Frank J Euvino from 56 Grickis Ln, Union City, CT 06770, age 64, Phone: 2037237577

Composite Integrally Bladed Rotor
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US Patent:

20050220621, Oct 6, 2005
Filed:

Dec 8, 2004
Appl. No.:

11/007503
Inventors:

David Hornick - East Hampton CT, US
Frank Euvino - Naugatuck CT, US
James Roach - East Hampton CT, US
International Classification:

B63H001/16
US Classification:

416189000
Abstract:

The present invention relates to an integrally bladed rotor for use in a gas turbine engine. The integrally bladed rotor comprises a plurality of pairs of airfoil blades. Each pair of blades has a spar which extends from a first tip of a first one of the airfoil blades in the pair to a second tip of a second one of the airfoil blades in the pair. The rotor further comprises an outer shroud integrally joined to the first and second tips in each pair of airfoil blades and an inner diameter hub.

Modular Fan Inlet Case
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US Patent:

20060269405, Nov 30, 2006
Filed:

May 31, 2005
Appl. No.:

11/140789
Inventors:

Frank Euvino - Naugatuck CT, US
David Lyders - Middletown CT, US
Assignee:

United Technologies Corporation - Hartford CT
International Classification:

F03B 11/02
US Classification:

415208100
Abstract:

A modular fan inlet case includes a center ring, an outer ring, and a plurality of struts each coupled at a first end to the center ring, and at a second end to the outer ring. A plurality of shell members are each configured to be removably coupled to a corresponding strut. Preferably, the plurality of shell members each define a longitudinal groove for being received onto the corresponding strut.

Electrothermal Inlet Ice Protection System
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US Patent:

20060280600, Dec 14, 2006
Filed:

May 31, 2005
Appl. No.:

11/140790
Inventors:

Frank Euvino - Naugatuck CT, US
Anthony Vinciquerra - Niskayuna NY, US
Assignee:

United Technologies Corporation - Hartford CT
International Classification:

F04D 29/00
US Classification:

415175000
Abstract:

A modular fan inlet ice protection system includes a center ring, an outer ring and a plurality of struts. The struts are each coupled at a first end to the center ring, and at a second end to the outer ring. A plurality of shell members are each configured to be removably coupled to a corresponding strut. Moreover, the shell members each include an electrothermal heater element Preferably the system further includes a plurality of inlet guide vanes each including an electrothermal heater element.

Organic Matrix Composite Integrally Bladed Rotor
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US Patent:

20040042902, Mar 4, 2004
Filed:

Sep 3, 2002
Appl. No.:

10/235025
Inventors:

David Hornick - East Hampton CT, US
Frank Euvino - Naugatuck CT, US
James Roach - East Hampton CT, US
International Classification:

F01D005/22
US Classification:

416/189000, 416/230000, 416/234000
Abstract:

The present invention relates to an integrally bladed rotor for use in a gas turbine engine. The integrally bladed rotor comprises a plurality of pairs of airfoil blades. Each pair of blades has a spar which extends from a first tip of a first one of the airfoil blades in the pair to a second tip of a second one of the airfoil blades in the pair. The rotor further comprises an outer shroud integrally joined to the first and second tips in each pair of airfoil blades and an inner diameter hub.

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Frank J Euvino