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Inventor profile of:

Daniel Benjamin

City:

Simsbury, Connecticut

Country:

United States

Published Applications:

Last publication date:

2020-10-29

Top Assignees for applications by Daniel Benjamin

The entities that hold a legal rights for patent applications filed by inventor Benjamin Daniel:

UNITED TECHNOLOGIES CORPORATION 12 Hartford, CT United States
UNITED TECHNOLOGIES CORPORATION 3 Farmington, CT United States
MTU AERO ENGINES AG 1 Munich, Germany
Pratt & Whitney 1 Farmington, United States
MTU Aero Engines AG 1 München, Germany
Raytheon Technologies Corporation 1 Farmington, CT United States
UNITED TECHNOLOGIES CORPORATION 1 Hartford, CO United States

Recent patent applications by Benjamin Daniel

Daniel Benjamin from Simsbury, US has applied for patents for these inventions. The list has both pending applications and granted patents:

#1 | 2020-10-29

US20200340369A1

Mechanical engineering

Rotating leaf spring seal

#2 | 2017-08-10

US20170227014A1

Mechanical engineering

Systems and methods for reducing friction during gas turbine engine assembly

#3 | 2014-12-04

US20140356099A1

Mechanical engineering

Thread load distribution

#4 | 2014-05-13

US13709498

Device and method for testing a gas turbine engine component

#5 | 2014-01-23

US20140023486A1

Mechanical engineering

Tie shaft for gas turbine engine and flow forming method for manufacturing same

#6 | 2014-01-16

US20140017087A1

Mechanical engineering

Dynamic stability and mid axial preload control for a tie shaft coupled axial high pressure rotor

#7 | 2013-10-24

US20130280028A1

Mechanical engineering

Thermal management system for a gas turbine engine

#8 | 2013-10-10

US20130266421A1

Mechanical engineering

Tie shaft arrangement for turbomachine

#9 | 2013-10-03

US20130259599A1

Mechanical engineering

Thread load distribution

#10 | 2013-02-28

US20130051985A1

Mechanical engineering

Assembly and method preventing tie shaft unwinding

#11 | 2012-05-10

US20120112415A1

Mechanical engineering

ROTATING SEAL RING WITH TARGETED SPLIT SURFACE ORIENTATION

#12 | 2012-05-03

US20120107098A1

Mechanical engineering

Gas turbine engine rotor tie shaft arrangement

#13 | 2011-09-15

US20110223026A1

Mechanical engineering

Gas turbine engine compressor and turbine section assembly utilizing tie shaft

#14 | 2011-09-15

US20110223025A1

Mechanical engineering

Gas turbine engine rotor sections held together by tie shaft, and with blade rim undercut

#15 | 2011-09-15

US20110219784A1

Mechanical engineering

COMPRESSOR SECTION WITH TIE SHAFT COUPLING AND CANTILEVER MOUNTED VANES

#16 | 2011-09-15

US20110219781A1

Mechanical engineering

GAS TURBINE ENGINE WITH TIE SHAFT FOR AXIAL HIGH PRESSURE COMPRESSOR ROTOR

#17 | 2011-06-23

US20110146298A1

Mechanical engineering

Retaining member for use with gas turbine engine shaft and method of assembly

InventorID:

113106 ⎘