KR102579703B1 - Aircraft direct connection transfer elevator device - Google Patents

Abstract

Existing aircraft transfers require a waiting time of at least 1 hour from disembarkation at a transit airport to boarding another aircraft to only 10 hours or more for a cheap airline ticket, and the distance traveled when passengers board another aircraft at a transit airport is Because it is often far away, it takes a lot of time to transfer, and passengers' baggage and delivery cargo also have to go through procedures such as disembarking at the airport, moving it, and transferring it to another aircraft, which requires a large number of workers and connects the aircraft to the airport. When disembarking and transferring to a transit aircraft, the boarding bridge must be connected to the aircraft twice, which takes a lot of time to connect, and when passengers transfer, it is necessary to connect the boarding bridge in case of rain, strong winds such as a typhoon, or hail. There are inconveniences such as using an umbrella due to exposure to external weather conditions such as falling teeth, and it is difficult to escape from danger due to natural disasters, wars between countries, or civil wars due to airport closures due to natural disasters, wars between countries, or civil wars, as it is directly connected to the airport passageway. In order to improve the problems that arise in situations where the aircraft is directly connected, a transfer elevator and an elevator electric car are configured to protect against external weather conditions such as rain, wind and rain such as a typhoon, or falling snow or hail when transferring at a transit airport. Instead of connecting the aircraft and the airport boarding bridge without any restrictions, the transfer of aircraft is made by directly connecting two aircraft, so it is possible to transfer aircraft without using the airport boarding gate, and passengers are protected from the external environment. The purpose is to provide transfer elevators and elevator electric cars directly connected to aircraft that can safely transfer without exposure and shorten the transfer time to minimize the waiting time required for transfer.

Description

Aircraft direct connection transfer elevator device {AIRCRAFT DIRECT CONNECTION TRANSFER ELEVATOR DEVICE}

The present invention relates to an aircraft direct connection transfer elevator device that matches the doors of large aircraft and small aircraft and connects each door to each other, allowing passengers to safely and quickly transfer aircraft without passing through the airport gate. .

Aircraft can only travel on designated routes depending on the air route, so if there is no air route for the passenger to arrive at the airport they are using, they must transfer aircraft.

However, existing aircraft transfers had the problem that the waiting time from disembarking at a transit airport to boarding another aircraft ranged from at least 1 hour to only 10 hours or more for cheap airline tickets.

In addition, when a passenger boards another aircraft at a transit airport, the travel distance is often long, so it takes a lot of time to transfer, and the baggage and delivery cargo carried by the passenger is also transferred after disembarking at the airport and then transferred to another aircraft. There was a problem that many workers were required to go through the loading procedure.

In addition, when connecting and disembarking from an aircraft to an airport, and when transferring to a transit aircraft, the boarding bridge must be connected to the aircraft twice, resulting in a lot of time required to connect the boarding bridge, and when passengers are transferring, they are exposed to rain, typhoons, and other weather conditions. At the same time, there was inconvenience in using an umbrella due to exposure to external weather conditions such as strong wind or falling hail.

In addition, existing aircraft were connected directly to the airport passageway when transferring, so there was a problem in that the airport was closed due to natural disasters, wars between countries, or civil wars, and the air route was blocked, making it difficult to escape from danger.

Republic of Korea Patent Publication No. 10-1369328 (registered on February 25, 2014)

In order to solve the above problem, in the present invention, instead of connecting the aircraft and the airport boarding bridge, regardless of the external weather environment such as rain, wind and rain such as a typhoon, or falling snow or hail when transferring at a transit airport, By connecting two aircraft directly to transfer aircraft, it is possible to transfer aircraft without using the airport boarding gate, passengers can transfer safely without being exposed to the external environment, and transfer time is shortened. The purpose is to minimize the waiting time required for transfer and to provide a transfer elevator device that directly connects two aircraft in the event of an airport closure due to a natural disaster, war between countries, or civil war.

In order to achieve the above object, the aircraft direct connection transfer elevator device according to the present invention is

In the shape of a large crane car, one aircraft fuselage is aligned at a certain angle and position, then raised and moved to place it in a vertically parallel structure with another aircraft fuselage, and then the doors and elevators of each aircraft fuselage are connected to raise and lower the two aircraft fuselages. This is achieved by constructing an aircraft direct connection transfer elevator device that connects boarding gates between aircraft.

As described above, in the present invention, when transferring at a transit airport, two aircraft are directly connected regardless of external weather conditions such as rain, wind and rain such as a typhoon, snow or hail, etc., so that the aircraft can be connected within the aircraft. By allowing transfers to take place at the airport, it is possible to transfer aircraft without using the airport's boarding gate, transfers are made safely without passengers being exposed to the external environment, and the transfer time due to transit through the aircraft is dramatically shortened, eliminating the need for transfers. It has the good effect of minimizing waiting time and allowing direct connection of two aircraft in case of airport closure due to natural disaster, war between countries, or civil war.

1 is a block diagram showing the configuration of an aircraft direct connection transfer elevator device according to the present invention;
Figure 2 is a perspective view showing the overall shape of the aircraft directly connected elevator electric car according to the present invention;
Figure 3 is a side view showing the overall shape of the aircraft directly connected elevator electric car according to the present invention;
Figure 4 is a front view showing the overall shape of the aircraft direct-connected elevator electric car according to the present invention, and a projection of the lower aircraft elevator unit formed inside the lower aircraft;
Figure 5 is a front view showing the overall shape of the elevator electric car directly connected to the aircraft according to the present invention, with the upper canopy docked at the bottom of the upper aircraft and the lower canopy docked at the top of the lower aircraft;
Figure 6 shows the overall shape of the elevator electric car directly connected to the aircraft according to the present invention from the front, where the upper canopy is docked at the bottom of the upper aircraft, the lower canopy is docked at the top of the lower aircraft, and the elevator car of the lower aircraft elevator part is operated by hydraulic pressure. A front view showing the projection of the state in which the upper aircraft has reached the lift-off barrier by ascending through the cylinder,
Figure 7 is a perspective view showing the overall shape of the aircraft lifting and lowering support frame according to the present invention;
Figure 8 is a perspective view showing the overall shape of the aircraft lifting support frame according to the present invention, and arrows indicate that the aircraft support frame is moved in the forward and backward directions along the longitudinal direction of the top of the slide support frame part;
Figure 9 is a perspective view showing a shape in which the upper aircraft and the lower aircraft according to the present invention are located in a vertically parallel structure, and the upper canopy and the lower canopy are spread around the position where the elevator car moves in the vertical direction;
Figure 10 shows an embodiment in which the elevating and lowering cylinder part according to the present invention is laid backward, the slide support frame part and the aircraft support frame are positioned at the lowest level, and the upper aircraft is moved to the top of the aircraft support frame, and the platform inside the upper aircraft is shown. A perspective view projected by
Figure 11 shows an embodiment of raising the upper aircraft by erecting and raising the elevating and lowering cylinder part according to the present invention, and moving the lower aircraft to the bottom of the upper aircraft, and shows a projection of the platform and elevator car inside the lower aircraft, An enlarged perspective view showing an embodiment in which an elevator car is raised,
Figure 12 is a block diagram showing the components of the integrated smart control unit according to the present invention;
Figure 13 is a perspective view showing the overall shape of the aircraft externally connected elevator electric car according to the present invention;
Figure 14 is a side view showing the overall shape of the aircraft external connected elevator electric car according to the present invention,
Figure 15 is a front view showing the overall shape of the aircraft external connected elevator electric car according to the present invention from the front, with the elevator unit coupled to the left side of the aircraft lifting support frame, and showing the interior of the elevator unit projected;
Figure 16 shows the overall shape of the elevator electric car connected to the outside of the aircraft according to the present invention from the front, where the upper boarding bridge is docked on the left side of the upper aircraft, the lower boarding bridge is docked on the left side of the lower aircraft, and the elevator car of the elevator unit is at the height of the upper boarding bridge. A front view showing a projection of a stationary shape positioned to coincide with
Figure 17 shows the overall shape of the elevator electric car connected to the outside of the aircraft according to the present invention from the front, where the upper boarding bridge is docked on the left side of the upper aircraft, the lower boarding bridge is docked on the left side of the lower aircraft, and the elevator car of the elevator unit is connected to the lower boarding bridge. A front view showing a projection of a stationary shape positioned to match the height,
Figure 18 is a perspective view showing the overall shape of the aircraft lifting and lowering support frame according to the present invention;
Figure 19 is a perspective view showing the overall shape of the aircraft lifting support frame according to the present invention, with arrows indicating that the aircraft support frame is moved in the forward and backward directions along the longitudinal direction of the top of the slide support frame portion.
Figure 20 is a partial enlarged view showing an embodiment in which the upper boarding bridge and the entrance of the upper aircraft are docked, and the lower boarding bridge and the lower aircraft are docked according to the present invention;
Figure 21 is a block diagram showing the components of an integrated smart control unit according to the present invention.

Hereinafter, a preferred embodiment according to the present invention will be described with accompanying drawings.

Figure 1 relates to a block diagram showing the configuration of a transfer elevator device directly connected to an aircraft according to the present invention, Figure 2 relates to a perspective view showing the overall shape of an elevator electric car directly connected to an aircraft according to the present invention, and Figure 3 is a It relates to a perspective view showing the overall shape of an elevator electric car connected to the outside of an aircraft according to the present invention, which consists of an elevator electric car directly connected to the aircraft (10) and an elevator electric car (20) connected to the outside of the aircraft.

The aircraft direct connection transfer elevator device (1) according to the present invention will be described.

The aircraft direct connection transfer elevator device (1) is in the shape of a large crane car, aligns one aircraft fuselage at a certain angle and position, raises and moves it, and places it in a vertically parallel structure with another aircraft fuselage, and then each aircraft fuselage It connects the entrance door and elevator to ascend and descend, and connects the boarding gates between the two aircraft.

This consists of an elevator electric car (10) directly connected to the aircraft or an elevator electric car (20) connected to the outside of the aircraft.

First, the electric elevator car 10 directly connected to an aircraft according to the present invention will be described.

The aircraft directly connected elevator electric car 10 vertically positions the bottom opening and closing door of the aircraft located at the top of the vertically parallel structure, and the upper opening and closing door of the aircraft located at the bottom, through the raising and lowering of the vertically rising elevator inside the aircraft located at the bottom. It serves to transfer passengers.

It consists of an aircraft lifting support frame 100, a lower aircraft elevator unit 200, an upper aircraft connecting unit 300, and an integrated control car operating unit 400.

The aircraft elevation support frame 100 has a rectangular frame shape and serves to support the aircraft fuselage and vertically raise and lower it. It includes an elevation support body 110, an elevation cylinder portion 120, and a slide support frame portion ( 130) and an aircraft support frame (140).

The lifting support body 110 is a 'ㄷ' shaped body coupled to the rear center of the integrated control car driving unit. The rear left and right sides are parallel and spaced apart from each other, and a moving wheel is formed at the bottom.

The lifting support body 110 according to the present invention forms the lower part of the aircraft lifting support frame and serves to support the aircraft lifting support frame as a whole.

This movement is achieved by combining one side of the front center with the rear of the integrated control car driver.

The raising and lowering cylinder parts 120 are spaced apart from each other on the left and right sides of the lifting support body, and the upright cylinder structure is formed symmetrically to raise and lower in the up and down directions and serves to raise and lower the aircraft support frame. .

The lifting cylinder unit 120 according to the present invention has a cylindrical shape whose length varies along the longitudinal direction of the cylinder, the lower end of which is coupled to one side of the left and right upper surfaces of the lifting support body in a rotating shaft structure, and the upper end of which slides. It is formed by combining a rotating shaft structure on one side of the left and right lower surfaces of the support frame.

This means that when the cylinder is rotated backwards and laid horizontally based on the lower rotation axis of the elevating cylinder unit 120, the slide support frame unit 130 and the aircraft support frame 140 are lowered to the bottom, and the cylinder is lowered based on the lower rotation axis. When rotated to be vertical and made upright, the slide support frame portion 130 and the aircraft support frame 140 rise in the vertical direction.

At this time, when the elevating cylinder is rotated and laid down so that it is horizontal, the slide support frame and the aircraft support frame are lowered to the lowest level, allowing the upper aircraft fuselage to be raised or lowered on the upper surface of the aircraft support frame, and the elevating and lowering cylinder is rotated so that it is vertical. By making it stand upright and adjusting the height, the aircraft support frame can adjust the height of the upper aircraft fuselage placed on the upper surface of the aircraft support frame.

Here, the fixed height of the slide support frame and the aircraft support frame can be adjusted according to the size of the lower aircraft and the height of the entrance by adjusting the length of the vertical cylinder of the elevating and lowering cylinder.

Through this, the upper aircraft fuselage is raised vertically and the lower aircraft fuselage is positioned at the bottom, so that the upper aircraft and lower aircraft can be positioned in a vertically parallel structure.

The slide support frame unit 130 has a square frame shape with the left and right sides in the longitudinal direction bent into the shape of an upper wing, and the upper end of the raising and lowering cylinder unit is coupled to one side of the lower surface of the left and right bent wings, and the front end is attached to one side of the upper surface. ·It is a frame with a slide groove (130a) formed in the rear direction and serves to support the aircraft support frame coupled to the top.

Here, a slide protrusion 140a protruding from the bottom surface of the aircraft support frame is inserted into the slide groove 130a to allow the aircraft support frame to move in the longitudinal direction.

In the slide support frame 130 according to the present invention, the upper canopy 132 and the lower canopy 133 are moved along the longitudinal direction of the opening/closing door groove 131 formed at the center of the upper surface of the slide support frame.

Here, the upper canopy 132 is raised and lowered in the upper direction and is folded in the shape of a corrugated pipe along the perimeter of the lower opening and closing door of the upper aircraft.

This completely blocks the circumferential surface from the aircraft support frame, which is moved when the elevator car 620 is raised and lowered, to the upper aircraft.

This prevents the elevator car from being exposed to the outside.

Here, the lower canopy 133 is raised and lowered in the downward direction and is folded in the shape of a corrugated pipe along the perimeter of the upper opening and closing door of the lower aircraft.

This completely blocks the circumferential surface from the aircraft support frame, which is moved when the elevator car 620 is raised and lowered, to the lower aircraft.

This prevents the elevator car from being exposed to the outside.

The aircraft support frame 140 is a frame in which slide protrusions 140a are formed in the forward and backward directions on one side of the bottom surface, and is coupled to the upper end of the forward and backward positioning portion in a slide manner to move back and forth in the forward and backward directions to adjust the position. It serves to support the aircraft fuselage on the top surface.

At this time, the aircraft support frame 140 moves forward and backward by converting rotational kinetic energy into linear kinetic energy through forward and reverse rotation of the motor connected to the integrated smart control unit and network.

Here, the slide protrusion 140a is inserted into the slide groove 130a formed on the upper surface of the aircraft support frame to enable the aircraft support frame to move smoothly in the longitudinal direction.

The lower aircraft elevator unit 200 has an elevator shape built into the lower aircraft, and has an upper opening and closing door 210 formed on one side of the upper part of the aircraft, and accommodates a platform 220 and an elevator car 230 inside the lower opening and closing door. , Serves to raise and lower the elevator car using the hydraulic cylinder 230 method.

Here, the top opening/closing door 210 is shaped like a slide door formed on one side of the upper center of the lower aircraft, and opens and closes the top of the platform and elevator car built into the vertical lower part of the door.

Here, the platform 220 is formed in a square structure inside the bottom of the upper opening and closing door to accommodate the elevator car 230, and lifting doors 221 are formed at the front and rear.

At this time, the elevator door 221 blocks the passengers on the lower aircraft from entering the platform when the elevator car 220 of the lower aircraft rises toward the upper aircraft, and opens and closes the car door of the elevator car when the elevator car reaches the platform. It opens and closes only when

This prevents passengers from being exposed to danger when getting on and off the elevator car and prevents accidents.

Here, the elevator car 230 is a rectangular car shape located at the vertical bottom of the upper opening/closing door, accommodates passengers inside, goes up and down in the vertical direction, and is docked toward the bottom of the upper aircraft and toward the top of the lower aircraft.

When placed at the bottom in the vertical direction, it stops at a position that matches the height of the bottom surface of the inner platform of the lower aircraft. It rises through a hydraulic cylinder and stops at a position that matches the height of the bottom surface of the inner platform of the upper aircraft when placed at the top in the vertical direction. It stops.

This allows transfer to occur by moving passengers and cargo located on the lower aircraft to the upper aircraft, or moving passengers and cargo located on the upper aircraft to the lower aircraft.

Through this, passengers boarding the upper and lower aircraft can transfer aircraft without using the airport boarding gate, transfers are made safely without passengers being exposed to the external environment, and the transfer time is shortened so that the waiting time required for transfer is shortened. Time can be minimized.

Here, the hydraulic cylinder 240 is shaped like a cylinder formed at the bottom of the elevator car 230 and functions to move the elevator car in the vertical direction by rising and falling in the vertical direction.

This detects the position of the elevator car through a sensor located on the platform and raises, lowers, and stops the vertical cylinder.

At this time, the cylinder descends to the bottom and stops when it matches the height of the bottom surface of the elevator car and the bottom surface of the lower aircraft platform, and rises to the top and stops when it matches the height of the bottom surface of the elevator car and the bottom surface of the upper aircraft platform.

The upper aircraft connecting portion 300 is shaped like a square hollow door frame formed on the inside of the upper aircraft, with a lower opening/closing door 310 formed on one side of the lower end, a platform 320 formed inside the upper opening/closing door, and a platform 320 formed on the upper inner side of the lower aircraft. It serves to accommodate the elevator car that goes up and down in the vertical direction from the elevator unit.

Here, the lower opening/closing door 310 is in the shape of a slide door formed on one side of the lower center of the upper aircraft, and opens and closes the lower end of the platform built into the vertical upper part of the door.

Here, the platform 320 is formed in a square structure inside the top of the lower opening and closing door to accommodate the elevator car 230 rising from the lower aircraft elevator unit, and lifting doors 321 are formed at the front and rear.

At this time, the elevator door 321 blocks the passengers on the upper aircraft from entering the platform when the elevator car 220 rises and enters the upper aircraft, and opens and closes only when the elevator car reaches the platform and opens and closes the car door of the elevator car. do.

This prevents passengers from being exposed to danger when getting on and off the elevator car and prevents accidents.

The integrated control car operating unit 400 is formed at the front of the aircraft direct-connected elevator electric car, operates and moves the entire aircraft, and controls the aircraft lifting and lowering support frame, the lower aircraft elevator unit, and the upper aircraft connecting unit through an integrated system.

It includes an aircraft lifting control unit 410, a lower aircraft elevator control unit 420, and an upper aircraft connecting control unit 430.

Here, the aircraft lifting and lowering control unit 410 overall controls the driving of the aircraft lifting and lowering support frame.

Here, the lower aircraft elevator control unit 420 overall controls the operation of the lower aircraft elevator unit.

Here, the upper aircraft connecting control unit 430 overall controls the operation of the upper aircraft connecting unit.

Next, the electric elevator car 20 connected to the outside of the aircraft according to the present invention will be described.

The elevator electric car 20 connected to the outside of the aircraft connects the boarding bridge horizontally to the left entrance door of the aircraft located at the top of the vertical parallel structure and the left entrance door of the aircraft located at the bottom, and transfers passengers through the raising and lowering of the elevator located on the left. It plays a role.

It consists of an aircraft lifting support frame 500, an elevator unit 600, an upper boarding bridge 700, a lower boarding bridge 800, and an integrated control car operation unit 900.

The aircraft elevation support frame 500 has a rectangular frame shape and serves to support the aircraft fuselage and vertically raise and lower it. It includes an elevation support body 510, an elevation cylinder portion 520, and a slide support frame portion ( 530) and an aircraft support frame (540).

The lifting support body 510 is a 'ㄷ' shaped body coupled to the rear center of the integrated control car driving unit. The rear left and right sides are parallel and spaced apart from each other, and a moving wheel is formed at the bottom.

The lifting support body 510 according to the present invention forms the lower part of the aircraft lifting support frame and serves to support the aircraft lifting support frame as a whole.

This movement is achieved by combining one side of the front center with the rear of the integrated control car driver.

The raising and lowering cylinder parts 520 are spaced apart from each other on the left and right sides of the lifting support body, and the upright cylinder structure is formed symmetrically to raise and lower in the up and down directions and serves to raise and lower the aircraft support frame. .

The lifting cylinder unit 520 according to the present invention has a cylindrical shape and has a length that varies along the longitudinal direction of the cylinder, the lower end is coupled to one side of the left and right upper surfaces of the lifting support body in a rotating shaft structure, and the upper end is a slide. It is formed by combining a rotating shaft structure on one side of the left and right lower surfaces of the support frame.

This means that when the cylinder is rotated backwards and laid horizontally based on the lower rotation axis of the elevating cylinder unit 520, the slide support frame unit 530 and the aircraft support frame 540 are lowered to the bottom, and the cylinder is lowered based on the lower rotation axis. When rotated to be vertical and made upright, the slide support frame portion 130 and the aircraft support frame 140 rise in the vertical direction.

At this time, when the elevating cylinder is rotated and laid down so that it is horizontal, the slide support frame and the aircraft support frame are lowered to the lowest level, allowing the upper aircraft fuselage to be raised or lowered on the upper surface of the aircraft support frame, and the elevating and lowering cylinder is rotated so that it is vertical. By making it stand upright and adjusting the height, the aircraft support frame can adjust the height of the upper aircraft fuselage placed on the upper surface of the aircraft support frame.

Here, the fixed height of the slide support frame and the aircraft support frame can be adjusted according to the size of the lower aircraft and the height of the entrance by adjusting the length of the vertical cylinder of the elevating and lowering cylinder.

Through this, the upper aircraft fuselage is raised vertically and the lower aircraft fuselage is positioned at the bottom, so that the upper aircraft and lower aircraft can be positioned in a vertically parallel structure.

The slide support frame unit 530 has a square frame shape with the left and right sides in the longitudinal direction bent into the shape of an upper wing, and the upper end of the raising and lowering cylinder unit is coupled to one side of the lower surface of the left and right bent wings, and the front end is attached to one side of the upper surface. ·It is a frame with a slide groove (530a) formed in the rear direction and serves to support the aircraft support frame coupled to the top.

Here, a slide protrusion 540a protruding from the bottom surface of the aircraft support frame is inserted into the slide groove 530a to allow the aircraft support frame to move in the longitudinal direction.

The aircraft support frame 540 is a frame with slide protrusions formed in the forward and backward directions on one side of the lower surface, and is coupled to the upper end of the forward and backward positioning portion in a slide manner to move back and forth in the forward and backward directions to adjust the position. It serves to support the aircraft fuselage.

At this time, the aircraft support frame 540 moves forward and backward by converting rotational kinetic energy into linear kinetic energy through forward and reverse rotation of the motor connected to the integrated smart control unit and network.

Here, the slide protrusion 540a is inserted into the slide groove 530a formed on the upper surface of the aircraft support frame to allow the aircraft support frame to move smoothly in the longitudinal direction.

The elevator unit 600 is in the shape of an upright elevator platform, accommodates an elevator car inside the platform, and is formed on one left side of the elevator support frame to raise and lower the elevator car in the vertical direction. This is the platform 610. , it is composed of an elevator car 620, a counterweight 630, and a traction machine 640.

The platform 610 stands upright on one left side of the elevator support frame, supports the entire elevator unit, and accommodates the elevator car 620.

The elevator car 620 is formed inside the platform and serves to move passengers in the vertical direction by ascending and descending.

The elevator car 620 according to the present invention is horizontally aligned with the upper boarding bridge, which is stopped by matching the vertical and horizontal directions with the boarding gate of the upper aircraft, or the lower boarding bridge is stopped by matching the vertical and horizontal directions with the boarding gate of the lower aircraft. It opens and closes only when the horizontal direction matches.

This stops when the vertical heights match the positions of the upper boarding bridge, which moves vertically according to the height of the entrance of the upper aircraft, and the lower boarding bridge, which moves vertically according to the height of the entrance of the lower aircraft, and the car door opens and closes. .

This allows transfer to occur by moving passengers and cargo located on the lower aircraft to the upper aircraft, or moving passengers and cargo located on the upper aircraft to the lower aircraft.

Through this, passengers boarding the upper and lower aircraft can transfer aircraft without using the airport boarding gate, transfers are made safely without passengers being exposed to the external environment, and the transfer time is shortened so that the waiting time required for transfer is shortened. Time can be minimized.

The counterweight 630 moves up and down in the reverse direction in response to the elevator car's own weight and load, and serves to compensate for the weight of the elevator car.

The hoisting machine 640 is connected to the integrated smart control unit and serves to raise and lower the elevator car by winding or unwinding the rope inside the platform according to the control signal.

The upper boarding bridge 700 is formed on one side of the upper right side of the elevator unit, goes up and down in the vertical direction, adjusts the length in the horizontal direction, and is connected to the aircraft fuselage placed on the aircraft lifting support frame, which is the first aviation entrance. It consists of a horizontal stop line display unit 710, a first aviation entrance vertical stop line display unit 720, a first boarding bridge elevation unit 730, a boarding tunnel unit 740, and a canopy 750.

The first aircraft entrance horizontal stop line display unit 710 is formed in the vertical longitudinal direction on one side of the upper side of the lift support frame and irradiates a laser in the direction of the aircraft entrance located on the left side of the upper aircraft to indicate the upper aircraft located at the top of the aircraft lift support frame. It serves to indicate the stopping position of the moving direction.

This indicates that the horizontal center of the upper aircraft entrance and the horizontal center of the upper boarding bridge are aligned horizontally.

Through this, the horizontal center of the entrance of the upper aircraft can be easily aligned with the horizontal center of the upper boarding bridge, allowing smooth access to the boarding bridge.

The first aircraft entrance vertical stop line display unit 720 is formed in the horizontal longitudinal direction on one side of the upper side of the lift support frame and irradiates a laser in the direction of the aircraft entrance located on the left side of the upper aircraft to indicate the upper aircraft located at the top of the aircraft lift support frame. It serves to indicate the vertical stopping position of.

This indicates that the vertical center of the upper aircraft entrance and the vertical center of the upper boarding bridge are aligned vertically.

Through this, the vertical center of the entrance of the upper aircraft can be easily aligned with the vertical center of the upper boarding bridge, allowing smooth access to the boarding bridge.

The first boarding bridge raising and lowering unit 730 is located at the upper left of the elevator unit and moves up and down in the upward and downward directions to change the height of the upper boarding bridge.

Through this, the entrance height of the upper boarding bridge can be easily adjusted in response to the height of the upper aircraft entrance.

The boarding tunnel section 740 is formed on the left side of the first boarding bridge elevation section, measures the separation distance between the upper aircraft spaced to the left and the left end, and moves forward and backward in the longitudinal direction to the left to change the length and form a passage. .

The canopy 750 is formed on the circumference of the left end of the boarding tunnel and unfolds and folds to correspond to the circumference of the entrance of the aircraft.

The lower boarding bridge 800 is formed on one side of the lower right side of the elevator unit, goes up and down in the vertical direction, adjusts the length in the horizontal direction, and is connected to the aircraft fuselage located at the bottom of the aircraft lifting support frame, which is the second aviation entrance. It consists of a horizontal stop line display unit 810, a second aviation entrance vertical stop line display unit 820, a second boarding bridge raising and lowering unit 830, a boarding tunnel unit 840, and a canopy 850.

The second aviation entrance horizontal stop line display unit 810 is formed in the vertical longitudinal direction on one side of the lower side of the lift support frame and irradiates a laser in the direction of the aircraft entrance located on the left side of the lower aircraft to detect the lower aircraft located at the bottom of the aircraft lift support frame. Displays the stopping position of the moving direction.

This indicates that the horizontal center of the lower aircraft entrance and the horizontal center of the lower boarding bridge are aligned horizontally.

Through this, the horizontal center of the entrance of the lower aircraft can be easily aligned with the horizontal center of the lower boarding bridge, allowing smooth access to the boarding bridge.

The second aviation entrance vertical stop line display unit 820 is formed in the horizontal longitudinal direction on one side of the lower side of the lift support frame and irradiates a laser in the direction of the aircraft entrance located on the left side of the lower aircraft to detect the lower aircraft located at the bottom of the aircraft lift support frame. Displays the vertical stop position of .

This indicates that the vertical center of the lower aircraft entrance and the vertical center of the lower boarding bridge are aligned vertically.

Through this, the vertical center of the entrance of the lower aircraft can be easily aligned with the vertical center of the lower boarding bridge, allowing smooth access to the boarding bridge.

The second boarding bridge raising and lowering unit 830 is located at the bottom left of the elevator unit and moves up and down in the upward and downward directions to vary the height of the lower boarding bridge.

Through this, the entrance height of the lower boarding bridge can be easily adjusted in response to the height of the lower aircraft entrance.

The boarding tunnel section 840 is formed on the left side of the second boarding bridge elevating and lowering section, measures the separation distance between the lower aircraft spaced to the left and the left end, and moves forward and backward in the longitudinal direction to the left to change the length and form a passage. .

The canopy 850 is formed on the circumference of the left end of the boarding tunnel and unfolds and folds to correspond to the circumference of the entrance of the aircraft.

The integrated control car operation unit 900 is formed in the front of the electric transfer elevator car directly connected to the aircraft, operates and moves it as a whole, and controls the aircraft lifting and lowering support frame, elevator unit, upper boarding bridge, and lower boarding bridge as an integrated system. do.

This includes an aircraft lift/lower control unit 910, an elevator control unit 920, an upper boarding bridge control unit 930, and a lower boarding bridge control unit 940.

Here, the aircraft lifting and lowering control unit 910 overall controls the driving of the aircraft lifting and lowering support frame.

Here, the elevator control unit 920 controls the overall operation of the elevator unit.

Here, the upper boarding bridge control unit 930 overall controls the operation of the upper boarding bridge.

Here, the lower boarding bridge control unit 940 overall controls the operation of the lower boarding bridge.

Hereinafter, the specific operation process of the aircraft direct connection transfer elevator device according to the present invention will be described.

First, the operation process of the elevator electric car directly connected to the aircraft is explained.

First, the lifting cylinder part of the aircraft lifting support frame is minimized in the longitudinal direction, and rotated backwards to be horizontal and laid down.

At this time, the slide support frame and the aircraft support frame descend to the lowest level.

In addition, the inclined support plate formed at the rear of the aircraft support frame rotates rearward and unfolds to allow the upper aircraft to be stably moved to the top of the aircraft support frame.

Next, when the upper aircraft is seated on the upper surface of the aircraft support frame, the inclined plane support plate is rotated upward and erected, and the elevating and lowering cylinder part is erected and raised vertically.

Next, move the lower aircraft to the rear of the aircraft lifting support frame, and align the lower opening and closing doors of the upper aircraft and the upper opening and closing doors of the lower aircraft in the vertical direction so that the upper and lower aircraft are positioned in a vertically parallel structure.

Next, the upper canopy of the slide support frame is raised to land on the surrounding surface of the lower opening and closing door of the upper aircraft, the lower canopy is lowered to land on the surrounding surface of the upper opening and closing door of the lower aircraft, and the slide opening and closing door of the aircraft support frame is opened. do.

Next, the elevator car in the elevator section of the lower aircraft is raised and lowered to transfer passengers and cargo of the upper and lower aircraft.

Finally, after completing the transfer, place the elevator car on the platform of the lower aircraft, close the opening and closing doors of the upper aircraft and lower aircraft, return the upper canopy and lower canopy to their original positions, and move the lower aircraft backward or After moving the direct-connected elevator electric car forward, the upper aircraft is placed on the ground.

Second, the operation process of the elevator electric car connected to the outside of the aircraft is explained.

First, the lifting cylinder part of the aircraft lifting support frame is minimized in the longitudinal direction, and rotated backwards to be horizontal and laid down.

At this time, the slide support frame and the aircraft support frame descend to the lowest level.

In addition, the inclined support plate formed at the rear of the aircraft support frame rotates rearward and unfolds to allow the upper aircraft to be stably moved to the top of the aircraft support frame.

Next, when the upper aircraft is seated on the upper surface of the aircraft support frame, the inclined plane support plate is rotated upward and erected, and the elevating and lowering cylinder part is erected and raised vertically.

Next, the lower aircraft is moved to the rear of the aircraft lifting support frame, and the entrance of the upper aircraft and the entrance of the lower aircraft are aligned in the vertical direction so that the upper aircraft and the lower aircraft are positioned in a vertically parallel structure.

Next, the first aviation entrance horizontal stop line indicator and the first aviation entrance vertical stop line indicator of the upper boarding bridge are positioned to match the center of the upper aircraft entrance, the boarding tunnel part is moved and docked, and the entrance is opened to connect the upper boarding bridge. I order it.

Next, the second aviation entrance horizontal stop line indicator and the second aviation entrance vertical stop line indicator of the lower boarding bridge are positioned to match the center of the entrance of the lower aircraft, the boarding tunnel part is moved and docked, and the entrance is opened to connect the lower boarding bridge. I order it.

Next, the elevator car in the elevator section is raised and lowered to transfer passengers and cargo of the upper and lower aircraft.

Finally, when the transfer is completed, the doors of the upper aircraft and lower aircraft are closed, the upper boarding bridge and lower boarding bridge are returned to their original positions, and the lower aircraft is moved rearward through a toy car or the elevator electric car directly connected to the aircraft is moved forward. After doing so, place the upper aircraft on the ground.

1: Aircraft direct-connected elevator device
10: Elevator electric car directly connected to aircraft
100: aircraft lifting support frame 200: lower aircraft elevator unit
300: Upper aircraft connecting part 400: Integrated smart control part
20: Elevator electric car connected to the outside of the aircraft
500: Aircraft lifting support frame 600: Elevator unit
700: upper boarding bridge 800: lower boarding bridge
900: Integrated smart control unit

Claims (11)

In the shape of a large crane car, one aircraft fuselage is aligned at a certain angle and position, then raised and moved to place it in a vertically parallel structure with another aircraft fuselage, and then the doors and elevators of each aircraft fuselage are connected to raise and lower the two aircraft fuselages. An aircraft direct connection transfer elevator device, characterized in that it connects the boarding gates between aircraft.
According to claim 1, the transfer elevator device directly connected to the aircraft is
An elevator electric car (directly connected to the aircraft) that vertically positions the bottom door of the aircraft located at the top of the vertically parallel structure and the top door of the aircraft located at the bottom, and transfers passengers through the raising and lowering of the vertically rising elevator inside the aircraft located at the bottom. 10) Wow,
Among the elevator electric cars (20) connected to the outside of the aircraft that connect the boarding bridge horizontally to the left entrance door of the aircraft located at the top of the vertically parallel structure and the left entrance door of the aircraft located at the bottom, and transfer passengers through the raising and lowering of the elevator located on the left side. An aircraft direct connection transfer elevator device, optionally comprising one configuration.
In claim 2, the elevator electric car (10) directly connected to the aircraft is
An aircraft lifting support frame 100, which has a rectangular frame shape and supports the aircraft fuselage and vertically raises and lowers it,
A lower aircraft elevator unit (200), which has an elevator shape built into the lower aircraft, has an upper opening and closing door on one side of the upper part of the aircraft, accommodates an elevator car inside the lower opening and closing door, and raises and lowers the elevator car using a hydraulic cylinder,
An upper aircraft connecting portion 300 in the shape of a square hollow door frame formed on the inside of the upper aircraft, with a lower opening and closing door formed on one side of the lower part to accommodate the elevator car that is vertically raised and lowered in the lower aircraft elevator unit,
It is formed in front of the aircraft directly connected elevator electric car, operates and moves it as a whole, and is characterized by consisting of an integrated control car operation unit 400 that controls the aircraft lifting and lowering support frame, the lower aircraft elevator part, and the upper aircraft connecting part in an integrated system. Aircraft direct connection transfer elevator device.
In clause 3, the aircraft lifting support frame 100 is
A 'ㄷ' shaped body coupled to the rear center of the integrated control car driving unit, the rear left and right sides are parallel and spaced apart from each other, and a lifting support body 110 with a moving wheel formed at the bottom,
An elevation cylinder unit 120 that is spaced apart from each other on the left and right sides of the elevation support body and has an upright cylinder structure formed symmetrically, raises and lowers in the upward and downward directions and raises and lowers the aircraft support frame,
A frame in the shape of a square frame with the left and right sides in the longitudinal direction bent into the shape of an upper wing. The upper end of the raising and lowering cylinder is joined to one side of the bottom surface of the left and right bent wings, and a slide groove is formed in the forward and backward directions on one side of the upper surface. A slide support frame portion 130 that supports the aircraft support frame coupled to the top,
It is a frame with a slide protrusion formed in the forward and backward directions on one side of the bottom side, and is attached to the top of the forward and backward positioning part in a slide manner to move back and forth in the forward and backward directions to adjust the position, and supports the aircraft fuselage on the upper side. A transfer elevator device directly connected to an aircraft, characterized in that it consists of a support frame (140).
According to claim 4, the slide support frame portion 130 is
An upper canopy (132) that is in the shape of a corrugated pipe that is raised and lowered in the upper direction and folded along the perimeter of the lower opening and closing door of the upper aircraft,
A lower canopy (133) is formed in the shape of a corrugated pipe that is raised and lowered in the downward direction and folded along the perimeter of the upper opening and closing door of the lower aircraft,
An aircraft direct connection transfer elevator device, characterized in that the upper canopy and the lower canopy are moved along the longitudinal direction of the opening/closing door groove (131) formed at the center of the upper surface of the slide support frame.
In claim 2, the elevator electric car (20) connected to the outside of the aircraft is
An aircraft elevation support frame 500, which has a rectangular frame shape and supports the aircraft fuselage and vertically raises and lowers it,
An elevator unit 600 that has the shape of an upright elevator platform, accommodates an elevator car inside the platform, and is formed on one left side of the elevator support frame to raise and lower the elevator car in the vertical direction,
An upper boarding bridge 700 formed on one side of the upper right side of the elevator unit, raises and lowers in the vertical direction, adjusts the length in the horizontal direction, and is connected to the aircraft fuselage placed on the aircraft lifting support frame,
A lower boarding bridge 800 that is formed on one side of the lower right side of the elevator unit, moves up and down in the vertical direction, adjusts the length in the horizontal direction, and is connected to the aircraft fuselage located at the bottom of the aircraft lifting support frame,
It consists of an integrated control car operation unit 900 that is formed in front of the electric transfer elevator car directly connected to the aircraft, operates and moves it as a whole, and controls the aircraft lifting and lowering support frame, elevator unit, upper boarding bridge, and lower boarding bridge in an integrated system. Characterized by aircraft direct connection transfer elevator device.
In claim 6, the lifting support frame 500 is
A 'ㄷ' shaped body coupled to the rear center of the integrated control car driving unit, the rear left and right sides are parallel and spaced apart from each other, and a lifting support body 510 with a moving wheel formed at the bottom,
An elevating cylinder unit 520 that is spaced apart from each other on the left and right sides of the elevating support body and has an upright cylinder structure formed symmetrically, elevating and lowering in the upward and downward directions and elevating and lowering the aircraft support frame,
A slide support frame portion 530 that is coupled to the upper end of the elevating cylinder and has a slide groove formed in the front and rear directions on one side of the upper surface, and supports the aircraft support frame coupled to the upper end,
It is a frame with a slide protrusion formed in the forward and backward directions on one side of the bottom side, and is attached to the top of the forward and backward positioning part in a slide manner to move back and forth in the forward and backward directions to adjust the position, and supports the aircraft fuselage on the upper side. A transfer elevator device directly connected to an aircraft, characterized in that it consists of a support frame (540).
In claim 6, the elevator unit 600 is
A platform 610 that stands upright on the left side of the elevator support frame and supports the elevator unit as a whole,
An elevator car 620 formed inside the platform to move passengers vertically by ascending and descending,
A counterweight 630 that moves up and down in the reverse direction in response to the self-weight and load of the elevator car and compensates for the weight of the elevator car,
A transfer elevator device directly connected to an aircraft, characterized in that it includes a traction machine 640 that is connected to an integrated smart control unit and raises and lowers the elevator car by winding or unwinding the rope inside the platform according to the control signal.
The elevator car 620 of claim 8 is
It is characterized in that it opens and closes only when the vertical and horizontal directions match the boarding gate of the upper aircraft and coincide with the horizontal direction with the stopped upper boarding bridge, or when the vertical and horizontal directions match the boarding gate of the lower aircraft and match the horizontal direction with the stopped lower boarding bridge. A transfer elevator device that connects directly to aircraft.
In clause 6, the upper boarding bridge (700) is
The first aviation entrance is formed in the vertical longitudinal direction on one side of the upper side of the lifting support frame and displays the stop position of the moving direction of the upper aircraft located at the top of the aircraft lifting support frame by irradiating a laser in the direction of the aircraft entrance located on the left side of the upper aircraft. A horizontal stop line display unit 710,
The first aviation entrance is formed in the horizontal longitudinal direction on one side of the upper side of the lifting support frame and displays the vertical stopping position of the upper aircraft located at the top of the aircraft lifting support frame by irradiating a laser in the direction of the aircraft entrance located on the left side of the upper aircraft. A vertical stop line display unit 720,
A first boarding bridge elevating and lowering unit 730 located at the upper left of the elevator unit and raising and lowering in the up and down directions and varying the height of the upper boarding bridge,
A boarding tunnel section 740 formed on the left side of the first boarding bridge elevating and lowering section, measuring the separation distance between the upper aircraft spaced to the left and the left end, and forming a passage with a variable length by moving forward and backward in the left longitudinal direction;
A transfer elevator device directly connected to an aircraft, characterized in that it consists of a canopy (750) formed on the left end circumference of the boarding tunnel section and unfolding and approaching the circumference of the entrance of the aircraft.
In clause 6, the lower boarding bridge (800) is
A second aviation entrance is formed in the vertical longitudinal direction on one side of the lower side of the lifting support frame and displays the stop position of the moving direction of the lower aircraft located at the bottom of the aircraft lifting support frame by irradiating a laser in the direction of the aircraft entrance located on the left side of the lower aircraft. A horizontal stop line display unit 810,
A second aviation entrance is formed in the horizontal longitudinal direction on one side of the lower side of the lift support frame and displays the vertical stopping position of the lower aircraft located at the bottom of the aircraft lift support frame by irradiating a laser in the direction of the aircraft entrance located on the left side of the lower aircraft. A vertical stop line display unit 820,
A second boarding bridge elevation unit 830 located at the bottom left of the elevator unit that rises and descends in the up and down directions and changes the height of the lower boarding bridge,
A boarding tunnel portion 840 formed on the left side of the second boarding bridge elevating and lowering section, measuring the separation distance between the lower aircraft spaced to the left and the left end, and forming a passage with a variable length by moving forward and backward in the longitudinal direction to the left;
A transfer elevator device directly connected to an aircraft, characterized in that it consists of a canopy (850) that is formed on the left end circumference of the boarding tunnel section and unfolds and approaches the circumference of the entrance of the aircraft.