Richard F Reilly

44453388, May 1, 1984

Oct 23, 1981

6/314285

Stanley J. Markowski - East Hartford CT
Richard S. Reilly - Lake Park FL

The United States of America as represented by the Secretary of the Navy - Washington DC

F02G 100
F02K 138

60748

An improved swirler assembly prevents flow separation in the diffuser secn. An annular swirling layer of air surrounds a linear jet with mixing occurring between these air flows prior to the diffuser section. A center tube through the swirler section provides the linear jet which mixes with the swirler flow in a mixing area prior to the diffuser section.

39370089, Feb 10, 1976

Dec 18, 1974

5/534018

Stanley J. Markowski - East Hartford CT
Richard S. Reilly - East Hartford CT

United Technologies Corporation - Hartford CT

F02C 324
F02M 2300
F02M 3100

60 3906

A low emission combustion chamber in which vitiated products of combustion from a pilot burner are caused to swirl about the combustion chamber axis before fuel droplets are introduced into the vitiated, swirling combustion products for flash vaporization therein to produce a vaporized, swirling, vitiated fuel-air mixture so as to effect ignition lag until swirling combustion air can be mixed with the swirling mixture to molecularly premix the fuel and air and increase its oxygen content to reduce the ignition lag to effect autoignition at an equivalence ratio less than 1 so as to effect high-rate, lean burning in the primary combustion chamber.

39746461, Aug 17, 1976

May 19, 1975

5/578974

Stanley J. Markowski - East Hartford CT
Richard S. Reilly - East Hartford CT

United Technologies Corporation - Hartford CT

F02C 722
F02K 304
F02K 310

60 3965

A mixed flow turbofan engine in which a portion of the core engine exhaust gases are passed into a pilot zone chamber where fuel is added thereto for vaporization therewith and wherein the fan air is passed over a series of vortex generators so that the vortex flow fan air and the vaporized fuel mixture will mix and combust rapidly in an augmentation combustion chamber.

39303705, Jan 6, 1976

Jun 11, 1974

5/478403

Stanley J. Markowski - East Hartford CT
Richard S. Reilly - East Hartford CT

United Technologies Corporation - Hartford CT

F02K 304
F02K 308

60261

A mixed flow turbofan engine in which a portion of the core engine exhaust gases are passed into a pilot zone chamber where fuel is added thereto for vaporization therewith and wherein the fan air is passed over a series of vortex generators so that the vortex flow fan air and the vaporized fuel mixture will mix and combust rapidly in an augmentation combustion chamber.

20180285977, Oct 4, 2018

Mar 29, 2017

15/473583

- Hartford CT, US
Kristin Shumway - West Hartford CT, US
Michael Commendatore - Southington CT, US
Richard I. Reilly - East Windsor CT, US
Sean T. Datcher - Weatogue CT, US

G06Q 40/08
H04W 4/00
H04L 29/06
H04W 12/04
H04W 12/06

Systems, methods, and articles of manufacture provide for multi-party sensors managed via a mobile device application that coordinates first-party data, thresholds, and alerts from a first-party server and second-party data, thresholds, and alerts from a second-party server.