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Inventor profile of:

Peter Broadhead

City:

Derby

Country:

United Kingdom

Published Applications:

Last publication date:

2020-06-25

Top Assignees for applications by Peter Broadhead

The entities that hold a legal rights for patent applications filed by inventor Broadhead Peter:

Rolls-Royce North American Technologies, Inc. 9 Indianapolis, IN United States
ROLLS-ROYCE CORPORATION 7 INDIANAPOLIS, IN United States
Rolls-Royce PLC 4 , United Kingdom
ROLLS-ROYCE PLC 2 London, United Kingdom
Rolls-Royce Deutschland Ltd & Co KG 2 Blankenfelde-Mahlow, Germany
Rolls-Royce High Temperature Composites Inc. 1 Cypress, CA United States

Recent patent applications by Broadhead Peter

Peter Broadhead from Derby, GB has applied for patents for these inventions. The list has both pending applications and granted patents:

#1 | 2020-06-25

US20200200788A1

Physics

SHAFT MONITORING SYSTEM

#2 | 2020-02-20

US20200056493A1

Mechanical engineering

Brazed blade track for a gas turbine engine

#3 | 2019-08-08

US20190242268A1

Mechanical engineering

Keystoned blade track

#4 | 2019-01-17

US20190017400A1

Mechanical engineering

Impingement tubes for gas turbine engine assemblies with ceramic matrix composite components

#5 | 2017-05-25

US20170145845A1

Mechanical engineering

Impingement tubes for CMC seal segment cooling

#6 | 2016-11-17

US20160333718A1

Mechanical engineering

Composite keystoned blade track

#7 | 2016-11-03

US20160319689A1

Mechanical engineering

Keystoned blade track

#8 | 2016-11-03

US20160319688A1

Mechanical engineering

Full hoop blade track with flanged segments

#9 | 2016-11-03

US20160319682A1

Mechanical engineering

Brazed blade track for a gas turbine engine

#10 | 2016-08-25

US20160245102A1

Mechanical engineering

Segmented turbine shroud with sealing features

#11 | 2009-12-24

US20090317245A1

Mechanical engineering

Method of forming a rotating blade assembly

#12 | 2009-10-29

US20090269190A1

Mechanical engineering

Arrangement for automatic running gap control on a two or multi-stage turbine

#13 | 2006-10-19

US20060233642A1

Mechanical engineering

Arrangement for internal passive turbine blade tip clearance control in a high pressure turbine

#14 | 2005-11-17

US20050254939A1

Mechanical engineering

Arrangement for the automatic running gap control on a two or multi-stage turbine

#15 | 2005-05-05

US20050095136A1

Mechanical engineering

Retaining arrangement

InventorID:

1631377 ⎘