due to passenger's boarding, and then the warning passenger that gives the alarm when causing connecting bridge docking framework to depart from fuselage cover larger distance (being such as 10 centimetres) postpones action, and laser rangefinder again starts wind2 release energy storage equipment or primer fluid hydraulic actuator, until can measure distance reenter safe range (sounding all clear).
Introduce the method for operating of the awning device 1 in the present invention below in detail.
First, before awning device contacts with fuselage cover, the initial stage is used at connecting bridge, the laser rangefinder opened on awning device measures the distance of flexible frame distance airframe, connecting bridge vertically retractable aircraft advance (two apomecometers being arranged at floor layer leading section can be utilized, if their two distances measured are equal, connecting bridge just vertically aircraft advance is described), and when close to the aircraft certain distance that will dock, this distance is (because aircraft surfaces is arc line shaped, therefore the data of each laser rangefinder measurement are different, distance herein can be any one in laser rangefinder data of measuring) when can be arbitrary set point value between 0.5-5 rice, preferably 1 meter, temporary transient stopping connecting bridge is near the motion of aircraft, controller controls each actuator according to the distance value that each laser rangefinder measures and carries out respective stretching with yielding flexibility framework.Concrete operation method is as follows:
With reference to accompanying drawing 2, it schematically simulates the mode of texturing of the flexible frame of the awning device in the present invention.First utilizing the distance of the distance fuselage measured by the apomecometer on flexible frame and floor layer, generating the fuselage cover surface radian that will dock via controller simulation, as marked shown in 101; Because the flexible frame in the present invention is articulated with fixed type floor, therefore flexible frame position bottom remains unchanged after deformation, therefore according to the above-mentioned radian calculated, flexible frame after known distortion divides and prevaricates as marked as shown in 102 (translation radian 101, and in conjunction with flexible frame longitudinally height can draw); Because the stereoplasm frame 106 of simulation keeps motionless, and the hinge-point position of actuator on flexible frame is fixed, and flexible frame longitudinally extends negligible, and associated extension or the retracted length of the actuator therefore after distortion just can calculate.And then controller according to aforementioned calculated amount activate hydraulic actuator of the present invention can realize the flexible frame after being out of shape can have with will in conjunction with the identical radian of fuselage cover.Mark 103,104,105 in this figure flexible frame respectively in representative simulation, flexible after actuator and the actuator of initial position.In addition, in order to the distortion of flexible frame more accurately can be guaranteed, the present invention can also arrange auxiliary actuator (not shown) between actuator and stereoplasm frame, because the deflection angle of simulation actuator 104 in frame deformation process can calculate according to the method described above, auxiliary actuator therefore can be used according to calculated angle to deflect the actuator between flexible frame and stereoplasm frame.Described computation process can be completed by controller, and relevant mathematic calculation is all the common practise in affiliated field.
In this process, framework both sides independently operate, that is the distortion of flexible frame both sides can be different when needed, and this is for being very favorable during the corner that the appearance of hatch door periphery is larger, and therefore the present invention has very outstanding alerting ability in docking operation.And the actuator in the present invention just completed actuating before docking, therefore overload can not be there is due to the fault of self or because of control system error.
After this, namely continue to control connecting bridge to advance, and (the laser rangefinder measuring distance of stronghold front edge of board and comparing of anticipated value when moving closer to airframe, described anticipated value is relevant relative to the installation site at flexible frame edge with apomecometer) slow down connecting bridge speed of advance, until (the laser rangefinder measuring distance of stronghold front edge of board and comparing of anticipated value) brakes connecting bridge when flexible frame fits in fuselage cover.
Then controller controls winding mechanism release energy storage equipment, make it that docking framework is closely pressed on fuselage cover, because the flexible frame in the present invention is by actuator-operated distortion, therefore the energy storage equipment in the present invention, without the need to applying larger thrust in the prior art, therefore also just reduces the risk that awning device damages fuselage cover.
In passenger's boarding process, because the weight extruding of external conditions or passenger causes awning device relative to fuselage cover generation deflection or disengaging, because laser rangefinder can measure the change of distance, if therefore the distance of flexible frame and fuselage cover reaches a predetermined threshold (being such as 10 centimetres), controller can control warning device accordingly and give the alarm, and again start wind2 release energy storage equipment or primer fluid hydraulic actuator, until laser rangefinder can measure distance reenter safe range, sound all clear.
Because the engagement frame in the present invention was just provided with the surperficial radian of fuselage cover before laminating fuselage cover, therefore, it is possible to improve sealing property, reduce the hurtful risk of fuselage skin simultaneously.Also there is alarm in addition and again revise the advantage of laminating degree.What below do not elaborate is all the common practise in affiliated field.
Those skilled in the art can make replacement or modification according to content disclosed by the invention and the art technology grasped to content of the present invention; but these replacements or modification should not be considered as disengaging the present invention design, and these replacements or modification are all in the interest field of application claims protection.
Claims (4)
1. one kind comprises the connecting bridge of awning device, comprise scalable bridge body passageway and awning device (1), it is characterized in that awning device comprises door-shaped frame (2) and docking framework (3), described docking framework (3) comprises stereoplasm frame (4) and flexible frame (5), jack (8) and energy storage equipment (7) is connected with between door-shaped frame (2) and stereoplasm frame (4), stereoplasm frame (4) and flexible frame (5) are articulated with non-telescoping floor (6) respectively, wherein flexible frame (5) is articulated with floor (6) front end, two, floor layer front end side end and flexible frame (5) both sides branch are also respectively arranged with laser rangefinder (10), be connected with multiple actuator (9) between stereoplasm frame (4) and flexible frame (5), the actuator hinge-point in the every side branch of flexible frame and laser rangefinder attachment point in the vertical direction should interlock and come, when close to the aircraft certain distance that will dock, the distance value measured according to each laser rangefinder controls each actuator and carries out respective flexible with yielding flexibility framework, the flexible frame realized after distortion can have with will in conjunction with the identical radian of fuselage cover.
2. connecting bridge according to claim 1, is characterized in that flexible frame is made up of plastic material.
3. connecting bridge according to claim 1 and 2, is characterized in that being connected with awning between stereoplasm frame (4) and flexible frame (5) and between stereoplasm frame (4) and door-shaped frame (2).
4. connecting bridge according to claim 1, characterized by further comprising the controller receiving laser rangefinder signal and control actuator (9).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201210484588.3A CN103085988B (en) | 2012-11-23 | 2012-11-23 | Connecting channel |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201210484588.3A CN103085988B (en) | 2012-11-23 | 2012-11-23 | Connecting channel |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN103085988A CN103085988A (en) | 2013-05-08 |
| CN103085988B true CN103085988B (en) | 2015-02-18 |
Family
ID=48199213
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201210484588.3A Active CN103085988B (en) | 2012-11-23 | 2012-11-23 | Connecting channel |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN103085988B (en) |
Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3484883A (en) * | 1966-12-20 | 1969-12-23 | Aviolanda Maatschappij | End structure for airport gangways |
| US5257431A (en) * | 1990-08-15 | 1993-11-02 | Bridgetech, Inc. | Airplane loading bridge |
Family Cites Families (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| SE515352C2 (en) * | 1999-11-09 | 2001-07-16 | Fmt Int Trade Ab | Coupling device for a passenger bridge |
-
2012
- 2012-11-23 CN CN201210484588.3A patent/CN103085988B/en active Active
Patent Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3484883A (en) * | 1966-12-20 | 1969-12-23 | Aviolanda Maatschappij | End structure for airport gangways |
| US5257431A (en) * | 1990-08-15 | 1993-11-02 | Bridgetech, Inc. | Airplane loading bridge |
Also Published As
| Publication number | Publication date |
|---|---|
| CN103085988A (en) | 2013-05-08 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN102991705B (en) | End element for abutting joint of sealing device | |
| CN102963542B (en) | Passageway for passenger to pass through | |
| CN102963538B (en) | Butting method for bridge type channel | |
| CN102991714B (en) | Method for manipulating connecting channel | |
| CN103407577B (en) | Intermediate equipment for transporting passengers | |
| CN103085986B (en) | Deformable assembly | |
| CN102991708B (en) | Erecting method of boarding bridge | |
| CN102991703B (en) | Method for docking bridge type channel | |
| CN102991722B (en) | A kind of Passenger pathway manipulation method | |
| CN102991723B (en) | Aerobridge manipulation method | |
| CN103010480B (en) | Awning device unfolding method | |
| CN102963541B (en) | Butting method for sealing device | |
| CN103085988B (en) | Connecting channel | |
| CN102991704B (en) | Abutting joint method of transporting device | |
| CN103253377B (en) | Method for curved docking with airplanes | |
| CN102991717B (en) | Aerobridge with sealing device | |
| CN102963537B (en) | Abutting joint frame for awning device | |
| CN102991711B (en) | Boarding channel | |
| CN102991696B (en) | Closed docking framework | |
| CN102991695B (en) | A kind of method of operating of connecting bridge | |
| CN102991702B (en) | Method for stretching folding shed | |
| CN103144776B (en) | Sealing device for docking | |
| CN103144778B (en) | Bendable element | |
| CN102991710B (en) | Rain shelter device | |
| CN102975863B (en) | Folding tent for boarding bridge |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant |