Inventor profile of:

Peter G. Smith

City:

Wallingford, Connecticut

Country:

United States

Published Applications:

15

Last publication date:

2015-07-09

Top Assignees for applications by Peter G. Smith

The entities that hold a legal rights for patent applications filed by inventor Smith Peter G.:

Recent patent applications by Smith Peter G.

Peter G. Smith from Wallingford, US has applied for patents for these inventions. The list has both pending applications and granted patents:

#1 | 2015-07-09
US20150192298A1
Mechanical engineering

GAS TURBINE ENGINE WITH IMPROVED FUEL EFFICIENCY

#2 | 2014-02-20
US20140050589A1
Mechanical engineering

Hybrid structure airfoil

#3 | 2013-02-14
US20130039774A1
Mechanical engineering

Hybrid structure airfoil

#4 | 2013-01-17
US20130014512A1
Mechanical engineering

Ceramic matrix composite combustor vane ring assembly

#5 | 2012-09-20
US20120233981A1
Mechanical engineering

GAS TURBINE ENGINE WITH LOW FAN PRESSURE RATIO

#6 | 2012-09-06
US20120222398A1
Mechanical engineering

GAS TURBINE ENGINE WITH GEARED ARCHITECTURE

#7 | 2012-09-06
US20120222397A1
Mechanical engineering

Gas turbine engine with low fan pressure ratio

#8 | 2012-05-24
US20120124964A1
Mechanical engineering

GAS TURBINE ENGINE WITH IMPROVED FUEL EFFICIENCY

#9 | 2012-03-22
US20120068003A1
Performing operations; transporting

Wireless sensor for an aircraft propulsion system

#10 | 2010-10-21
US20100266415A1
Mechanical engineering

Hybrid structure fan blade

#11 | 2009-12-31
US20090325468A1
Performing operations; transporting

Abrasive waterjet machining and method to manufacture a curved rotor blade retention slot

#12 | 2009-12-31
US20090320285A1
Performing operations; transporting

EDM MACHINING AND METHOD TO MANUFACTURE A CURVED ROTOR BLADE RETENTION SLOT

#13 | 2009-04-16
US20090097967A1
Mechanical engineering

Gas turbine engine with variable geometry fan exit guide vane system

#14 | 2008-05-01
US20080098894A1
Performing operations; transporting

Acoustic degassing heat exchanger

#15 | 2006-11-30
US20060266051A1
Mechanical engineering

Bleed diffuser for gas turbine engine

InventorID:

34662 ⎘