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Samuel D Spring, 70378 Davisville Rd UNIT 14, East Falmouth, MA 02536

Known as:
Spring Sd
Related to:
Lucille V Power 72 Edward D Anderson 81

Samuel Spring Phones & Addresses

378 Davisville Rd, East Falmouth, MA 02536   

Waquoit, MA   

Bourne, MA   

10 Hemlock St, Hampton, NH 03842    603-6012487   

Naples, FL   

Exeter, NH   

Stratham, NH   

Townsend, MA   

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Samuel Spring Photo 13

Samuel Spring

Samuel D. Spring (born in Uxbridge, Massachusetts Colony in 1746-died in Newburyport, Massachusetts, in 1819) was an early Revolutionary War chaplain and Congregationalist minister.

Us Patents

Bay Cooled Turbine Casing

US Patent:
6227800, May 8, 2001
Filed:
Nov 24, 1998
Appl. No.:
9/200386
Inventors:
Samuel D. Spring - Stratham NH
Robert J. Carita - Needham MA
Herbert A. Stocking - Salem MA
Assignee:
General Electric Company - Cincinnati OH
International Classification:
F04D 3100
US Classification:
415116
Abstract:
A turbine casing supports a row of nozzle vanes through which are flowable hot combustion gases. A baffle surrounds the casing to define a cooling duct. A nacelle surrounds the turbine casing to define a bay having an inlet for receiving bay air, and an outlet for discharging the air. The cooling duct includes an inlet which receives the bay air for flow along the turbine casing for selective cooling thereof.

Turbine Blade Having Offset Turbulators

US Patent:
5681144, Oct 28, 1997
Filed:
Dec 17, 1991
Appl. No.:
7/809193
Inventors:
Samuel Dale Spring - Stratham NH
Nesim Abuaf - Schenectady NY
Mohammad Esmail Taslim - Needham MA
Assignee:
General Electric Company - Cincinnati OH
International Classification:
F01D 518
US Classification:
416 97R
Abstract:
A gas turbine engine blade includes an airfoil having first and second sides and an internal passage extending longitudinally therebetween for channeling air to cool the airfoil. Respective pluralities of first and second turbulator ribs extend inwardly from at least one of the first and second airfoil sides. Adjacent ones of second ends of the first and second ribs are staggered apart longitudinally and overlap chordally for defining a gap therebetween facing transversely for turning cooling air upon flow through the gap. The gap increases convective heat transfer enhancement for reducing cooling air requirements and improving blade creep life.

Possible Relatives

Cynthia M Spring  David C Spring  Daniel P Spring  Aaron J Spring  Denise M Spring  Danielle L Spring  Dennis P Spring  Samuel C Johnson  Samuel J Stanage  Samuel Johnston 

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