IP Library Granted Patent US 9,302,455
Granted Patent B1
US 9,302,455 · App. 13/835,051 · Granted Apr 5, 2016

Fast cure process

Inventors: Richard Boone (Wichita, KS); Engin Sabuncu (Wichita, KS)
Assignee: Textron Innovations, Inc.
B32B37/02
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Quick Facts
Patent No.
US 9,302,455
App. No.
13/835,051
Granted
Apr 5, 2016
Kind
B1
Abstract

A method for fast curing a component made from composite laminate. The method rapidly raising the temperature of the component by applying heat at an accelerated temperature for a ramp time, holding the temperature of the component at a set temperature for a set dwell time, and removing heat from the component to slow curing process. The method may additionally include inspecting the component after removing the component from heat, and curing the component a final time to equivalent or better strength.

Claims (18)

1. A method for fast curing a component made from composite laminate, comprising:

assembling the component within a bond tool, wherein the bond tool is adapted to prevent inconsistent heating of the component;

rapidly raising the temperature of the component at a rate of 15-20 degrees Fahrenheit per minute by applying heat at an accelerated temperature for a ramp time until the temperature of the component reaches a component temperature threshold;

holding the temperature of the component at the component temperature threshold for a dwell time until the glass transition temperature is raised to a desired glass transition temperature threshold; and

removing heat from the component to slow the curing process.

2. The method of claim 1 , wherein the ramp time is equivalent to 20 to 30 minutes.

3. The method of claim 1 , wherein the glass transition temperature comprises as a temperature where thermal transition that occurs in a solid polymeric materials, which marks the onset of coordinated multi-atom movement or softening of that material.

4. The method of claim 1 , further comprising the step of analyzing the component for quality assurance.

5. The method of claim 1 , further comprising the step of manipulating the component to a desired format after the step of removing heat.

6. The method of claim 5 further comprising completing the cure of the component such that a strength of the component is at least equivalent to a fully cured component cured in a single stage.

7. The method of claim 1 wherein the dwell time is determined based upon a defined temperature.

8. A method for fast curing a component made from composite laminate, comprising:

assembling the component within a bond tool;

rapidly raising the temperature of the component at a rate of at least about 15 degrees Fahrenheit per minute by applying heat at an accelerated temperature for a ramp time until the temperature of the component reaches a component temperature threshold;

holding the temperature of the component at the component temperature threshold for a dwell time until the glass transition temperature is raised to a desired glass transition temperature threshold; and

removing heat from the component to slow the curing process.

9. The method of claim 8 , the step of rapidly raising the temperature of the component comprising a rate between 15 degrees and 20 degrees Fahrenheit per minute.

10. The method of claim 8 , the step of rapidly raising the temperature of the component comprising a rate of greater than 20 degrees Fahrenheit per minute.

Assignments (3)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Oct 19, 2014
From: CESSNA AIRCRAFT COMPANY
To: CESSNA AIRCRAFT RHODE ISLAND
Reel/Frame 033976/0736 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Oct 19, 2014
From: CESSNA AIRCRAFT RHODE ISLAND
To: TEXTRON INNOVATIONS, INC.
Reel/Frame 033976/0743 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Sep 26, 2013
From: BOONE, RICHARD; SABUNEU, ENGIN
To: CESSNA AIRCRAFT COMPANY
Reel/Frame 031292/0496 →
Continuity (2)
Continuation In Part 13763416 · Feb 8, 2013
Provisional Application 61596651 · Feb 8, 2012