Resumes
Resumes
Mark Vignali Phones & Addresses
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Simsbury, CT
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Northfield, CT
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405 Neill Dr, Watertown, CT 06795 (860) 274-4803
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New Orleans, LA
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405 Neill Dr, Watertown, CT 06795
Work
Position:
Professional/Technical
Education
Degree:
High school graduate or higher
Publications
Us Patents
Cabin Air Compressor Outlet Duct
View pageUS Patent:
20140045415, Feb 13, 2014
Filed:
Aug 9, 2012
Appl. No.:
13/570905
Inventors:
Mark Vignali - Northfield CT, US
Assignee:
HAMILTON SUNDSTRAND CORPORATION - Windsor Locks CT
International Classification:
F04D 29/40
F04D 29/60
B64D 13/02
F04D 29/60
B64D 13/02
US Classification:
454 76, 4151821, 4152131
Abstract:
A cabin air compressor outlet duct includes an outlet portion, a first inlet portion fluidly connected to the outlet portion, and a second inlet portion fluidly connected to the outlet portion and joined to the first inlet through a curvilinear surface having a bend radius between about 2.50 inches (6.35 cm) and about 2.60 inches (6.60 cm).
Usage Based Propeller Life Monitoring
View pageUS Patent:
20210309384, Oct 7, 2021
Filed:
Feb 25, 2021
Appl. No.:
17/184826
Inventors:
- Figeac Cedex, FR
Brian P. Huth - West Hartford CT, US
Mark Vignali - Simsbury CT, US
Olivier Lacroix - BEDUER, FR
Brian P. Huth - West Hartford CT, US
Mark Vignali - Simsbury CT, US
Olivier Lacroix - BEDUER, FR
International Classification:
B64D 45/00
Abstract:
A system for monitoring propeller health includes a processing unit having a processor which is programmed to apply a plurality of algorithms to inputted aircraft parameter data. The system also includes a plurality of data inputs for inputting aircraft parameter data into the algorithms, wherein the processor is configured to apply the physics based algorithms to the aircraft parameter data to determine at least the fatigue life consumption of one or more critical components of a propeller. In addition, the system includes an output device which is able to output an indication of the determined fatigue life consumption to an observer.
Adaptable Dual Delta-P Flow Measurement
View pageUS Patent:
20200088107, Mar 19, 2020
Filed:
Sep 13, 2018
Appl. No.:
16/129919
Inventors:
- Charlotte NC, US
Patrick Yung - South Windsor CT, US
John M. Maljanian - Farmington CT, US
Jeffry K. Kamenetz - Windsor CT, US
Mark Vignali - Northfield CT, US
John A. Schwemmer - Ellington CT, US
Patrick Yung - South Windsor CT, US
John M. Maljanian - Farmington CT, US
Jeffry K. Kamenetz - Windsor CT, US
Mark Vignali - Northfield CT, US
John A. Schwemmer - Ellington CT, US
International Classification:
F02C 9/18
B64D 13/06
F02M 26/47
B64D 13/06
F02M 26/47
Abstract:
A system includes a venturi duct, a first delta P sensor, a second delta P sensor, and an ECS controller. The venturi duct is configured to receive a first bleed air flow or a second bleed air flow. The first and second delta P sensors are configured to sense a first and second pressure difference between a first point and a second point of the venturi duct. The first and second delta P sensors are configured to sense pressure difference over different pressure ranges. The ECS controller is configured determine a flow rate of an ECS air flow based upon the first pressure and/or second sensed pressure differences.
Fan Rotor Blade Having An Optimized Blade Root
View pageUS Patent:
20170108001, Apr 20, 2017
Filed:
Oct 16, 2015
Appl. No.:
14/885614
Inventors:
- Windsor Locks CT, US
Eric Chrabascz - Longmeadow MA, US
Mark Vignali - Northfield CT, US
Harold W. Hipsky - Willington CT, US
Eric Chrabascz - Longmeadow MA, US
Mark Vignali - Northfield CT, US
Harold W. Hipsky - Willington CT, US
International Classification:
F04D 29/38
F04D 19/00
F04D 19/00
Abstract:
A fan rotor blade extending radially from a hub is described. The fan rotor blade may include first surface and a second surface, where the first surface and second surfaces are respectively defined by a set of X-coordinates, Y-coordinates and Z-coordinates. The X, Y and Z coordinates can be set out in any of Tables T-1, T-2, E-1, and E-2. The X, Y, and Z-coordinates can also be scaled by a predetermined factor, with the X-coordinates are oriented in a tangential direction, the Z-coordinates are oriented in an axial direction, and the Y-coordinates are oriented in a radial direction.
Cabin Supply Bracket
View pageUS Patent:
20140367543, Dec 18, 2014
Filed:
Jun 12, 2013
Appl. No.:
13/915907
Inventors:
- Windsor Locks CT, US
John Perella - Monson MA, US
Mark Vignali - Northfield CT, US
John Perella - Monson MA, US
Mark Vignali - Northfield CT, US
International Classification:
B64D 13/08
US Classification:
2483091, 29428
Abstract:
A cabin supply bracket for a cabin supply duct assembly is provided. The cabin supply bracket includes a base plate with a first, second, and third mounting hole distributed in a substantially triangular arrangement. The first mounting hole has a centerline defined therethrough. A coupling socket extends from the base plate. The coupling socket includes a first and second tie rod coupling support having a tie rod coupling hole formed therethrough and a first and second outer edge. The first outer edge is proximate the second mounting hole, and the second outer edge is proximate the third mounting hole. The coupling socket has a socket width defined between a first socket edge proximate the first outer edge and a second socket edge proximate the second outer edge. A ratio of the socket width to a thickness of the base plate is between 6.31 and 7.84.
Mixer And Air Pack For Use In Aircraft Air Supply System
View pageUS Patent:
20140245775, Sep 4, 2014
Filed:
Dec 21, 2012
Appl. No.:
13/723398
Inventors:
Hamilton Sundstrand Corporation - , US
Mark Vignali - Northfield CT, US
Calvin R. Parent - Enfield CT, US
Brent J. Merritt - Southwick MA, US
Gary T. Luedtke - Tolland CT, US
Mark Vignali - Northfield CT, US
Calvin R. Parent - Enfield CT, US
Brent J. Merritt - Southwick MA, US
Gary T. Luedtke - Tolland CT, US
Assignee:
HAMILTON SUNDSTRAND CORPORATION - Windsor Locks CT
International Classification:
B64D 13/08
B64D 13/06
B64D 13/06
US Classification:
62401, 366136
Abstract:
A mixer has an internal bore with an inlet to a chamber, and an outlet at an opposed end/A duct is connected to receive a recirculated air flow. The duct communicates air into the chamber through recirculating air ports such that the recirculating air can mix with the air from the inlet. The mixer housing has a cockpit outlet for delivering air to a second outlet, with the cockpit output being located axially upstream from the recirculating air ports. An isolator is mounted at an outer periphery of the mixer housing, and has flat sides on each of two circumferentially spaced sides. A belly band is bolted to an outer periphery of the mixer housing and to flat sides of the isolator.