CN112184121A - Method and device for generating loading scheme of aircraft cargo compartment and electronic equipment - Google Patents
Method and device for generating loading scheme of aircraft cargo compartment and electronic equipment Download PDFInfo
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Abstract
The invention discloses a method and a device for generating an aircraft cargo compartment loading scheme and electronic equipment. According to the invention, a plurality of loading templates are generated for the selection of the fitter, so that the professional requirements on the fitter, namely the labor cost is reduced, the loading efficiency is improved, and each loading condition is fully utilized, so that the loading is safer.
Description
Technical Field
The invention relates to the technical field of information processing, in particular to a method and a device for generating an aircraft cargo compartment loading scheme and electronic equipment.
Background
The loading of the aircraft cargo hold is a necessary program before the aircraft takes off, and the selection of the existing loading scheme of the aircraft cargo hold requires that a fitter selects an appropriate template from templates of the loading scheme of the aircraft cargo hold according to flight loading requirements, including information of goods, mails, luggage and the like of the flight and experience of the fitter. However, this approach has the following disadvantages: firstly, the requirement on the specialty of the stowage personnel is high, the stowage personnel need abundant stowage experience, long-time training is needed in the early stage to carry out the operation on duty, and the labor cost is high; secondly, the stowage personnel need to allocate the goods space to each cargo, mail and luggage in turn and need to adjust according to the loading rule, so that the working procedure is complex and the efficiency is low; finally, there may be human error in the operation process of the distribution personnel, for example, the dangerous goods isolation rule cannot be fully considered, and the dangerous goods which cannot be put in the same cargo space are put together, which brings risks and hidden troubles to transportation.
It can be seen that the loading of the cargo hold of an aircraft by the subjective experience of the fitter has not been able to meet the actual requirements.
Disclosure of Invention
In order to solve the problems, the invention provides a method and a device for generating a cargo compartment loading scheme of an aircraft, and electronic equipment, so that the aims of reducing personnel cost and improving loading efficiency and cargo loading safety are fulfilled.
In order to achieve the purpose, the invention provides the following technical scheme:
an aircraft cargo compartment loading scheme generation method comprising:
acquiring information of an article to be loaded, wherein the article to be loaded comprises one or more of goods, mails and luggage;
generating at least one loading template based on the to-be-installed article information, the cargo compartment layout map information and preset loading conditions, wherein the loading conditions comprise one or more of weight limitation conditions, gravity limitation conditions, isolation conditions and loading priority conditions, and the cargo compartment layout map information comprises container positions, container plate positions, cabin door positions and bulk compartment positions;
determining an initial template in response to the selection of the loading template;
generating visual loading display information according to the initial template and the information of the articles to be loaded;
and if the visual loading display information is determined, determining the initial module as a target loading template, so that the object to be loaded is loaded through the target loading template.
An aircraft cargo compartment loading solution generating apparatus comprising:
the device comprises an acquisition unit, a storage unit and a processing unit, wherein the acquisition unit is used for acquiring information of articles to be loaded, and the articles to be loaded comprise one or more of cargos, mails and luggage;
a first generating unit, configured to generate at least one loading template based on the to-be-loaded item information, the cargo space layout map information, and preset loading conditions, where the loading conditions include one or more of a weight limitation condition, a center-of-gravity limitation condition, an isolation condition, and a loading priority condition, and the cargo space layout map information includes a container position, a container panel position, a hatch door position, and a bulk cargo space position;
a first determining unit for determining an initial template in response to the selection of the loading template;
the second generation unit is used for generating visual loading display information according to the initial template and the information of the articles to be loaded;
and the second determining unit is used for determining the initial module as a target loading template if the visual loading display information is determined, so that the object to be loaded is loaded through the target loading template.
A storage medium having stored thereon executable instructions that, when executed by a processor, implement the aircraft cargo compartment loading scenario generation method of any of the above.
An electronic device, comprising:
a memory for storing a program;
a processor configured to execute the program, the program specifically configured to:
acquiring information of an article to be loaded, wherein the article to be loaded comprises one or more of goods, mails and luggage;
generating at least one loading template based on the to-be-installed article information, the cargo compartment layout map information and preset loading conditions, wherein the loading conditions comprise one or more of weight limitation conditions, gravity limitation conditions, isolation conditions and loading priority conditions, and the cargo compartment layout map information comprises container positions, container plate positions, cabin door positions and bulk compartment positions;
determining an initial template in response to the selection of the loading template;
generating visual loading display information according to the initial template and the information of the articles to be loaded;
and if the visual loading display information is determined, determining the initial module as a target loading template, so that the object to be loaded is loaded through the target loading template.
Compared with the prior art, the invention provides a method and a device for generating an aircraft cargo compartment loading scheme and electronic equipment. According to the invention, a plurality of loading templates are generated for the selection of the fitter, so that the professional requirements on the fitter, namely the labor cost is reduced, the loading efficiency is improved, and each loading condition is fully utilized, so that the loading is safer.
Drawings
The above and other features, advantages and aspects of embodiments of the present disclosure will become more apparent from the following detailed description when taken in conjunction with the accompanying drawings. Throughout the drawings, the same or similar reference numbers identify the same or similar elements. It should be understood that the drawings are diagrammatic and that elements and features are not necessarily drawn to scale.
Fig. 1 is a schematic flow chart of a method for generating a cargo compartment loading scheme of an aircraft according to an embodiment of the present invention;
FIG. 2 is a schematic structural diagram of an automatic selection system for templates of cargo compartment loading schemes of an aircraft according to an embodiment of the present invention;
fig. 3 is a flowchart illustrating a distribution process of articles to be loaded according to an embodiment of the present invention;
fig. 4 is a schematic structural diagram of an aircraft cargo compartment loading scheme generating device according to an embodiment of the present invention.
Detailed Description
Embodiments of the present disclosure will be described in more detail below with reference to the accompanying drawings. While certain embodiments of the present disclosure are shown in the drawings, it is to be understood that the present disclosure may be embodied in various forms and should not be construed as limited to the embodiments set forth herein, but rather are provided for a more thorough and complete understanding of the present disclosure. It should be understood that the drawings and embodiments of the disclosure are for illustration purposes only and are not intended to limit the scope of the disclosure.
The term "include" and variations thereof as used herein are open-ended, i.e., "including but not limited to". The term "based on" is "based, at least in part, on". The term "one embodiment" means "at least one embodiment"; the term "another embodiment" means "at least one additional embodiment"; the term "some embodiments" means "at least some embodiments". Relevant definitions for other terms will be given in the following description.
It should be noted that the terms "first", "second", and the like in the present disclosure are only used for distinguishing different devices, modules or units, and are not used for limiting the order or interdependence relationship of the functions performed by the devices, modules or units. The modifications referred to in this disclosure as "a", "an", and "the" are illustrative and not restrictive, and it will be understood by those skilled in the art that "one or more" may be used unless the context clearly dictates otherwise.
In an embodiment of the present invention, a method for generating a cargo compartment loading scheme of an aircraft is provided, and referring to fig. 1, the method may include the following steps:
s101, obtaining information of the object to be loaded.
The articles to be loaded comprise one or more of goods, mails and luggage. The types of items loaded in the aircraft cargo hold in embodiments of the invention may be varied, i.e. the method may be based on the generation of loading schemes for different types of items. The information of the goods to be loaded comprises the arrival stations of goods, mails and baggage, the types of the goods, the predicted weight, the actual weight, the volume of the goods, the station passing identification, the priority, the special goods code, the final arrival station and the like, and for the containerized airplane, the information comprises the types of the containers used by the goods, the serial numbers of the containers and the like.
And S102, generating at least one loading template based on the information of the articles to be arranged, the information of the cargo compartment layout and preset loading conditions.
The loading condition includes one or more of a weight limit condition, a center of gravity limit condition, an isolation condition, and a loading priority condition. The loading conditions can meet the loading requirements of goods in the cargo hold of the airplane, and the properties of the goods, the isolation requirements of the goods and the limit information of the airplane are fully considered, so that the goods loading efficiency is higher and the goods loading is safer. The generated loading template is a loading scheme obtained based on the articles to be loaded currently, and in the embodiment of the application, the information in the loading template is visual information and information which can be adjusted, displayed and fed back by receiving a trigger instruction of a user. The cargo bay layout information includes container location, pallet location, bay door location, and bulk bay location.
S103, responding to the selection of the loading template, and determining an initial template.
And S104, generating visual loading display information according to the initial template and the information of the articles to be loaded.
S105, if the visual loading display information is determined, the initial module is determined to be a target loading template, and articles to be loaded are loaded through the target loading template.
When a user selects one loading template as an initial template, displaying information of the articles to be loaded based on the initial template, wherein the displaying refers to the visual loading display information which is the virtual display information after the articles are loaded in the cargo hold, and if an allocator confirms the information, the assembling scheme is approved, and the initial template is determined as a target loading template. And if the visual loading display information is adjusted, adjusting the initial template according to the adjustment information to obtain a target loading template.
In another possible implementation manner, if the visual loading display information is adjusted, based on the adjustment information, a loading result of the to-be-loaded item is obtained; and judging whether the loading result meets the preset loading condition, if not, generating prompt information, wherein the prompt information is used for prompting that the adjustment information does not meet the loading condition.
It should be noted that the information generated in the embodiment of the present application may be embodied in the form of presentation information, that is, the information is visual information for users, and the information may respond to the needs of users for increasing, deleting and modifying, so as to facilitate the visualization operation for users. Specifically, the method comprises the following steps: acquiring airplane flight information corresponding to the information of the articles to be loaded; and generating flight display information according to the airplane flight information, wherein the flight display information comprises flight basic information and flight gravity center information, the flight basic information is displayed in a text format, and the flight center information is displayed in a graphic format.
The display information of the articles to be loaded is generated based on the information of the articles to be loaded, and the display information of the articles to be loaded comprises label information and description information; and receiving a modification instruction aiming at the information of the articles to be loaded, and modifying the display information of the articles to be loaded to obtain modified display information of the articles to be loaded, wherein the modification instruction comprises one or more of instructions for increasing, decreasing, checking and modifying the articles.
Correspondingly, the method further comprises the following steps:
acquiring flight cargo space information based on the airplane flight information;
generating cargo compartment display information corresponding to the flight cargo compartment information, wherein the cargo compartment display information comprises a cargo compartment layout chart, compartment position information, cargo position information and allocated cargo position information;
and if the aircraft is a containerized aircraft, generating container information supported by the aircraft.
Optionally, the method further comprises:
generating a cargo distribution schematic diagram for the information of the articles to be loaded;
responding to the display of the acquired distribution schematic diagram, and receiving a selection instruction of a user;
if the selection instruction of the user is a determination instruction of the distribution schematic diagram, determining that the distribution schematic diagram is a loading scheme corresponding to the information of the articles to be loaded;
otherwise, a new cargo allocation map is generated.
According to the method for generating the loading scheme of the aircraft cargo hold, provided by the embodiment of the invention, the loading rules including weight limit rules, gravity center limit rules, dangerous goods isolation rules, loading service priority rules and the like are fully considered according to the conditions of cargos, mails and luggage to be loaded, the applicable cargo hold loading templates are automatically selected, and meanwhile, a plurality of sets of templates can be selected for the configuration personnel to select and use. The method of the invention can effectively improve the defects of the prior loading scheme: firstly, the method can automatically select the applicable cargo hold loading template, and simultaneously can select a plurality of sets of templates for the configuration and carrier to select for use, the configuration and carrier only needs to select one set of templates, the loading rule of the given loading template is fully considered, the configuration and carrier does not need to adjust the templates, the professional requirement on the configuration and carrier is reduced, and the training cost of the configuration and carrier at the early stage is saved; secondly, after the fitter selects the template, the system can automatically distribute goods, mails, luggage and the like to each cargo space of the aircraft cargo hold and display back a graphical distribution result, so that the operation is simple and rapid, the result is clear, and the working efficiency of the fitter is improved; finally, the cargo compartment loading scheme provided by the invention fully considers loading rules, including weight limit rules, gravity center limit rules, dangerous goods isolation rules, loading service priority rules and the like, does not need to be manually adjusted, reduces the interference of human factors, meanwhile, any abnormal condition is generated in the operation process of the cargo allocation personnel, for example, the cargo position of a certain cargo position is manually adjusted, so that the loading weight of the certain cargo position exceeds the specified weight limit, the system can give an error report prompt, the cargo allocation personnel can carry out the next operation only by processing the error report, and the potential safety hazard of production is reduced.
The method for generating the aircraft cargo compartment loading scheme provided by the invention is applied to an automatic selection system of the aircraft cargo compartment loading scheme template. Referring to fig. 2, the system comprises a flight basic information management component, a flight cargo mail baggage information management component, a flight cargo space information management component, an automatic balancing component and other templates. The components that make up the system in fig. 2 are merely schematic representations of one possible implementation and may include other components as well, which the present application does not limit.
Flight basic information management component: the basic functions of the flight information display system are to display basic flight information, help an onloader to know the basic situation of the flight, display graphical flight center-of-gravity information, and enable the onloader to know whether the flight center-of-gravity is within a safety range or not by observing the information. The flight basic information comprises flight number, flight date, takeoff station, arrival station, airplane registration number, airplane cabin layout, airplane team of the airplane, residual service load of the flight and the like; the flight gravity center information comprises ZFW (Zero Fuel Weight), TOW (Take-Off Weight), MAC (MAC: Mean Aerodynamic Chord, Chord length behind a wing of the airplane which is simplified into a rectangular wing, the gravity center condition of the airplane is generally represented by a method of projecting the gravity center of the airplane onto the MAC, and is called MAC percent value, FWDMAC (Forward MAC, MAC percent front limit) value, AFTMAC (Afterward MAC, MAC percent rear limit) value and MAC value of DLW (DeadWeight ).
Flight cargo mail baggage information management component: the component can help the stowage personnel to comprehensively know the information of the goods, the mails and the luggage of the flight, and meanwhile, the stowage personnel can manage the information of the goods, the mails and the luggage of the flight through the component; the information of the goods, the mails and the luggage comprises the arrival stations of the goods, the mails and the luggage, the types of the goods, the predicted weight, the actual weight, the volume of the goods, the station passing identification, the priority, the special goods code, the final arrival station and the like, and for the containerized airplane, the information comprises the types of containers used by the goods, the serial numbers of the containers and the like; the management of the flight goods, mails and baggage information comprises the operations of adding, viewing and modifying, pulling down, recovering, deleting and the like to the goods, the mails and the baggage.
Flight cargo hold information management component: the method can help the stowage personnel to comprehensively know the information of the flight cargo hold, and is an important way for the stowage personnel to distribute the position of the flight cargo; the flight cargo hold information comprises cargo hold layout drawing information, hold space information, cargo space information, allocated cargo mail luggage information and container information supported by an airplane; the cargo compartment layout map information comprises a container position, a container plate position, a cabin door position and a bulk cargo compartment position; the bin information comprises the name of the cargo hold, the current total weight of the cargo mail and the baggage of each cargo hold and the residual load capacity of each cargo hold; the cargo space information comprises a cargo space position name, the maximum cargo space capacity and a container type supported by the cargo space for the containerized airplane; the information of the distributed goods, mails and luggage comprises information of distributed goods, mails, cargo positions of the luggage, arrival stations, goods types, weights and the like, and for the containerized airplane, information of a container type, a container serial number and the like; the information of the containers supported by the aircraft is only aimed at the containerized aircraft and comprises the type of the container, the weight of the container and the maximum weight of the container.
Automatic trim subassembly: the assembly facilitates automatic allocation of cargo space by a stowage personnel for goods, mail, luggage and display of the allocated results.
The above components are specifically described below, where the embodiment in the description is only one possible implementation manner, and the present invention does not limit the forms of the specific display mode, the display frame, the trigger instruction, and the like as long as the functions in the embodiment of the present invention are implemented.
The flight basic information management component can display flight basic information and flight gravity center information for the stowage personnel, wherein the flight basic information is directly displayed in a text mode, and the flight gravity center information is displayed in a horizontal bar graph mode.
The specific implementation process of the imaging display of the flight center information may include:
(1) displaying the gravity center information of the ZFW/TOW/LAW in a horizontal bar graph mode, dividing the bar graph into a left part and a right part by using the current gravity center position value, wherein the bar graphs with different gravity centers have different colors, and displaying the FWDMAC value, the left bar graph, the MAC% value, the gravity center position value, the right bar graph and the AFTMAC value in sequence, wherein the DLW only displays the MAC% value;
(2) the calculation formula of the gravity center position value is as follows: the gravity center position value is (MAC% -FWDMAC)/(AFTMAC-FWDMAC), two decimal places are reserved as a result, when the gravity center position value is 0.5, the lengths of the front bar graph and the rear bar graph are equal, when the gravity center position value is less than 0.5, the length of the left bar graph is less than that of the right bar graph, and when the gravity center position value is greater than 0.5, the length of the left bar graph is greater than that of the right bar graph;
(3) if the position value of the center of gravity is larger than 1 or smaller than 0, the center of gravity of the flight is beyond the safety range, namely the MAC% value is not within the range of the (FWDMAC, AFTMAC) interval, at the moment, the color of the bar graph is changed, and the bar graph is used as early warning information to inform an operator that the center of gravity of the flight is beyond the safety range;
(4) if FWDMAC and AFTMAC are equal, the current barycentric position value cannot be calculated, and is not displayed at this time.
Flight cargo mail baggage information management component: the graphical information of the flight goods, the mails and the luggage can be displayed for the stowage personnel, and meanwhile, the stowage personnel can add, check and modify the flight goods, the mails and the luggage through the component, pull down and restore the goods and the mails, and delete the luggage;
the graphical display of the flight goods, mails and luggage information is realized by the following specific principle:
(1) the relevant information of goods, mails and luggage is described by the fields in the table 1.
TABLE 1
(2) Each cargo, mail, luggage, is displayed by a rectangular frame icon: each piece of goods, mails and luggage has a corresponding rectangular frame icon, main information of the goods, the mails or the luggage can be displayed in the rectangular frame icon, the main information comprises an arrival station three-character code, a goods type code, a goods predicted weight or actual weight and a special goods identifier, and for a containerized airplane, the type of a container used by the goods and a serial number of the container are further included.
(3) Setting an area as a ' Cargo column ', wherein the Cargo column ' comprises three label pages, namely a ' Cargo & Mail ' label page, a ' bag ' label page and a ' PullDown ' label page; the 'Cargo & Mail' tab page is specially used for storing goods and mails of goods positions to be allocated, and the corresponding rectangular frame icons are sequentially displayed on the 'Cargo & Mail' tab page; the 'bag' label page is specially used for storing luggage to be allocated with goods spaces, and the corresponding rectangular frame icons are sequentially displayed on the 'bag' label page; the "PullDown" tab is specially used for storing pulled-down goods and mails, and the corresponding rectangular frame icons are sequentially displayed on the "PullDown" tab.
The adding operation of the flight goods, the mails and the luggage is realized by the following steps:
(1) the 'cargo column' defines an 'ADD' button, clicks the button, pops up a dialog box, and displays blank cargo, mail and luggage information input dialog boxes;
(2) the information required by goods, mails and luggage is input by a fitter in an input dialog box, and comprises three-character codes of an arrival station, a goods type code, a goods predicted weight, a goods actual weight, a special goods identifier, a goods volume, whether the goods are the goods passing the station, a priority level, three-character codes of a final arrival station and the like, and for a containerized airplane, the information also comprises a container type used by the goods and a container serial number;
(3) after the input of the stowage person is finished, clicking a confirmation button, after the input data is verified, closing a dialog box, successfully adding the confirmation button, displaying newly added goods, mails and luggage without allocated goods positions in a 'goods bar', wherein rectangular box icons corresponding to the goods and the mails are added to a 'Cargo & Mail' label page, rectangular box icons corresponding to the luggage are added to a 'bag' label page, and the stowage person can click a cancel button or directly close the dialog box to cancel the newly added operation;
the operation of checking and modifying flight goods, mails and baggage is specifically realized by the following steps:
(1) the method comprises the steps that a 'View' button is defined in a rectangular frame icon corresponding to each piece of goods, mails and luggage, when a mouse is placed on the rectangular frame icon, the button is displayed, a dialogue box for editing the goods, the mails and the luggage is displayed by clicking the button, relevant information of the piece of goods, the mails and the luggage can be displayed in the dialogue box, the dialogue box comprises a three-character code of an arrival station, a goods type code, a goods predicted weight, an actual weight, a special goods identification, a goods volume, whether the goods are the goods which are in the station, a priority level, a three-character code of the final arrival station and the like, for a containerized airplane, a container type and a container serial number used by the goods are also included, and if the goods and the mails are pulled down, a pulling-down reason can;
(2) if the goods and the mails are pulled down, other information except the pulling-down reason cannot be modified, otherwise, the information of the goods, the mails and the luggage can be modified by the stowage assistant, the confirmation button is clicked after the modification is finished, the dialog box is closed after the input data is verified, the modification is successful, the information of the goods, the mails and the luggage displayed in the rectangular box icon is updated, and the stowage assistant can also click the cancel button or directly close the dialog box to cancel the modification;
the method for pulling down the flight goods and the mails comprises the following specific steps:
(1) goods and mails in a label page of 'Cargo & Mail' or goods and mails with goods and mails allocated with goods and mails, wherein the corresponding rectangular box icons define a 'PullDown' button, and when a mouse is placed on the rectangular box icon, the button is displayed, and is clicked to pop up a 'Reason' dialog box;
(2) the stowage person can input the pull-down Reason in the 'Reason' dialog box, after clicking the confirmation button, the goods and the mails can be pulled down to the 'PullDown' label page, namely the rectangular box icons corresponding to the goods and the mails disappear from the original positions and appear in the 'PullDown' label page of the goods column, and meanwhile, the pull-down Reason is added in the goods and the mails, and the stowage person can also click the cancel button or directly close the dialog box to cancel the pull-down operation;
the method for restoring the flight goods and the mails comprises the following specific implementation steps:
(1) the corresponding rectangular frame icons of goods and mails in the 'PullDown' tab page define a 'Recover' button, and when a mouse is placed on the rectangular frame icons, the button is displayed;
(2) after the fitter clicks the 'Recover' button, the goods and the mails can be restored to the 'Cargo & Mail' label page, namely the rectangular frame icons corresponding to the goods and the mails disappear from the original positions and appear in the 'Cargo & Mail' label page of the goods column;
the flight baggage deleting operation is implemented by the following steps:
(1) the corresponding rectangular box icons of the luggage in the tag page of the bag or the luggage with the allocated goods space define a 'Delete' button, when a mouse is placed on the rectangular box icon, the button is displayed, and is clicked to pop up a confirmation dialog box;
(2) after clicking the confirmation button, the stowage bin can be directly deleted, and meanwhile, the corresponding rectangular frame icon disappears from the original position, and the stowage bin can click the cancel button to cancel the deletion operation.
The flight cargo hold information management component can display graphical flight cargo hold information for a stowage person, wherein the flight cargo hold information comprises a cargo hold layout chart, cabin position information, cargo mail luggage information of an allocated cargo position, and for a containerized airplane, the flight cargo hold information management component also comprises container information supported by the airplane;
the display of the cargo compartment layout specifically realizes the following processes:
(1) the background of the system defines the layout information of the cargo hold, the layout information of the cargo hold can be used for knowing which positions the flight aircraft contains, which cargo space each position has, the position covered by each cargo space, the position name of the cargo space and the type of a container supported by the cargo space, according to the information, a large rectangular frame is drawn firstly to represent the whole cargo hold, the rectangular frame represents the cargo hold from left to right from top to bottom, and the rectangular frame represents the cargo hold from front to back from right to left; using a small rectangular frame to represent the cargo space, sequentially drawing small rectangular frames representing the cargo space in a large rectangular frame representing the whole cargo hold according to the position covered by the cargo space, and displaying the position name of the cargo space at the upper left corner of the small rectangular frame;
(2) the background of the system defines the single bottom diagram information of the patterning machine, the specific offset of each cargo space can be known from the single bottom diagram information of the patterning machine, the offset determines the width (length in the horizontal direction) of a small rectangular frame representing the cargo space, and the position drawn before is corrected according to the information; meanwhile, the single base map information of the patterning machine defines the position information of the airplane cabin door of the flight, and a thickened black line is used for representing the position of the airplane cabin door on the bottom frame of a large rectangular frame representing the whole cargo cabin according to the information;
the display of the cabin space information is realized by the following specific principle:
(1) drawing three rows of tables at the top of the cargo compartment layout, wherein the number of the columns of the tables is the number of the compartment positions, and each column of the tables corresponds to the compartment position marked in the cargo compartment layout;
(2) the first row of tables displays the names of the cargo holds, the second row of tables displays the current total weight of the cargos, the mails and the luggage in each cargo hold, and the third row of tables displays the residual load capacity of each cargo hold;
the goods position information display method comprises the following specific implementation steps:
(1) each small rectangle box representing the goods space is marked with a position name at the upper left corner, a mouse clicks the position name to pop up a dialog box,
(2) displaying the related information of the cargo space in a dialog box, wherein the related information comprises a position name, the maximum loading capacity of the cargo space, and a container type supported by the cargo space for a containerized airplane;
the display of the information of the goods, mails and luggage with the allocated goods space has the following specific realization principle:
(1) for the goods, mails and luggage with allocated goods positions, the corresponding rectangular frame icons can be displayed in the rectangular frames corresponding to the allocated goods positions
(2) The rectangular frame icons corresponding to goods, mails and luggage can adjust the width (length in the horizontal direction) of the rectangular frame icons according to the size of the goods space rectangular frame, if the width is narrowed after adjustment, a part of information can be shielded, at the moment, a mouse can be moved onto the icons, the icons can be unfolded, complete information can be seen, and meanwhile, operation buttons are displayed;
the display of the information of the container supported by the airplane comprises the following specific implementation steps:
(1) the "cargo bar" defines the "ULD-Info" button, which the loader clicks to pop up a "container Info" dialog;
(2) if the aircraft is a containerized aircraft, the type of the container supported by the aircraft, the weight of the container and the maximum weight of the container are displayed in a dialog box in a form of a table, and if the aircraft is a non-containerized aircraft, the aircraft is displayed to be empty.
The automatic balancing component can help a fitter to automatically allocate goods, mails and luggage of the cargo column according to the cargo space, and a specific implementation process can be shown in fig. 3.
The system main interface comprises an 'AutoLoad' drop-down list, a loader clicks the 'AutoLoad' drop-down box TO display four distribution strategies of 'Optimal distribution', 'Optimal BF' (Optimal distribution, luggage front compartment), 'F TO R' (front TO back distribution) and 'R TO F' (front TO back distribution), and the loader can select one of the options as required; the system can automatically allocate the cargos on the label page of 'Cargo & Mail' in the 'Cargo column', the mails and the luggage on the label page of 'bag' to each Cargo space of the Cargo hold according to the allocation strategy and the loading rule selected by the stowage person, display the allocated result in the Cargo hold layout drawing, update the allocated graphical gravity center information, if the system provides a plurality of allocation schemes, the arrow of 'next allocation scheme' can be displayed, if partial errors or all errors occur in the automatic allocation, an error prompt box is popped up, and the original interface is not changed; the fitter can select the current stowage scheme to be directly submitted, and can click on a 'next distribution scheme' arrow, and the system displays the distribution result of the next distribution scheme in the form of step 2 until the final submission is finished.
The allocation strategy refers to a goods space use sequence rule, and the specific implementation principle is as follows:
(1) formulating a cargo space using sequence principle: a. the principle of the average distribution of front and rear cargo holds; b. the principle of distribution from the middle of the cargo hold to both ends; c. the principle of filling one cabin first and then filling the other cabin;
(2) the three principles are in priority order, the priority levels are a, b and c from high to low, and the system defines an optimal distribution order for each machine type according to the three principles;
(3) in actual use, the system arranges the using sequence of the cargo space according TO the Optimal distribution sequence of the airplane of the flight and different distribution strategies selected by a user, if the Optimal distribution sequence is selected, the distribution process of the cargo is guided according TO the Optimal distribution sequence, if the Optimal distribution sequence is selected, the luggage is distributed in the front cabin TO guide the distribution process of the cargo, and if the F TO R is selected, the distribution process of the cargo is guided by adopting the sequence of distributing the front cabin first and distributing the rear cabin later; if "Rto F" is selected, the order of dividing the rear compartment first and then allocating the front compartment second will be used to guide the cargo allocation process.
Correspondingly, the loading rule refers to that the loading rule needs to be satisfied in the process of distributing goods, mails and luggage according to the distribution strategy, and specifically includes the following points:
(1) after the goods distribution is finished, the MAC% values of ZFW, TOW and LAW are ensured to be in a safe range;
(2) after the goods are matched, weight limit rules are satisfied, wherein the weight limit rules comprise combined weight limit (the combined weight of a plurality of positions cannot exceed a specified value), front and rear cabin weight limit (the weight of a front cabin and the weight of a rear cabin cannot exceed the specified value), cabin weight limit (the weight of each cabin cannot exceed the specified value), cargo space weight limit (the weight of each cargo space cannot exceed the specified value), and regional weight limit (the weight of a plurality of defined regions cannot exceed the specified value);
(3) after the goods distribution is finished, the volume of goods, mails and luggage in each cabin is ensured not to exceed the maximum allowable volume of the cabin;
(4) after the goods distribution is finished, the isolation rule of special goods is ensured;
(5) after the goods distribution is finished, the position of the luggage industry load is ensured to be closer to the cabin door than the position of the goods mail industry load, and meanwhile, the goods can not block the luggage, namely, the goods mail industry load can not block the luggage industry load;
(6) for multi-leg flights, after the distribution of goods is finished, the positions of goods, mails and luggage arriving at the station in the current leg are ensured to be closer to the cabin door, and the service loads of other arriving stations can not block the service loads of the current arriving station.
It is to be noted that the flowcharts and block diagrams in the figures referred to in the embodiments illustrate the architecture, functionality, and operation of possible implementations of systems, methods and computer program products according to various embodiments of the present disclosure. In this regard, each block in the flowchart or block diagrams may represent a module, segment, or portion of code, which comprises one or more executable instructions for implementing the specified logical function(s). It should also be noted that, in some alternative implementations, the functions noted in the block may occur out of the order noted in the figures. For example, two blocks shown in succession may, in fact, be executed substantially concurrently, or the blocks may sometimes be executed in the reverse order, depending upon the functionality involved. It will also be noted that each block of the block diagrams and/or flowchart illustration, and combinations of blocks in the block diagrams and/or flowchart illustration, can be implemented by special purpose hardware-based systems which perform the specified functions or acts, or combinations of special purpose hardware and computer instructions.
The names of messages or information exchanged between devices in the embodiments of the present disclosure are for illustrative purposes only, and are not intended to limit the scope of the messages or information. Although the operations are depicted in a particular order, this should not be understood as requiring that such operations be performed in the particular order shown or in sequential order. Under certain circumstances, multitasking and parallel processing may be advantageous. It should be understood that the various steps recited in the method embodiments of the present disclosure may be performed in a different order, and/or performed in parallel. Moreover, method embodiments may include additional steps and/or omit performing the illustrated steps. The scope of the present disclosure is not limited in this respect.
Referring to fig. 4, there is further provided in an embodiment of the present invention, an aircraft cargo compartment loading scheme generating apparatus, including:
the device comprises an acquisition unit 10, a storage unit and a processing unit, wherein the acquisition unit is used for acquiring information of articles to be loaded, and the articles to be loaded comprise one or more of cargos, mails and luggage;
a first generating unit 20, configured to generate at least one loading template based on the to-be-loaded item information, the cargo space layout map information, and preset loading conditions, where the loading conditions include one or more of weight limitation conditions, gravity limitation conditions, isolation conditions, and loading priority conditions, and the cargo space layout map information includes container positions, container plate positions, hatch door positions, and bulk cargo space positions;
a first determining unit 30 for determining an initial template in response to the selection of the loading template;
the second generating unit 40 is configured to generate visual loading display information according to the initial template and the information of the articles to be loaded;
a second determining unit 50, configured to determine the initial module as a target loading template if the visual loading display information is determined, so that the object to be loaded is loaded through the target loading template.
On the basis of the above embodiment, the apparatus further includes:
and the first adjusting unit is used for adjusting the initial template according to the adjusting information to obtain a target loading template if the visual loading display information is adjusted.
On the basis of the above embodiment, the apparatus further includes:
the second adjusting unit is used for obtaining a loading result of the to-be-loaded articles based on the adjusting information if the visual loading display information is adjusted;
and the judging unit is used for judging whether the loading result meets the preset loading condition or not, and if not, generating prompt information which is used for prompting that the adjustment information does not meet the loading condition.
On the basis of the above embodiment, the apparatus further includes:
the first information acquisition unit is used for acquiring airplane flight information corresponding to the information of the articles to be loaded;
and the third generating unit is used for generating flight display information according to the airplane flight information, wherein the flight display information comprises flight basic information and flight gravity center information, the flight basic information is displayed in a text format, and the flight center information is displayed in a graphic format.
On the basis of the above embodiment, the apparatus further includes:
the fourth generating unit is used for generating the display information of the articles to be loaded based on the information of the articles to be loaded, wherein the display information of the articles to be loaded comprises label information and description information;
the first receiving unit is used for receiving a modification instruction aiming at the information of the articles to be loaded, and modifying the display information of the articles to be loaded to obtain modified display information of the articles to be loaded, wherein the modification instruction comprises one or more of instructions for increasing, decreasing, checking and modifying the articles.
On the basis of the above embodiment, the apparatus further includes:
the second information acquisition unit is used for acquiring flight cargo space information based on the airplane flight information;
a fifth generating unit, configured to generate cargo hold display information corresponding to the flight cargo hold information, where the cargo hold display information includes a cargo hold layout diagram, hold information, and allocated hold information;
and the sixth generating unit is used for generating container information supported by the aircraft if the aircraft is a containerized aircraft.
On the basis of the above embodiment, the apparatus further includes:
a seventh generating unit, configured to generate a cargo allocation diagram for the information of the to-be-loaded cargo;
the second receiving unit is used for responding to the display of the acquired distribution schematic diagram and receiving a selection instruction of a user;
a third determining unit, configured to determine, if a selection instruction of a user is a determination instruction of the distribution schematic diagram, that the distribution schematic diagram is a loading scheme corresponding to the information of the to-be-loaded items;
and the eighth generating unit is used for generating a new cargo allocation schematic diagram if the cargo allocation schematic diagram is not generated.
The invention provides an aircraft cargo compartment loading scheme generation device, which is characterized in that information of articles to be loaded is acquired, at least one loading template is generated based on cargo compartment layout diagram information and preset loading conditions, visual loading display information can be generated in response to the selection of the loading template, if the information is determined, a corresponding target loading template is obtained, and the articles to be loaded are loaded through the target loading template. According to the invention, a plurality of loading templates are generated for the selection of the fitter, so that the professional requirements on the fitter, namely the labor cost is reduced, the loading efficiency is improved, and each loading condition is fully utilized, so that the loading is safer.
The units described in the embodiments of the present disclosure may be implemented by software or hardware. Where the name of an element does not in some cases constitute a limitation on the element itself.
In an embodiment of the present invention, there is also provided a storage medium having stored thereon executable instructions that, when executed by a processor, implement the aircraft cargo compartment loading scheme generation method as described in any one of the above.
An embodiment of the present invention further provides an electronic device, including:
a memory for storing a program;
a processor configured to execute the program, the program specifically configured to:
acquiring information of an article to be loaded, wherein the article to be loaded comprises one or more of goods, mails and luggage;
generating at least one loading template based on the to-be-installed article information, the cargo compartment layout map information and preset loading conditions, wherein the loading conditions comprise one or more of weight limitation conditions, gravity limitation conditions, isolation conditions and loading priority conditions, and the cargo compartment layout map information comprises container positions, container plate positions, cabin door positions and bulk compartment positions;
determining an initial template in response to the selection of the loading template;
generating visual loading display information according to the initial template and the information of the articles to be loaded;
and if the visual loading display information is determined, determining the initial module as a target loading template, so that the object to be loaded is loaded through the target loading template.
Further, the method further comprises:
and if the visual loading display information is adjusted, adjusting the initial template according to the adjustment information to obtain a target loading template.
Further, the method further comprises:
if the visual loading display information is adjusted, obtaining a loading result of the to-be-loaded article based on the adjustment information;
and judging whether the loading result meets the preset loading condition, if not, generating prompt information, wherein the prompt information is used for prompting that the adjustment information does not meet the loading condition.
Further, the method further comprises:
acquiring airplane flight information corresponding to the information of the articles to be loaded;
and generating flight display information according to the airplane flight information, wherein the flight display information comprises flight basic information and flight gravity center information, the flight basic information is displayed in a text format, and the flight center information is displayed in a graphic format.
Further, the method further comprises:
generating display information of the articles to be loaded based on the information of the articles to be loaded, wherein the display information of the articles to be loaded comprises label information and description information;
and receiving a modification instruction aiming at the information of the articles to be loaded, and modifying the display information of the articles to be loaded to obtain modified display information of the articles to be loaded, wherein the modification instruction comprises one or more of instructions for increasing, decreasing, checking and modifying the articles.
Further, the method further comprises:
acquiring flight cargo space information based on the airplane flight information;
generating cargo compartment display information corresponding to the flight cargo compartment information, wherein the cargo compartment display information comprises a cargo compartment layout chart, compartment position information, cargo position information and allocated cargo position information;
and if the aircraft is a containerized aircraft, generating container information supported by the aircraft.
Further, the method further comprises:
generating a cargo distribution schematic diagram for the information of the articles to be loaded;
responding to the display of the acquired distribution schematic diagram, and receiving a selection instruction of a user;
if the selection instruction of the user is a determination instruction of the distribution schematic diagram, determining that the distribution schematic diagram is a loading scheme corresponding to the information of the articles to be loaded;
otherwise, a new cargo allocation map is generated.
In the context of this disclosure, a machine-readable medium may be a tangible medium that can contain, or store a program for use by or in connection with an instruction execution system, apparatus, or device. The machine-readable medium may be a machine-readable signal medium or a machine-readable storage medium. A machine-readable medium may include, but is not limited to, an electronic, magnetic, optical, electromagnetic, infrared, or semiconductor system, apparatus, or device, or any suitable combination of the foregoing. More specific examples of a machine-readable storage medium would include an electrical connection based on one or more wires, a portable computer diskette, a hard disk, a Random Access Memory (RAM), a read-only memory (ROM), an erasable programmable read-only memory (EPROM or flash memory), an optical fiber, a portable compact disc read-only memory (CD-ROM), an optical storage device, a magnetic storage device, or any suitable combination of the foregoing.
According to one or more embodiments of the present disclosure, an information processing method, a system, a storage medium, and an electronic device for threat-oriented modeling are provided.
An aircraft cargo compartment loading scheme generation method comprising:
acquiring information of an article to be loaded, wherein the article to be loaded comprises one or more of goods, mails and luggage;
generating at least one loading template based on the to-be-installed article information, the cargo compartment layout map information and preset loading conditions, wherein the loading conditions comprise one or more of weight limitation conditions, gravity limitation conditions, isolation conditions and loading priority conditions, and the cargo compartment layout map information comprises container positions, container plate positions, cabin door positions and bulk compartment positions;
determining an initial template in response to the selection of the loading template;
generating visual loading display information according to the initial template and the information of the articles to be loaded;
and if the visual loading display information is determined, determining the initial module as a target loading template, so that the object to be loaded is loaded through the target loading template.
An aircraft cargo compartment loading solution generating apparatus comprising:
the device comprises an acquisition unit, a storage unit and a processing unit, wherein the acquisition unit is used for acquiring information of articles to be loaded, and the articles to be loaded comprise one or more of cargos, mails and luggage;
a first generating unit, configured to generate at least one loading template based on the to-be-loaded item information, the cargo space layout map information, and preset loading conditions, where the loading conditions include one or more of a weight limitation condition, a center-of-gravity limitation condition, an isolation condition, and a loading priority condition, and the cargo space layout map information includes a container position, a container panel position, a hatch door position, and a bulk cargo space position;
a first determining unit for determining an initial template in response to the selection of the loading template;
the second generation unit is used for generating visual loading display information according to the initial template and the information of the articles to be loaded;
and the second determining unit is used for determining the initial module as a target loading template if the visual loading display information is determined, so that the object to be loaded is loaded through the target loading template.
A storage medium having stored thereon executable instructions that, when executed by a processor, implement the aircraft cargo compartment loading scenario generation method of any of the above.
An electronic device, comprising:
a memory for storing a program;
a processor configured to execute the program, the program specifically configured to:
acquiring information of an article to be loaded, wherein the article to be loaded comprises one or more of goods, mails and luggage;
generating at least one loading template based on the to-be-installed article information, the cargo compartment layout map information and preset loading conditions, wherein the loading conditions comprise one or more of weight limitation conditions, gravity limitation conditions, isolation conditions and loading priority conditions, and the cargo compartment layout map information comprises container positions, container plate positions, cabin door positions and bulk compartment positions;
determining an initial template in response to the selection of the loading template;
generating visual loading display information according to the initial template and the information of the articles to be loaded;
and if the visual loading display information is determined, determining the initial module as a target loading template, so that the object to be loaded is loaded through the target loading template.
Although the subject matter has been described in language specific to structural features and/or methodological acts, it is to be understood that the subject matter defined in the appended claims is not necessarily limited to the specific features or acts described above. Rather, the specific features and acts described above are disclosed as example forms of implementing the claims.
While several specific implementation details are included in the above discussion, these should not be construed as limitations on the scope of the disclosure. Certain features that are described in the context of separate embodiments can also be implemented in combination in a single embodiment. Conversely, various features that are described in the context of a single embodiment can also be implemented in multiple embodiments separately or in any suitable subcombination.
The foregoing description is only exemplary of the preferred embodiments of the disclosure and is illustrative of the principles of the technology employed. It will be appreciated by those skilled in the art that the scope of the disclosure herein is not limited to the particular combination of features described above, but also encompasses other embodiments in which any combination of the features described above or their equivalents does not depart from the spirit of the disclosure. For example, the above features and (but not limited to) the features disclosed in this disclosure having similar functions are replaced with each other to form the technical solution.
Claims (10)
1. An aircraft cargo compartment loading plan generating method, comprising:
acquiring information of an article to be loaded, wherein the article to be loaded comprises one or more of goods, mails and luggage;
generating at least one loading template based on the to-be-installed article information, the cargo compartment layout map information and preset loading conditions, wherein the loading conditions comprise one or more of weight limitation conditions, gravity limitation conditions, isolation conditions and loading priority conditions, and the cargo compartment layout map information comprises container positions, container plate positions, cabin door positions and bulk compartment positions;
determining an initial template in response to the selection of the loading template;
generating visual loading display information according to the initial template and the information of the articles to be loaded;
and if the visual loading display information is determined, determining the initial module as a target loading template, so that the object to be loaded is loaded through the target loading template.
2. The method of claim 1, further comprising:
and if the visual loading display information is adjusted, adjusting the initial template according to the adjustment information to obtain a target loading template.
3. The method of claim 2, further comprising:
if the visual loading display information is adjusted, obtaining a loading result of the to-be-loaded article based on the adjustment information;
and judging whether the loading result meets the preset loading condition, if not, generating prompt information, wherein the prompt information is used for prompting that the adjustment information does not meet the loading condition.
4. The method of claim 1, further comprising:
acquiring airplane flight information corresponding to the information of the articles to be loaded;
and generating flight display information according to the airplane flight information, wherein the flight display information comprises flight basic information and flight gravity center information, the flight basic information is displayed in a text format, and the flight center information is displayed in a graphic format.
5. The method of claim 1, further comprising:
generating display information of the articles to be loaded based on the information of the articles to be loaded, wherein the display information of the articles to be loaded comprises label information and description information;
and receiving a modification instruction aiming at the information of the articles to be loaded, and modifying the display information of the articles to be loaded to obtain modified display information of the articles to be loaded, wherein the modification instruction comprises one or more of instructions for increasing, decreasing, checking and modifying the articles.
6. The method of claim 4, further comprising:
acquiring flight cargo space information based on the airplane flight information;
generating cargo compartment display information corresponding to the flight cargo compartment information, wherein the cargo compartment display information comprises a cargo compartment layout chart, compartment position information, cargo position information and allocated cargo position information;
and if the aircraft is a containerized aircraft, generating container information supported by the aircraft.
7. The method of claim 1, further comprising:
generating a cargo distribution schematic diagram for the information of the articles to be loaded;
responding to the display of the acquired distribution schematic diagram, and receiving a selection instruction of a user;
if the selection instruction of the user is a determination instruction of the distribution schematic diagram, determining that the distribution schematic diagram is a loading scheme corresponding to the information of the articles to be loaded;
otherwise, a new cargo allocation map is generated.
8. An aircraft cargo compartment loading solution creating apparatus comprising:
the device comprises an acquisition unit, a storage unit and a processing unit, wherein the acquisition unit is used for acquiring information of articles to be loaded, and the articles to be loaded comprise one or more of cargos, mails and luggage;
a first generating unit, configured to generate at least one loading template based on the to-be-loaded item information, the cargo space layout map information, and preset loading conditions, where the loading conditions include one or more of a weight limitation condition, a center-of-gravity limitation condition, an isolation condition, and a loading priority condition, and the cargo space layout map information includes a container position, a container panel position, a hatch door position, and a bulk cargo space position;
a first determining unit for determining an initial template in response to the selection of the loading template;
the second generation unit is used for generating visual loading display information according to the initial template and the information of the articles to be loaded;
and the second determining unit is used for determining the initial module as a target loading template if the visual loading display information is determined, so that the object to be loaded is loaded through the target loading template.
9. A storage medium having stored thereon executable instructions which, when executed by a processor, carry out a method of generating an aircraft cargo compartment loading scheme according to any one of claims 1 to 7.
10. An electronic device, comprising:
a memory for storing a program;
a processor configured to execute the program, the program specifically configured to:
acquiring information of an article to be loaded, wherein the article to be loaded comprises one or more of goods, mails and luggage;
generating at least one loading template based on the to-be-installed article information, the cargo compartment layout map information and preset loading conditions, wherein the loading conditions comprise one or more of weight limitation conditions, gravity limitation conditions, isolation conditions and loading priority conditions, and the cargo compartment layout map information comprises container positions, container plate positions, cabin door positions and bulk compartment positions;
determining an initial template in response to the selection of the loading template;
generating visual loading display information according to the initial template and the information of the articles to be loaded;
and if the visual loading display information is determined, determining the initial module as a target loading template, so that the object to be loaded is loaded through the target loading template.
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| CN202011084504.8A CN112184121A (en) | 2020-10-12 | 2020-10-12 | Method and device for generating loading scheme of aircraft cargo compartment and electronic equipment |
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| CN115796502B (en) * | 2022-11-22 | 2024-03-08 | 中国民航信息网络股份有限公司 | Load balancing control method and device for cargo hold and computer readable medium |
| CN116308974A (en) * | 2023-05-25 | 2023-06-23 | 中国民航信息网络股份有限公司 | Unloading information generation method and device and electronic equipment |
| CN116308974B (en) * | 2023-05-25 | 2024-03-01 | 中国民航信息网络股份有限公司 | Unloading information generation method and device and electronic equipment |
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