| FR2318811A1 | 1977-02-18 | |||
| EP0263540A1 | 1988-04-13 | |||
| CH468917B |
| 1. | An automatic device to facilitate the loading and unloading of the passengers luggage into and out of the door of the hold or luggage compartment of the aircraft , which device comprises : a horizontal platform which supports an endless belt in a temporary prosecution to an conventional elevating conveyor of the luggage the purpose of which is to receiving said luggage in succession, an outer wheeled frame adapted for travelling over the aircraft hold bottom; said wheeled frame being connected with said platform by means of telescopic elements ; means for causing said telescopic elements to slide and carry said platform with each luggage on top of it as far as the operator located inside the aircraft hold; a proximity switch for interrupting the • platform travel near the operator and a luggage presence sensing switch which controls the return of the platform to its initial position. |
| 2. | A device according fco claim 1 characterized by the fact that said telescopic elements connecting said outer wheeled frame with said platform comprise an inner frame (16) which is bound to said elevating conveyor and is stationary within said fuselage hold in front of said hold door and a middle telescopic frame (17) wrapped up on inner frame (l6) and slidable to extend for all its lenght forwards and rearwards of he luggage compartment, the outer frame (l8) being wrapped up on middle frame (17) and slidable fco extend for all its lenght from said middle frame (17) forwards and rearwards of the luggage compartment, the stretching of middle frame (17) with respect to inner frame (l6) being controlled by four pneumatic rodless pistons ( 19, 19 ' , 20,21) which are actuated by a logical circuit controlled by a detector of a presence of a piece of luggage on the platform belt 5 (9'). |
| 3. | A device as claimed in claims 1 and 2 wherein the outer surface of the outer frame (18) is wrapped up by said platform (9) which is fastened to it and is provided with an endless belt (91) mounted on a pair of end rollers o and on a pair of transmission rollers idly mounted on the platform sides (14) A device according to claims 13 characterized by the fact that said device comprises a means for controlling the movement of going and coming of the ]5 platform (9) along the luggage compartment of the aircraft which means is adapted for being controlled by the operator whereby the travel of said going and coming movement is progressively shortened and extended. |
| 4. | A device as claimed in claims 14 characterized '20 ~~Υ the fact that the return movement of the empty platform (9) to the spot where a next piece of luggage ■is received to said platform from said elevator conveyor is controlled by a.sensor of weight. |
| 5. | A device according to claims 15 characterized 25 by the fact' of being provided with a means for transferring each piece of luggage (26) from conventional elevating conveyor to said platform (9) which means comprises a roller (23) interposed between the upper end of said elevating conveyor and the beginning of said 30 endless belt (9'); said roller being actuated by a pneumatic j'ack. |
| 6. | A device according fco claims 16 characterized by the fact that said platform endless belt (91 ) is provided with a sensor of weight adapted for interrupting the movement of said endless belt, as soon as said piece of luggage has 'reached the center of said platform within the inside of the aircraft hold. |
| 7. | A device according to claims 17 characterized by the fact of being provided with a control for inverting the coming and going movement of said platform along the aircraft luggage compartment whereby the two rearward and forward spaces of said compartment can be filled by the operator with passengers luggage. |
| 8. | A device according to the claims 18 characterized by the fact that said four rodless pistons are pneumatically operated and laying coplanar within the space defined by said inner, middle and outer telescopic frames of which pistons two (19,19' ) are central with respect to the other two (20,21) and are fastened to the middle frame while the other two are lateral, and are associated respectively with the inner frame and with the outer frame, the mobile frame of said lateral, pistons being fastened to the' mobile frame of the adjacent central piston. |
f The object of fche present invention is an automatic device to facilifcate the loading and unloading of luggage in and out of an aircraft hold.
All the efforts of the designers and engineers
5 in the field of air travel are finalized according to two main directions: to improve the aircraft performances, the safety and the comfort of the aircraft and fco improve the ground services which constitute an integrating and indispensable part of the air activity.
10 Among the ground facilities the luggages transportation to the aircraft and their settlement within the aircraft hold are not disregardful with respect to the effectiveness and then to the good quality of the service.
The same should be said about the reverse
15 operations of unloading and sorting the luggages at the end of a flight .
. Presently such operations • are carried out by means of an elevating fcruck. provided with an endless . conveyor which carries the luggages in succession up to
20 the aircraft hold door. At fche inside of the hold in an inconvenient position due fco the very limited height (which could be less than 80 cm. ) , two or more operators take up the luggages from the elevating conveyor and arrange them in the hold. This method, implies several 25 drawbacks such as fche need for equalizing the intervention speeds of fche various operators to the • speed of the elevating conveyor, the luggages accumulation being consequently caused in addition to fche chance of damaging
the luggages and stopping the conveyor itself, the luggage being some times transferred from an operator to another by hurling i .
The purpose of the invention is to realize a device adapted to prevent the above drawbacks so that the arrangement of the luggages within the aircraft hold is made rational, quick and easy.
According to the invention an automatic loading and unloading device is provided which comprises an endless belt platform adapted for receiving rom a conventional elevating conveyor various luggage pieces in succession and for disposing them at the level of the hold floor, an assembly of telescopic frames being provided for moving said receiving platform; means being provided for causing said frames to slide along the aircraft hold together with said platform until the latter automatically stops near an operator; means being provided for returning said platform, when empty, to the starting point for receiving a novel luggage after the operator has lifted fche luggage for arranging it in a proper position within the hold. Said means for operating the coming and - going movement of the platform comprises a contact sensor which ■ acts ' depending on fche operator physical contact so that the coming and going travel is progressively shortened any time the operator proceeds from the hold end wall to the loading door.
Still according to the invention the sliding motion of said telescopic frames is controlled by a series of rodless pistons pneumatically operated which are controlled by a logic circuit which depends on said contact sensor and on a sensor of the luggage presence on said endless conveyor of the platform.
In order to transfer each luggage from the free end of fche conventional elevating conveyor to said platform a pneumatic roller is provided which is interposed between the elevator conveyor and the endless -5 belt of the sliding platform which roller fits to contact the last roller of the elevating conveyor together with the first roller of the sliding platform endless belt. Thus the movement of the elevating conveyor is transmitted to said platform and a piece of luggage is transferred 0 onto the platform to reach the center of the latter. As it will be explained hereinafter the platform is then disengaged from the elevating conveyor and by other means hereinafter described it can be moved towards either of the two spaces of the aircraft hold forward and rearward
15 with respect to the hold door.
The invention will be now described with reference to the attached drawings wherein a preferred . embodiment thereof is described as an illustration and not as a limitation thereof.
20 - ~ - n tne drawings:
Fig.1 is a side perspective view of a- conventional elevating conveyor which is a " constituent ■ part of the device according to the invention and is approached to the luggage hold of an aircraft;
25 Figj 2 shows a plan view corresponding to Fig.l;
Fig.3 shows the detail of the endless belt platform according to the invention as shown in cross section along plane III-III of fig.2 and in an elarged j scale;
30 Fig. 4 and 5 show two views similar to figures 1 and 2, said platform being inserted into the luggage hold of the aircraft;
Fig.6 shows in an enlarged scale, the detail A of fig.4;
Figs .7 and 8 show two views similar to Figs.l and 2 wherein the first luggage piece is arranged on said platform within the hold;
Fig.9 is a view similar to Fig.6 and shows the motion transmission from the elevating conveyor to said platform;
Figs. 10 and 11 show the sliding of the platform along the inside of the hold to reach the operator;
Figs. 12 and 13 show the progressive filling of one of the two spaces of the aircraft hold starting from one end of the hold and reaching the filling door. Figs.14 and 15 show the beginning of the loading of the luggage into the second space of the hold;
With reference to figures 1 and 2 number 1 indicates the whole of a wheeled truck , of known type, which carries an elevating belt conveyor 2 combined with an hydraulic jack 3, the purpose of which is lifting the upper roller 4 of the elevating belt conveyor up to the level of the floor 5 of the aircraft hold where the luggage 6 is loaded, which hold is located ' in the lower compartment of an aircraft fuselage; said hold being closed by a door 8. The device according to the invention comprises an endless belt 9' supported by a platform 9 which is temporarily mounted in continuation to said elevating belt conveyor 2 and which has a breadth sucht that it can be fitted into the throat 10 at the level of the floor 5 of hold 6.
The device according to the invention is shown in detail in figure 3. The endless belt 9' of platform 9
is mounted on a pair of end rollers 11,12 and on a second pair of transmission rollers 13 which are mounted idle on the side panels 14 of platform 9 which fastened to the outermost frame 18 of a group of three telescopic frames
5 indicated by l6,17,l8 which are located underneath the endless belt 9 ' of platform 9 •
As can be seen in figures 3, 10 and 11 the inner frame 16 is firmly bound to the frame 30 of elevator truck 1 through rods 15 and therefore when platform 9 enters the
10 loading door of the aircraft and stops therein, the frame 16 also stops and defines the moving direction of platform 9 in either directions that is rearward and forward of the aircraft .
In fact the two frames 17 and l8 are wrapped up
15. on stationary frame 16, the frame 17 being slidably wrapped up on frame 16 while frame 18 is slidably wrapped up on frame 17- The successive stretching of frame 17 from frame 16 and of frame 18 from frame 17 is such that the three frames at the maximum of their stretching, extend
20 from the loading door to one or the other end of the luggage compartment.
As shown in F.ig.3 the outer surface of frame l8 is wrapped up by platform 9 which is fastened to it- and. therefore it accompanies the same along the total of its
25 travel. It is to be noted that frame l8 is provided with wheels which run on the floor 5 of the loading compartment of the aircraft.
The displacement of platform 9 in either of the two directions is determined by the stretching of frames
30 17 and 18 in one or the other directions, the movement of these frames depending on a command imparted by an operator who stands within the aircraft hold and is free
fco move from one to the other end of the luggage compartment.
The sliding movement of said telescopic frames
17,l8 ( and then the translation of the platform 9 within • the load space ) is controlled by four pneumatic rodless pistons indicated by numbers 19, 19', 20 and 21 which are not described in detail inasmuch as they are known and can be found in the trade. The two center pistons 19,19' , are associated to the intermediate frame 17, while the two side pistons 20 and 21, the sliding elements of which are each connected with the sliding movement of the contiguous center piston, are respectively associated with the inner frame 16 and with the outer frame 18. Said pistons are all controlled by an operating logics assembly which is also preferably pneumatic and determines from time to time both the travel of the platform within the load space and the two opposite directions of the same travel as it will be better explained hereinafter.-
In order to transmit the movement of elevating conveyor 2 to endless belt of platform 9 the system illustrated in Fig.6 is provided . ' It comprises an idler roller 22 sustained by a .pneumatic cylinder 23 which is mounted on arm 2 • -
The operation is as follows: the wheeled truck 1 with platform 9 is approached to the aircraft fuselage and the loading door 8 is opened (Fig.l and 2). Thereafter j ' ack 3 is actuated to bring platform " 9 up to fche level of the " aircraft hold.
The total of the platform 9 including the package of frames 16,17 and 18 and including the battery of four pneumatic rodless pistons 19,19' , 20 and 21 is then inserted into fche aircraft hold so that the wheels 25
of telescopic frame 18 are laid down to mate the floor of the aircraft hold.
Subsequently a piece of luggage 26 is disposed in succession with other pieces on the elevating conveyor belt 2 which takes it to the level of the loading hold. The endless belt 9' of the platform 9 is stopped for the moment as illustrated by Fig.6.
As soon as the first piece of luggage 26 has reached the summit of elevating conveyor 2, the engagement of the transmission roller 22 is obtained by means of the pneumatic cylinder 23 (Fig.9) whereby belt 9' of platform 9 starts to run and receives the piece of luggage 26 from conveyor 2. As soon as the piece of luggage 26 reaches the center of platform 9 (Figs. 7 and 8) the assembly of conveyors 2 and 9' stops automatically and platform 9 . slides along the inside of the hold (Figs.10 and 11) being actuated by pistons 19, 19', 20, 21 of Fig.3 which determine the extension of telescopical frames 17 and lδ.
When platform 9 with piece of luggage 26 has reached the operafcor 27 which is standing near the end wall 28 of the aircraft hold (Fig.11) then a circuit breaker stops the. sliding of the platform 9 and operator 27 lifts the piece of luggage and places it in the ' hold. Another load sensing circuit breaker feels the luggage taking and operates the return of the empty platform to its original position . Subsequently the cycle is repeated by starting the movement of conveyor 9' of platform 9 and by the arrival of the next luggage piece until the loading of one of the two hold spaces is completed as shown by figure 13-
At the end of the above period the operator actuates a control which inverts fche sliding travel of -
platform 9 along the aircraft hold and the loading of the second space is initiated, starting from the end wall 29 of fche hold as shown in Fig.15. At the end of this second period, the wheeled truck 1 is wifchdrawn and the aircraft door 8 is closed.
The above operations in the reversed order are effected for unloading the luggage at the end of the flight.
. From the above it clearly appears that the described device permits along other advantages, to "humanize" the loading and unloading work inasmuch as the frequency of loading and unloading operations is determined by the operator and not by the speed of the elevator conveyor 2 as it presently occurs. Furthermore the luggage loading and unloading can be effected by a single operator located inside of the hold.
The present invention has been illustrated and described in a preferred embodiment; however it is intended that structural variants can be added thereto without departing from the scope of the present invention.