Patent Application
20130246008
The subject matter described herein relates to airflow modeling in confined spaces and more particularly to computer-based systems and methods for airflow modeling of cabins. Vehicles such as commercial air, marine and land vehicles may include one or more cabins to house crew, passengers and/or cargo. Owners and operators of such vehicles may specify varying cabin configurations to accommodate different types of travel and different classes of passengers, branding, and the like.
For example, commercial aircraft may include a cockpit, passenger cabin, and a storage compartment. The passenger cabin may be divided into a first-class section, business class section, and an economy section. As part of the design process, aircraft designers and engineers may need to model airflow parameters through the cabin for health and safety reasons. Accordingly, systems and methods for cabin airflow modeling may find utility.
Embodiments of systems and methods in accordance with the present disclosure may provide improved cabin airflow modeling. In one embodiment, a computer based method to model airflow dynamics in a controlled cabin environment comprises creating a data store comprising a template of the controlled cabin environment and a plurality of logical objects which represent physical objects, wherein the logical objects comprise airflow characteristics associated therewith, constructing a two-dimensional layout of the cabin environment, and generating, from the two-dimensional layout of the cabin environment, a script to construct a three-dimensional airflow model for the cabin environment.
In one embodiment, a computer based system to model airflow dynamics in a controlled cabin environment, comprises a data store in a tangible computer readable memory which stores a template of the controlled cabin environment and a plurality of logical objects which represent physical objects, wherein the logical objects comprise airflow characteristics associated therewith and a processor to construct a two-dimensional layout of the cabin environment, and generate, from the two-dimensional layout of the cabin environment, a script to construct a three-dimensional airflow model for the cabin environment.
Further areas of applicability will become apparent from the description provided herein. It should be understood that the description and specific examples are intended for purposes of illustration only and are not intended to limit the scope of the present disclosure.
Embodiments of methods and systems in accordance with the teachings of the present disclosure are described in detail below with reference to the following drawings.
Systems and methods for cabin airflow modeling are described herein. Specific details of certain embodiments are set forth in the following description and in
In the context of an aircraft, cabin template data store 110 may comprise one or more templates for layouts for a specific aircraft associated with aircraft data such as, e.g., an aircraft identifier, data pertaining to the aircraft operator, flight operations, and data related to one or more of the aircraft systems. The cabin layout module 122, the script generator module 124, the data parser/loader 150, and the reporting module 152 may be implemented as logic instructions stored on a computer readable medium and executable by a processor, e.g., software.
In some embodiments the various data stores 110, 112 may be implemented as databases or as flat files stored on a computer readable medium. The cabin template 110 may be used to store various aircraft cabin layouts, while the logical object database 112 may be used to store logical objects which represent physical objects that reside in an aircraft cabin. By way of example, logical objects may include fixtures such as seats, partitions, walls, stationary and mobile galley equipment, luggage equipment, occupants (i.e. passengers and crew), and the like. Logical objects may further include systems such as ventilation and airflow systems. Logical objects may further include human or animal objects. The data in databases 110 and 112 may be stored in a suitable computer readable storage medium, e.g., a magnetic storage medium, an optical storage medium, or combinations thereof.
The modeling script 140 and the execution environment 142 may be embodied as modular components which are functionally separate from the configuration module 120. In some embodiments the modeling script 140 may be implemented as logic instructions encoded in a computer readable medium and executable on a processor. By way of example, in one embodiment the execution environment 142 may comprise hardware and software on which the modeling script may be executed.
In some embodiments the simulation(s) 146 may be used to simulate air flow modeling under varying cabin configurations and conditions in accordance with one or more predetermined models. The simulation(s) 146 may utilize parameters provided by a user of the system or derived from operational data for an aircraft fleet as inputs. The simulation(s) 146 may interface with a reporting module 152, which may create one or more reports 154 accessible via a user interface 160.
In some embodiments the system depicted in
The computing device 208 includes system hardware 220 and memory 230, which may be implemented as random access memory and/or read-only memory. A file store 280 may be communicatively coupled to computing device 208. File store 280 may be internal to computing device 208 such as, e.g., one or more hard drives, CD-ROM drives, DVD-ROM drives, or other types of storage devices. File store 280 may also be external to computer 208 such as, e.g., one or more external hard drives, network attached storage, or a separate storage network.
System hardware 220 may include one or more processors 222, a two graphics processor(s) 224, network interfaces 226, and bus structures 228. As used herein, the term “processor” means any type of computational element, such as but not limited to, a microprocessor, a microcontroller, a complex instruction set computing (CISC) microprocessor, a reduced instruction set (RISC) microprocessor, a very long instruction word (VLIW) microprocessor, or any other type of processor or processing circuit.
Graphics processor(s) 224 may function as adjunct processors that manage graphics and/or video operations. Graphics processor(s) 224 may be integrated onto the motherboard of computing system 400 or may be coupled via an expansion slot on the motherboard.
In one embodiment, network interface 226 could be a wired interface such as an Ethernet interface (see, e.g., Institute of Electrical and Electronics Engineers/IEEE 802.3-2002) or a wireless interface such as an IEEE 802.11a, b or g-compliant interface (see, e.g., IEEE Standard for IT-Telecommunications and information exchange between systems LAN/MAN—Part II: Wireless LAN Medium Access Control (MAC) and Physical Layer (PHY) specifications Amendment 4: Further Higher Data Rate Extension in the 2.4 GHz Band, 802.11G-2003). Another example of a wireless interface would be a general packet radio service (GPRS) interface (see, e.g., Guidelines on GPRS Handset Requirements, Global System for Mobile Communications/GSM Association, Ver. 3.0.1, December 2002).
Bus structures 228 connect various components of system hardware 228. In one embodiment, bus structures 228 may be one or more of several types of bus structure(s) including a memory bus, a peripheral bus or external bus, and/or a local bus using any variety of available bus architectures including, but not limited to, 11-bit bus, Industrial Standard Architecture (ISA), Micro-Channel Architecture (MSA), Extended ISA (EISA), Intelligent Drive Electronics (IDE), VESA Local Bus (VLB), Peripheral Component Interconnect (PCI), Universal Serial Bus (USB), Advanced Graphics Port (AGP), Personal Computer Memory Card International Association bus (PCMCIA), and Small Computer Systems Interface (SCSI).
Memory 230 may include an operating system 240 for managing operations of computing device 208. In one embodiment, operating system 240 includes a hardware interface module 254 that provides an interface to system hardware 220. In addition, operating system 240 may include a file system 250 that manages files used in the operation of computing device 208 and a process control subsystem 252 that manages processes executing on computing device 208.
Operating system 240 may include (or manage) one or more communication interfaces that may operate in conjunction with system hardware 220 to transceive data packets and/or data streams from a remote source. Operating system 240 may further include a system call interface module 242 that provides an interface between the operating system 240 and one or more application modules resident in memory 230. Operating system 240 may be embodied as a Windows® brand operating system or as a UNIX operating system or any derivative thereof (e.g., Linux, Solaris, etc.), or other operating systems.
In various embodiments, the computing device 208 may be embodied as a computer system such as a personal computer, a laptop computer, a server, or another computing device.
In one embodiment, memory 230 includes a cabin layout module 122, a script generator module 124, one or more simulation modules 146, and a reporting module 152 to implement the operations described with reference to
At operation 310 an aircraft cabin may be selected. By way of example, in some embodiments one or more aircraft types may be presented on a user interface 104 and one or more users of the system 100 may select an aircraft cabin from the choices presented on the user interface 104. The aircraft cabin template for the selected aircraft cabin may be retrieved from the data store and presented on the user interface for manipulation and configuration.
At operation 315 a two-dimensional internal configuration for the selected aircraft is constructed. By way of example, in some embodiments one or more logical objects may be retrieved from the logical object data store 112 and positioned in the cabin template selected in operation 310. As described above, in some embodiments the cabin configuration may define the dimensions of various cabin measurements and fixture such as exit doors 402. Logical objects may represent the lavatories 404, galley fixtures 406, first class seats 408 and economy seats 410. Additional logical objects may be added to represent overhead luggage compartments and airflow systems not visible in the floor plan view depicted in
The various logical objects have physical properties associated with them. By way of example, the objects may have physical dimensions and shapes associated with them. In addition, a user may specify one or more physical and material properties such as, e.g., airflow rates, angles, temperatures, heat flux parameters, viscosity and thermal conductivity of fluids, etc., associated with the objects.
In some embodiments the various logical objects may be added to the template using a drag and drop technique. By way of example, logical objects stored in the logical object data store 112 may be represented by icons which may be selected, dragged and dropped onto the template in desired positions and quantities. As the graphical user interface is populated the system generates a file structure 420 corresponding to the layout.
A user of the system may populate one or more of the seats with a human object. A human object may have physical characteristics associated with it, e.g., height weight, shape, etc., and may have airflow characteristics associated with them. In addition, human objects may be assigned a mobile capability in which an object can move about aisles in the cabin.
In some embodiments the user interface allows a user to generate a three-dimensional view of the cabin. The three dimensional view may be viewed from various perspectives to evaluate the cabin layout.
Referring back to
At operation 330 results of the simulation may be presented to a user of the system. By way of example, referring back to
Thus, described herein is a computer based system and method for cabin airflow modeling. In brief, the system enables a user to select a two-dimensional cabin template and design a cabin layout by populating the template with objects. The two-dimensional module may then be used to construct a three-dimensional CFD model, which may be input to a simulation processor.
In the foregoing discussion, specific implementations of exemplary processes have been described, however, it should be understood that in alternate implementation, certain acts need not be performed in the order described above. In alternate embodiments, some acts may be modified, performed in a different order, or may be omitted entirely, depending on the circumstances. Moreover, in various alternate implementations, the acts described may be implemented by a computer, controller, processor, programmable device, firmware, or any other suitable device, and may be based on instructions stored on one or more computer-readable media or otherwise stored or programmed into such devices (e.g. including transmitting computer-readable instructions in real time to such devices). In the context of software, the acts described above may represent computer instructions that, when executed by one or more processors, perform the recited operations. In the event that computer-readable media are used, the computer-readable media can be any available media that can be accessed by a device to implement the instructions stored thereon.
While various embodiments have been described, those skilled in the art will recognize modifications or variations which might be made without departing from the present disclosure. The examples illustrate the various embodiments and are not intended to limit the present disclosure. Therefore, the description and claims should be interpreted liberally with only such limitation as is necessary in view of the pertinent prior art.
