Robert J Dolan

Address:

155 Cooper Pl, New Haven, CT 06515

Phone:

(203)3895652

VIN:

KNAGE124X75082917

Make:

KIA

Model:

OPTIMA

Year:

2007

US Patent:

20070254170, Nov 1, 2007

Filed:

Apr 28, 2006

Appl. No.:

11/413459

Inventors:

Kelly Hoover - Glastonbury CT, US
Charles Watson - Windsor CT, US
John Putnam - Glastonbury CT, US
Robert Dolan - Coventry CT, US
Bret Bonarrigo - Avon CT, US
Phyllis Kurz - Hebron CT, US
Michael Weisse - Tolland CT, US

International Classification:

B05D 3/02
B05D 1/36
B05D 1/02
B05D 1/28
B05D 1/18
B32B 9/04

US Classification:

428447000, 427402000, 427372200, 427421100, 427429000, 427430100, 428448000

Abstract:

A process for protecting an article using an anti-icing coating includes the steps of applying upon at least one surface of an article an anti-icing composition comprising at least one polysiloxane free of additives; and curing the anti-icing composition to form an anti-icing coating exhibiting an ice shear strength of about 19 kPA to about 50 kPa.

US Patent:

20210032997, Feb 4, 2021

Filed:

Aug 2, 2019

Appl. No.:

16/530917

Inventors:

- Farmington CT, US
Dmitri Novikov - Avon CT, US
Robert C. Dolan - Coventry CT, US
Eric W. Malmborg - Amston CT, US
Steven T. Gordon - Glastonbury CT, US

International Classification:

F01D 5/30
F01D 5/14
F04D 29/38
B23K 1/00

Abstract:

An airfoil for a gas turbine engine according to an example of the present disclosure includes, among other things, a first portion welded to a second portion along an interface such that at least the first portion establishes an airfoil section and the second portion establishes a root section mountable to a rotatable hub. The airfoil section includes an airfoil body extending between leading and trailing edges in a chordwise direction, extending between pressure and suction sides separated in a thickness direction, and extending from the root section in a spanwise direction to a tip portion. A recessed region extends inwardly from at least one of the pressure and suction sides. The airfoil body includes at least one rib bounding a respective pocket within a perimeter of the recessed region. A cover skin is welded to the airfoil body along the at least one rib to enclose the recessed region. A method of forming a gas turbine engine component is also disclosed.

US Patent:

20190040744, Feb 7, 2019

Filed:

Aug 7, 2017

Appl. No.:

15/670654

Inventors:

- Framington CT, US
Dmitri Novikov - Avon CT, US
Robert C. Dolan - Coventry CT, US
Kenneth A. Frisk - West Hartford CT, US
Steven T. Gordon - Glastonbury CT, US
William R. Graves - Amston CT, US
Eric W. Malmborg - Amston CT, US
Francis B. Parisi - West Suffield CT, US
Randy P. Salva - Baltic CT, US
Michael A. Weisse - Tolland CT, US
Russell A. Beers - Manchester CT, US
Xuedong Zhou - Glastonbury CT, US
Christopher Treese - West Hartford CT, US
Tri Nguyen - Windsor CT, US

International Classification:

F01D 5/14
F04D 29/26
B23P 15/04
B23K 15/00
B23K 26/28

Abstract:

An airfoil including an airfoil body, a recessed portion of a first depth in a first side of the airfoil body, the recessed portion including a plurality of pockets of a second depth located within the recessed portion and ribs of the first depth located between the pockets, a cover configured to fit into the recessed portion such that an interior surface of the cover engages the ribs and an exterior surface of the cover is about flush with an exterior surface of the first side of the airfoil body, and a high energy beam weld configuration extending through the cover and into the ribs and positioned to attach the cover to the ribs.