IP Library Granted Patent US 7,623,996
Granted Patent B1
US 7,623,996 · App. 11/256,534 · Granted Nov 24, 2009

Mass morphing system and method

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Quick Facts
Patent No.
US 7,623,996
App. No.
11/256,534
Granted
Nov 24, 2009
Kind
B1
Abstract

Disclosed is a system and process for creating mass property models for new product designs. Engineers are able to use this robust model to perform various assessments. The system morphs legacy mass property values into new design project configurations. This is done by building linear transformations in four-dimensional homogeneous coordinates. The transformations capture source and target geometric characteristic shapes. Filtering techniques are used to retrieve relevant source mass properties from the database. These detailed mass properties are collected into bay wise functional groups and then converted to equivalent mass particulates. These point masses are transformed from the source domain to the target domain, and summed back together to generate target mass property data. The process outputs detailed mass property distributions used in engineering models and reports and is continually updated to accommodate detailed designs throughout project development.

Claims (47)

1. A system for generating a mass-property model of a target aircraft design comprising:

a digital processor;

a process controlled by the digital processor for implementing steps comprising:

extracting mass properties regarding a source aircraft design from a database;

establishing source homogenous coordinates defining at least one discrete source bay;

incorporating said source homogenous coordinates into a source matrix;

using target homogeneous coordinates defining at least one target bay;

incorporating said target homogenous coordinates into a target matrix;

calculating a transformation matrix using said source matrix and said target matrix to generate transformed source coordinates and target coordinates;

converging said transformation matrix for transformations to minimize differences between the transformed source coordinates and the target coordinates, wherein said converging comprises:

setting a fourth dimensional element of each homogeneous coordinate to unity in said source matrix;

initializing a fourth dimensional element in said target matrix at unity; and

repeatedly changing the value of said fourth dimensional element in said target matrix until normalization is achieved;

using the source homogenous coordinates and the target homogeneous coordinates to generate new target coordinates;

morphing source mass property information into target mass property information using said new target coordinates to generate the mass-property model; and

generating a report including characteristics of the mass-property model.

2. The system of claim 1 comprising:

performing a least squares fit in generating said target coordinate system.

3. The system of claim 1 including:

using the system to perform one of taper, translational, rotational, shearing, and scaling transformations.

4. The system of claim 1 comprising:

manipulating target base geometry directly from parametric spreadsheet input.

5. The system of claim 1 comprising:

using box geometries to comprise each of said source and target bays;

using each of said source homogeneous coordinates as a control point at one corner of a source box; and

using each of said target homogeneous coordinates as a control point at one corner of a target box.

6. The system of claim 1 wherein said system generates said model of one of centers of gravity, weights, and moments of inertia of the target design.

7. The system of claim 1 comprising:

reducing source inertial data into equivalent point mass representations so that said source inertial data is useable in said morphing step.

8. The system of claim 1 comprising:

calculating the offsets of mass points relative to the center of gravity given moments of inertia and the products of inertia; and

scaling mass using said offsets.

9. A system for generating a mass property model for a target product design comprising:

a digital processor executing instructions for:

extracting legacy mass properties information regarding a source product design from a legacy database;

defining a plurality of discrete source bays which together substantially represent said source product geometry;

using said plurality of source bay coordinates and said plurality of target bay coordinates to determine a transform;

using said transform to generate transformed target geometries;

using said transformed target geometries for making source to target mass property transformations to generate the mass property model; and

generating a report including characteristics of the mass-property model.

10. The system of claim 9 comprising:

reducing source inertial data into equivalent point mass representations before making said target mass property transformations.

11. The system of claim 9 comprising:

calculating offsets of mass points relative to the center of gravity given moments of inertia and the products of inertia; and

scaling target product mass using said offsets.

12. The system of claim 9 , wherein said method is adapted to use box geometries to comprise source and target bays, use source homogeneous coordinates as a control points at each corner of a source box, use target homogeneous coordinates as a control points at each corner of a target box, and create linear transformations to generate target geometries for the mass property model.

13. The system of claim 9 , wherein said legacy database is organized such that functional part groups are coded in a hierarchal fashion; wherein parent/child code relationships are organized via a tree structure with the top of the tree representing the complete target product.

Assignments (3)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Feb 10, 2009
From: CESSNA AIRCRAFT RHODE ISLAND INC.
To: TEXTRON INNOVATIONS INC.
Reel/Frame 022231/0908 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jan 22, 2009
From: CESSNA AIRCRAFT COMPANY
To: CESSNA AIRCRAFT RHODE ISLAND INC.
Reel/Frame 022137/0033 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Oct 21, 2005
From: BEYER, MARK E.
To: CESSNA AIRCRAFT COMPANY
Reel/Frame 017141/0729 →