Inventor profile of:

David WADDLETON

City:

Candiac

Country:

Canada

Published Applications:

22

Last publication date:

2025-05-08

Top Assignees for applications by David WADDLETON

The entities that hold a legal rights for patent applications filed by inventor WADDLETON David:

Recent patent applications by WADDLETON David

David WADDLETON from Candiac, CA has applied for patents for these inventions. The list has both pending applications and granted patents:

#1 | 2025-05-08
US20250146461A1
Mechanical engineering

Gas Turbine Engine Fuel System for an Aircraft Propulsion System

#2 | 2024-03-07
US20240077032A1
Mechanical engineering

System and method for purging a fuel manifold of a gas turbine engine using a flow divider assembly

#3 | 2023-10-26
US20230340910A1
Mechanical engineering

System and method for purging a fuel manifold of a gas turbine engine through a flow divider valve

#4 | 2023-03-16
US20230083847A1
Mechanical engineering

System and method for purging a fuel manifold of a gas turbine engine through a flow divider valve

#5 | 2022-09-22
US20220298972A1
Mechanical engineering

System and method for purging a fuel manifold of a gas turbine engine using a flow divider assembly

#6 | 2022-06-09
US20220178544A1
Mechanical engineering

METHOD OF OPERATING AN AIRCRAFT ENGINE AND FUEL SYSTEM USING MULTIPLE FUEL TYPES

#7 | 2022-06-09
US20220178306A1
Mechanical engineering

METHOD OF OPERATING AN AIRCRAFT ENGINE AND FUEL SYSTEM USING MULTIPLE FUEL TYPES

#8 | 2020-11-19
US20200362764A1
Mechanical engineering

System and method for purging a fuel manifold of a gas turbine engine using a flow divider assembly

#9 | 2020-11-19
US20200362763A1
Mechanical engineering

System and method for purging a fuel manifold of a gas turbine engine through a flow divider valve

#10 | 2020-10-22
US20200331623A1
Performing operations; transporting

Aircraft motive flow line

#11 | 2020-10-08
US20200318644A1
Mechanical engineering

Rotodynamic pump and method

#12 | 2020-09-24
US20200300179A1
Mechanical engineering

Rotodynamic pump having a body defining a body cavity with a first and second housing portion defining a portion of an impeller cavity and disposed within the body cavity wherein the body cavity extends at least in part around the second housing portion and the housing portions defining an impeller clearance

#13 | 2020-09-10
US20200284205A1
Mechanical engineering

Aircraft engine fuel system and method

#14 | 2020-05-07
US20200141322A1
Mechanical engineering

Engine fuel system for use with composite aircraft

#15 | 2020-04-23
US20200123942A1
Mechanical engineering

Shared oil system arrangement for an engine component and a generator

#16 | 2018-03-15
US20180072402A1
Performing operations; transporting

Propeller blade angle control system

#17 | 2018-03-08
US20180066552A1
Mechanical engineering

Shared oil system arrangement for an engine component and a generator

#18 | 2017-12-21
US20170361919A1
Performing operations; transporting

Propeller blade angle control system

#19 | 2017-06-22
US20170175639A1
Mechanical engineering

Engine fuel system for use with composite aircraft

#20 | 2014-09-11
US20140252171A1
Performing operations; transporting

Nitrogen bubbler system in fuel tank and method

#21 | 2010-12-30
US20100326090A1
Mechanical engineering

Air filtration system for gas turbine engine pneumatic system

#22 | 2005-06-23
US20050135929A1
Mechanical engineering

Pressurized oil supply for propeller engine system

InventorID:

900345 ⎘