Dimelow
Chris Dimelow, Leicestershire GB
Patent application number | Description | Published |
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20110223297 | Anti-Caking Agent for Flavored Products - The present invention generally relates to the use of porous particles to control the release of a liquid, such as the release of a flavor in a food product. Liquid components, such as flavorants, are loaded into porous particles to form a composition. The pore diameter, pore tortuosity and loading parameters determine the characteristics of the composition and the release profile of the liquid. | 09-15-2011 |
20140266194 | METHOD AND APPARATUS FOR MEASURING PHYSICO-CHEMICAL PROPERTIES USING A NUCLEAR MAGNETIC RESONANCE SPECTROMETER - Methods for measuring physico-chemical properties using a nuclear magnetic resonance spectrometer are disclosed, including methods to determine an initial amount of a substance, usually a liquid, contained inside a porous material and an initial amount of the substance, usually a liquid, present outside the porous material, methods to measure the release kinetics of a substance, such as a liquid, from a porous material, and methods for performing chemical reactions and other physico-chemical operations in situ inside a nuclear magnetic resonance probe after a sample is loaded into a nuclear magnetic resonance spectrometer. The apparatuses for performing these methods are also disclosed. | 09-18-2014 |
Stephen J. Dimelow, Uttoxeter GB
Patent application number | Description | Published |
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20110000183 | ASSEMBLY PROVIDING CONTAMINANT REMOVAL - An assembly for the removal of contaminants from a contact zone between respective contact surfaces | 01-06-2011 |
20130071234 | ABRADABLE PANEL AND METHOD OF FORMING THE SAME - An abradable panel for a fan track liner assembly comprises an abradable layer comprising a syntactic material. The abradable panel is arranged to be attached to a fan track liner so as to provide an abradable gas-washed surface. The abradable panel may further comprise a carrier tray to which the abradable layer is attached. There is also disclosed a method of manufacturing an abradable panel. | 03-21-2013 |
Stephen Jonathan Dimelow, Staffordshire GB
Patent application number | Description | Published |
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20110081230 | METHOD FOR FORMING A PRESSURE MEASUREMENT HOLE IN A COMPONENT - A method for forming a pressure measurement hole in a component includes the step of forming a hole in a body of the component, the hole extending from a body surface of the component. An insert having a longitudinal passage is fitted into the hole such that the insert protrudes from the body surface. The protruding end of the insert is machined to define an insert surface profile matched to the body surface profile and displaced from the body surface by a distance substantially equal to a thickness of a covering layer that is to be bonded onto the body surface. A blocking pin is inserted into the insert passage. The covering layer is then bonded to the body surface in the region of the hole and insert after which the blocking pin is removed from the insert to open the pressure measurement hole. | 04-07-2011 |
Stephen Jonathan Dimelow, Uttoxeter GB
Patent application number | Description | Published |
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20140023508 | ROTOR ASSEMBLY - A rotor assembly includes a rotor disc and a plurality of circumferentially-spaced, radially outwardly extending rotor blades. The rotor disc has a rim and a plurality of circumferentially spaced slots provided in the rim of the rotor disc, each rotor blade having a root, the root of each rotor blade being arranged in a corresponding one of the slots in the rim of the rotor disc, and at least one of the slots having a chocking device accommodated within a space between a radially outer surface of the slot and a radially inner surface of the root of the rotor blade. The chocking device includes at least a first spring and a second spring, the first and second springs each abutting a radially inner surface of the root of the corresponding rotor blade and arranged transversely relative to a longitudinal axis of the slot. | 01-23-2014 |
20140271148 | ENGINE CASING ASSEMBLY - A gas turbine engine casing assembly has a first casing element which is located radially outward of one or more rotating aerofoil elements of the gas turbine engine. The first casing element is radially enclosed by a track element, a septum layer, a second casing element and a fan case. The track element is formed from an abrasion resistant material in order to prevent abrasion of the septum layer during excoriation of the first casing element. | 09-18-2014 |