System and method for performing vehicle interior configuration design

• US 20020161563A1
• Filed: 03/13/2002
• Published: 10/31/2002
• Est. Priority Date: 03/13/2001
• Status: Abandoned Application

• Current Assignee: Bombardier Incorporated
• Original Assignee: Bombardier Incorporated
• Inventors: Vick, Shawn W., Elabiad, Naji
• Application Number:
  US10/096,249
• Publication Number:
  US 20020161563A1
• Time in Patent Office: Days
• US Class Current: 703/8
• CPC Class Codes: G06F 30/15 Vehicle, aircraft or watercraft design

Abstract

A system for designing the interior configuration of a vehicle, where the vehicle is characterized by a vehicle type. The system includes a data storage unit storing a plurality of predetermined validation criteria. A processing unit is operative to generate an aircraft interior configuration design on a basis of the aircraft type. In response to design instructions received from the system user, the processing unit modifies the aircraft interior configuration design accordingly and performs a validation operation on each design instruction, at least in part on the basis of the contents of the data storage unit.

Claims

1. A system for designing the interior configuration of a vehicle, the vehicle characterized by a vehicle type, said system comprising;

a) an input for receiving design instructions from a system user;

b) a data storage unit storing a plurality of predetermined validation criteria associated with the vehicle type;

c) a processing unit coupled to said data storage unit, said processing unit being operative to;

i) generate a vehicle interior configuration design on a basis of the vehicle type;

ii) modify said vehicle interior configuration design in response to design instructions received from the system user;

iii) attempt to validate each design instruction at least in part on the basis of the contents of said data storage unit.

2. A system as defined in claim 1, wherein said vehicle interior configuration design includes a spatial arrangement of a plurality of vehicle modules.

3. A system as defined in claim 2, wherein the vehicle is an aircraft, said vehicle interior configuration design being an aircraft interior configuration design, said vehicle modules being aircraft modules.

4. A system as defined in claim 3, wherein said plurality of aircraft modules are selected from the group consisting of furniture, cabinets, trim schemes, paint schemes, aircraft accessories, and service options.

5. A system as defined in claim 3, wherein said plurality of aircraft modules are selected from the group consisting of seats, galleys, wardrobes, lavatories, credenzas, material, woodwork, paint schemes, aircraft accessories, warranty requirements, training requirements, interim aircraft lift requirements, trade-in requirements, payment terms and concessions.

6. A system as defined in claim 3, wherein said processing unit includes a design unit for generating said aircraft interior configuration design, said design unit including a set of aircraft interior configuration models, each model being associated with a particular aircraft type.

7. A system as defined in claim 6, wherein said design unit consults said set of aircraft interior configuration models on the basis of the aircraft type for generating said aircraft interior configuration design.

8. A system as defined in claim 7, wherein said design unit is responsive to the design instructions received from the system user for modifying said aircraft interior configuration design.

9. A system as defined in claim 8, wherein said design instructions are selected from the group consisting of displacing an aircraft module, removing an aircraft module, adding an aircraft module, modifying an aircraft module.

10. A system as defined in claim 9, wherein said predetermined validation criteria include certification rules for a plurality of different aircraft types.

11. A system as defined in claim 10, wherein said predetermined validation criteria include safety standards for a plurality of different aircraft types.

12. A system as defined in claim 11, wherein said predetermined validation criteria include performance targets for a plurality of different aircraft types.

13. A system as defined in claim 11, wherein said predetermined validation criteria include financial targets for a plurality of different aircraft types.

14. A system as defined in claim 11, wherein said predetermined validation criteria include delivery targets for a plurality of different aircraft types.

15. A system as defined in claim 11, wherein said predetermined validation criteria include manufacturing targets for a plurality of different aircraft types.

16. A system as defined in claim 12, wherein said processing unit includes a validation unit for attempting to validate each design instruction submitted by the system user.

17. A system as defined in claim 16, wherein said validation unit consults the validation criteria stored in said database for attempting to validate a design instruction.

18. A system as defined in claim 17, wherein if a particular design instruction violates one or more of the validation criteria stored in said database, said validation unit determines that the particular design instruction is invalid.

19. A system as defined in claim 18, whereby if a particular design instruction is invalid said validation unit generates a violation message for transmission to the system user, the violation message including an indication of the particular design instruction that is invalid.

20. A system as defined in claim 12, wherein said processing unit includes an evaluator unit for evaluating a plurality of project targets in response to each design instruction received from the system user.

21. A system as defined in claim 20, wherein said evaluator unit is operative to perform measurement calculation operations.

22. A system as defined in claim 21, wherein said project targets are selected from the group consisting of performance targets, financial targets, delivery targets and manufacturing targets.

23. A system as defined in claim 22, wherein said measurement calculation operations are selected from the group consisting of aircraft weight measurements, aircraft range measurements, delivery schedule determination and financial value calculations.

24. A system as defined in claim 1, wherein said system receives at said input an input signal from the system user specifying the vehicle type.

25. A system as defined in claim 24, wherein said input signal conveys the vehicle type.

26. A system as defined in claim 1, wherein said processing unit is further operative to transmit said vehicle interior configuration design to the system user.

27. A system as defined in claim 26, wherein said vehicle interior configuration design is in a graphical form.

28. A system as defined in claim 26, wherein said vehicle interior configuration design is in a textual form.

29. A system as defined in claim 1, wherein said system is implemented in software on a computing platform.

30. A system as defined in claim 29, wherein the computing platform is a workstation.

31. A system as defined in claim 29, wherein the computing platform is a laptop.

32. A system as defined in claim 29, wherein the computing platform uses Pentium technology.

33. A system as defined in claim 1, wherein said data storage unit is a computer-readable database.

34. A machine readable storage medium containing program instructions for execution on a computing device to implement a system for designing the interior configuration of a vehicle, the vehicle characterized by a vehicle type, said system comprising:

a) an input for receiving design instructions from a system user;

b) a data storage unit storing a plurality of predetermined validation criteria associated with the vehicle type;

c) a processing unit coupled to said data storage unit, said processing unit being operative to;

i) generate a vehicle interior configuration design on a basis of the vehicle type;

ii) modify said vehicle interior configuration design in response to the design instructions received from the system user; and

iii) attempt to validate each design instruction received from the system user at least in part on the basis of the contents of said data storage unit.

35. A method for designing the interior configuration of a vehicle, the vehicle characterized by a vehicle type, said method comprising:

a) storing a plurality of predetermined validation criteria associated with the vehicle type;

b) receiving design instructions from a system user;

c) generating a vehicle interior configuration design on a basis of the vehicle type;

d) modifying the vehicle interior configuration design in response to the design instructions received from the system user;

e) attempting to validate each design instruction at least in part on the basis of the validation criteria.

36. A system for designing the interior configuration of a vehicle, the vehicle characterized by a vehicle type, said system comprising:

a) an input for receiving design instructions from a system user;

b) a data storage unit storing a plurality of predetermined validation criteria associated with the vehicle type;

c) a processing unit coupled to said data storage unit, said processing unit being operative to;

i) generate a vehicle interior configuration design on a basis of the vehicle type;

ii) attempt to validate each design instruction at least in part on the basis of the contents of said data storage unit;

iii) modify said vehicle interior configuration design in response to validated design instructions.

37. A vehicle configurator device for configuring the interior of a vehicle, the vehicle characterized by a vehicle type, said vehicle configurator device being in data communication with a database storing a plurality of predetermined validation criteria, said vehicle configurator device comprising:

a) an input for receiving design instructions from a system user;

b) a design unit coupled to said input, said design unit operative to generate a vehicle interior configuration design on the basis of the aircraft type, said design unit being responsive to design instructions received from the system user for modifying said vehicle interior configuration design;

c) a validation unit coupled to said design unit, said validation unit operative to attempt to validate each design instruction received from the system user at least in part on the basis of the contents of the database.

38. An aircraft configurator device for configuring the interior of an aircraft, the aircraft being characterized by an aircraft type, said aircraft configurator device in data communication with a database storing a plurality of predetermined aircraft specifications, said aircraft configurator device comprising:

a) an input for receiving design instructions from the system user;

b) a controller unit;

c) a memory in data communicative relationship with said controller unit;

d) a program element in said memory that is executed by said controller unit for;

i) generating an aircraft interior configuration design on the basis of the aircraft type;

ii) modifying said aircraft interior configuration design in response to the design instructions received from the system user;

iii) performing a validation operation on each design instruction at least in part on the basis of the contents of the data storage unit.