IP Library Granted Patent US 8,983,801
Granted Patent B2
US 8,983,801 · App. 12/428,983 · Granted Mar 17, 2015

Method and system for transforming a CAD model of an object between engineering states

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Quick Facts
Patent No.
US 8,983,801
App. No.
12/428,983
Granted
Mar 17, 2015
Kind
B2
Abstract

In one embodiment, a computer-implemented method for transforming a CAD model of an object between engineering states includes generating a first reference geometry to represent a first engineering state. A parametric CAD model of the object may be generated to represent the object in the first engineering state by constructing the parametric CAD model as having dependence on the first reference geometry. A second reference geometry may be generated to represent a second engineering state. The parametric CAD model may be regenerated to represent the object in the second engineering state by replacing the first reference geometry with the second reference geometry.

Claims (54)

1. A computer-implemented method for transforming a CAD model of an object between engineering states, comprising:

generating a first reference geometry representing a final engineering state of an object, wherein the first reference geometry comprises a first surface and a second surface, the first surface and the second surface intersecting to form a first reference curve;

constructing a parametric CAD model of the object, the parametric CAD model representing the object in the final engineering state, the parametric CAD model of the object having dependence on the first reference geometry, the parametric CAD model of the object having a top surface both located on the second surface and having, a curvature of the second surface, the parametric CAD model of the object further having a bottom surface both located a first distance from the second surface and having a curvature of the second surface;

defining a fixed reference point on the first reference curve, the fixed reference point being located a second distance from an end of the first reference curve;

generating a second reference geometry representing a flat manufacturing state, wherein the second reference geometry comprises a third surface and a fourth surface, the third surface and the fourth surface intersecting to form a second reference curve;

using a computer system, regenerating the parametric CAD model to represent the object in the flat manufacturing state by:

inserting the third surface and the fourth surface into the parametric CAD Model;

replacing the first surface with the third surface and replacing the second surface with the fourth surface; and

defining the fixed reference point on the second reference curve as being located the second distance from an end of the second reference curve.

2. A computer-implemented method for transforming a CAD model of an object between engineering states, comprising:

generating a first reference geometry representing a first engineering state; wherein the first reference geometry comprises a first surface and a second surface, the first surface and the second surface intersecting to form a first reference curve;

constructing a parametric CAD model of an object, the parametric CAD model representing the object in the first engineering state, the parametric CAD model having dependence on the first reference geometry; the parametric CAD model of the object having a top surface both located on the second surface and having a curvature of the second surface, the parametric CAD model of the object further having a bottom surface both located a first distance from the second surface and having a curvature of the second surface;

defining a fixed reference point on the first reference curve, the fixed reference point being located a second distance from an end of the first reference curve;

generating a second reference geometry representing a second engineering state, wherein the second reference geometry comprises a third surface and a fourth surface, the third surface and the fourth surface intersecting to form a second reference curve;

using a computer system, regenerating the parametric CAD model to represent the object in the second engineering state by:

inserting the third surface and the fourth surface into the parametric CAD Model;

replacing the first surface with the third surface and replacing the second surface with the fourth surface; and

defining the fixed reference point on the second reference curve as being located the second distance from an end of the second reference curve.

3. The method of claim 2 , wherein:

the first engineering state represents a condition of the object in a final engineering state; and

the second engineering state represents a condition of the object in a flat manufacturing state.

4. The method of claim 2 , further comprising adjusting a length of the second reference curve to approximate a length of the first reference curve.

5. The method of claim 2 , wherein the defining a fixed reference point on the first reference curve further comprises:

determining an intersection between the first reference curve and a reference plane; and

defining the fixed reference point as a point on the reference curve without dependence on the reference plane.

6. The method of claim 2 , further comprising:

determining an intersection between the first reference curve and a reference plane; and

identifying a reference coordinate system formed by an intersection of the reference plane and the first surface, an intersection of the reference plane and the second surface, and the first reference curve.

7. The method of claim 2 , wherein:

generating a second reference geometry representing a second engineering state comprises generating the second reference geometry in an off-line CAD file; and

importing the second reference geometry into the parametric CAD Model.

8. A non-transitory machine-readable storage medium having logic stored thereon and operable, when executed on a processor, to:

store a parametric CAD model of an object, the parametric CAD model representing the object in a first engineering state, wherein:

a first reference geometry represents the first engineering state wherein the first reference geometry comprises a first surface and a second surface, the first surface and the second surface intersecting to form a first reference curve;, and

the parametric CAD model is dependent on the first reference geometry, the parametric CAD model of the object having a top surface both located on the second surface and having a curvature of the second surface, the parametric CAD model of the object further having a bottom surface both located a first distance from the second surface and having a curvature of the second surface;; and

regenerate the parametric CAD model to represent the object in a second engineering state by:

defining a fixed reference point on the first reference curve, the fixed reference point being located a second distance from an end of the first reference curve;

generating a second reference geometry representing the object in the second engineering state, wherein the second reference geometry comprises a third surface and a fourth surface, the third surface and the fourth surface intersecting to form a second reference curve;

inserting the third surface and the fourth surface into the parametric CAD Model;

replacing the first surface with the third surface and replacing the second surface with the fourth surface; and

defining the fixed reference point on the second reference curve as being located the second distance from an end of the second reference curve.

9. The non-transitory machine-readable storage medium of claim 8 , wherein:

the first engineering state represents the condition of the object in a final engineering state; and

the second engineering state represents the condition of the object in a flat manufacturing state.

10. The non-transitory machine-readable storage medium of claim 8 , wherein the length of the second reference curve is adjusted to approximate the length of the first reference curve.

11. The non-transitory machine-readable storage medium of claim 8 , wherein defining a fixed reference point on the first reference curve further comprises:

determining an intersection between the first reference curve and a reference plane; and

defining the fixed reference point as a point on the reference curve without dependence on the reference plane.

12. The non-transitory machine-readable storage medium of claim 8 , the logic further operable to toggle between the first reference geometry and the second reference geometry.

13. The non-transitory machine-readable storage medium of claim 8 , the logic further operable to regenerate the parametric CAD model to represent the object in the first engineering state by replacing the second reference geometry with the first reference geometry.

14. The non-transitory machine-readable storage medium of claim 8 , the logic further operable to:

determine an intersection between the first reference curve and a reference plane; and

identify a reference coordinate system formed by an intersection of the reference plane and the first surface, an intersection of the reference plane and the second surface, and the first reference curve.

15. The non-transitory machine-readable storage medium of claim 8 , the logic further operable to import the second reference geometry into the parametric CAD Model from an off-line CAD file.

Assignments (13)
RELEASE OF SECURITY INTEREST RECORDED AT REEL/FRAME 053570/0149 Recorded Jul 25, 2025
From: WILMINGTON TRUST, NATIONAL ASSOCIATION
To: TRIUMPH ACTUATION SYSTEMS-CONNECTICUT, LLC; TRIUMPH AEROSTRUCTURES, LLC; TRIUMPH CONTROLS, LLC; TRIUMPH ENGINE CONTROL SYSTEMS, LLC; TRIUMPH THERMAL SYSTEMS-MARYLAND, INC.; TRIUMPH INTEGRATED AIRCRAFT INTERIORS, INC.
Reel/Frame 072224/0841 →
SECURITY INTEREST Recorded Jul 24, 2025
From: TRIUMPH ACTUATION SYSTEMS-CONNECTICUT, LLC; TRIUMPH AEROSTRUCTURES, LLC; TRIUMPH ENGINE CONTROL SYSTEMS, LLC; TRIUMPH THERMAL SYSTEMS-MARYLAND, INC.; TRIUMPH CONTROLS, LLC
To: APOLLO ADMINISTRATIVE AGENCY LLC
Reel/Frame 071823/0096 →
RELEASE OF SECURITY INTEREST Recorded Mar 15, 2023
From: U.S. BANK TRUST COMPANY, NATIONAL ASSOCIATION
To: TRIUMPH GROUP, INC.; TRIUMPH CONTROLS, LLC; TRIUMPH THERMAL SYSTEMS - MARYLAND, INC.; TRIUMPH ACTUATION SYSTEMS - CONNECTICUT, LLC; TRIUMPH AEROSTRUCTURES, LLC; TRIUMPH AEROSTRUCTURES, LLC.; TRIUMPH ENGINE CONTROL SYSTEMS, LLC
Reel/Frame 064050/0497 →
RELEASE OF SECURITY INTEREST Recorded Jun 22, 2021
From: TRIUMPH AEROSTRUCTURES, LLC
To: U.S. BANK NATIONAL ASSOCIATION
Reel/Frame 056622/0392 →
RELEASE OF SECURITY INTEREST Recorded May 28, 2021
From: WILMINGTON TRUST, NATIONAL ASSOCIATION
To: TRIUMPH AEROSTRUCTURES, LLC
Reel/Frame 056384/0436 →
SECURITY AGREEMENT Recorded May 7, 2021
From: QARBON AEROSPACE (FOUNDATION), LLC, AS GRANTOR
To: ALLY BANK, AS THE COLLATERAL AGENT
Reel/Frame 056179/0290 →
GRANT OF SECURITY INTEREST IN PATENT RIGHTS Recorded Aug 20, 2020
From: TRIUMPH ACTUATION SYSTEMS - CONNECTICUT, LLC; TRIUMPH AEROSTRUCTURES, LLC; TRIUMPH CONTROLS, LLC; TRIUMPH ENGINE CONTROL SYSTEMS, LLC; TRIUMPH THERMAL SYSTEMS - MARYLAND, INC.; TRIUMPH INTEGRATED AIRCRAFT INTERIORS, INC.
To: WILMINGTON TRUST, NATIONAL ASSOCIATION
Reel/Frame 053570/0149 →
RELEASE OF SECURITY INTEREST Recorded Aug 17, 2020
From: PNC BANK, NATIONAL ASSOCIATION
To: TRIUMPH ACTUATION SYSTEMS, LLC; TRIUMPH ACTUATION SYSTEMS - CONNECTICUT, LLC; TRIUMPH AEROSTRUCTURES, LLC; TRIUMPH BRANDS, INC.; TRIUMPH CONTROLS, LLC; TRIUMPH ENGINE CONTROL SYSTEMS, LLC; TRIUMPH GEAR SYSTEMS, INC.; TRIUMPH GROUP, INC.; TRIUMPH INSULATION SYSTEMS, LLC; TRIUMPH INTEGRATED AIRCRAFT INTERIORS, INC.; TRIUMPH ACTUATION SYSTEMS - YAKIMA, LLC; TRIUMPH THERMAL SYSTEMS - MARYLAND, INC.; TRIUMPH ENGINEERED SOLUTIONS, INC.
Reel/Frame 053516/0200 →
GRANT OF SECURITY INTEREST IN PATENT RIGHTS Recorded Oct 3, 2019
From: TRIUMPH ACTUATION SYSTEMS - CONNECTICUT, LLC; TRIUMPH AEROSTRUCTURES, LLC; TRIUMPH CONTROLS, LLC; TRIUMPH ENGINE CONTROL SYSTEMS, LLC; TRIUMPH THERMAL SYSTEMS - MARYLAND, INC.
To: U.S. BANK NATIONAL ASSOCIATION, AS COLLATERAL AGENT
Reel/Frame 050624/0641 →
RELEASE OF SECURITY INTEREST Recorded Sep 23, 2019
From: ROYAL BANK OF CANADA
To: TRIUMPH AEROSTRUCTURES, LLC
Reel/Frame 050462/0287 →
MERGER Recorded Sep 23, 2019
From: VOUGHT AIRCRAFT INDUSTRIES, INC.
To: TRIUMPH AEROSTRUCTURES, LLC
Reel/Frame 050463/0054 →
SECURITY AGREEMENT Recorded Jul 23, 2010
From: TRIUMPH AEROSTRUCTURES, LLC
To: ROYAL BANK OF CANADA, AS ADMINISTRATIVE AGENT
Reel/Frame 024733/0151 →
SECURITY AGREEMENT Recorded Jul 6, 2010
From: TRIUMPH AEROSTRUCTURES, LLC
To: PNC BANK, NATIONAL ASSOCIATION
Reel/Frame 024630/0444 →