The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Oct. 12, 2021

Filed:

Feb. 03, 2017
Applicant:

Bell Helicopter Textron Inc., Fort Worth, TX (US);

Inventors:

Tom S. Chiang, Dallas, TX (US);

Bruce B. Bacon, Euless, TX (US);

Frank S. Allen, North Richland Hills, TX (US);

Jahanzeb Tareen, Grapevine, TX (US);

Christopher L. Gravelle, Fort Worth, TX (US);

Assignee:

Bell Helicopter Textron Inc., Fort Worth, TX (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B29C 35/04 (2006.01); B64C 3/18 (2006.01); F16B 5/01 (2006.01); F16B 11/00 (2006.01); B64F 5/10 (2017.01); B29C 70/30 (2006.01); B29C 70/34 (2006.01); B64C 29/00 (2006.01); B29K 105/08 (2006.01); B29L 31/30 (2006.01);
U.S. Cl.
CPC ...
B64C 3/187 (2013.01); B29C 35/045 (2013.01); B29C 70/30 (2013.01); B29C 70/34 (2013.01); B64C 3/185 (2013.01); B64C 29/0033 (2013.01); B64F 5/10 (2017.01); F16B 5/01 (2013.01); F16B 11/006 (2013.01); B29K 2105/0872 (2013.01); B29L 2031/3085 (2013.01);
Abstract

In one aspect, a heating tool includes a heat source having a discharge outlet; and a manifold including an intake conduit configured to releasably connect to the discharge outlet of the heat source and a chamber coupled to the intake conduit having a ventilation path. The chamber includes a diverging portion configured to provide uniform airflow through the ventilation path to provide heating to a surface. In an embodiment, the chamber has a first portion and a second portion configured for assembly and disassembly. A method of curing an aircraft component is provided.


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