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.
Patent No.:
Date of Patent:
Dec. 04, 2018
Filed:
Nov. 18, 2014
Applicant:
Lord Corporation, Cary, NC (US);
Inventors:
Daniel C. Zameroski, McKean, PA (US);
Gerald P. Whiteford, Waterford, PA (US);
Assignee:
LORD Corporation, Cary, NC (US);
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64D 27/00 (2006.01); B64D 27/26 (2006.01); G06F 11/34 (2006.01); B64D 27/10 (2006.01); F01D 25/04 (2006.01); F01D 25/28 (2006.01);
U.S. Cl.
CPC ...
B64D 27/26 (2013.01); B64D 27/10 (2013.01); F01D 25/04 (2013.01); F01D 25/28 (2013.01); G06F 11/3433 (2013.01); G06F 11/3447 (2013.01); G06F 11/3466 (2013.01); B64D 2027/266 (2013.01); F05D 2220/323 (2013.01); F05D 2230/60 (2013.01); F05D 2240/90 (2013.01); F05D 2260/96 (2013.01); G06F 11/3409 (2013.01); G06F 11/3419 (2013.01);
Abstract
An engine attachment system (EAS) includes a forward collar (), an aft collar (), at least one truss subassembly () disposed between the forward collar and the aft collar for supporting an engine, and at least one vibration isolator () integrated with each of the forward and aft collars for isolating engine vibration and reducing noise. A method of attaching a turboprop engine includes providing an EAS and hoisting a turboprop engine at least partially within the at least one truss subassembly ().