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Bem Case, Toronto CA
| Patent application number | Description | Published |
|---|---|---|
| 20090035090 | FASTENER RESTRAINT ASSEMBLY TO PREVENT ROTATIONAL LOOSENING OF MECHANICAL FASTENERS, FASTENER AND METHOD - An engagement fitting attaches to a rotational fastener, and is anchored to a point stationary relative to the fastener. A rotational coupling attaches the engagement fitting to an anchor member, allowing uni-directional rotation of said engagement fitting on the rotational fastener, relative to the anchor member, about the fastener axis, in a loosening direction of said rotational fastener, to prevent self-loosening of the fastener. | 02-05-2009 |
| 20110110744 | FASTENER RESTRAINT ASSEMBLY TO PREVENT ROTATIONAL LOOSENING OF MECHANICAL FASTENERS, FASTENER AND METHOD - An engagement fitting attaches to a rotational fastener, and is anchored to a point stationary relative to the fastener. A rotational coupling attaches the engagement fitting to an anchor member, allowing uni-directional rotation of said engagement fitting on the rotational fastener, relative to the anchor member, about the fastener axis, in a loosening direction of said rotational fastener, to prevent self-loosening of the fastener. | 05-12-2011 |
Ian Case, Bristol GB
| Patent application number | Description | Published |
|---|---|---|
| 20110231056 | METHOD OF OPERATING AN AIRCRAFT FUEL MANAGEMENT SYSTEM - A method of operating an aircraft fuel management system for an aircraft having at least one fuel tank, each fuel tank having an associated fuel quantity indicator arranged to provide an indication of the amount of fuel in the associated fuel tank, the method comprising calculating a value for the amount of fuel on board (FOB_FailedFQI) the aircraft to be utilised by the fuel management system in the event of a failure of at least one of the fuel quantity indicators, the amount of fuel on board being calculated as a value for the initial amount of fuel on board (FOBinit) minus the amount of fuel used. Additionally or alternatively a value for the gross weight centre of gravity of the aircraft is calculated using an assigned value of fuel for each of the fuel tanks having an associated failed fuel quantity indicator. | 09-22-2011 |
Michael Lee Case, Mississauga CA
| Patent application number | Description | Published |
|---|---|---|
| 20110126541 | MUFFLER SYSTEM FOR NOISE ABATEMENT AND ICE CONTROL - A method of controlling a discharge of an exhaust gas from a pneumatic device includes directing the exhaust gas from an exhaust port of the pneumatic device into proximity with a heated portion of the pneumatic device, expanding the exhaust gas in proximity with the heated portion of the pneumatic device to heat the exhaust gas, and discharging the exhaust gas to atmosphere. | 06-02-2011 |
Simon J Case, Redland GB
| Patent application number | Description | Published |
|---|---|---|
| 20080235203 | Information Retrieval - A method and apparatus are provided for accessing a relevant information resource in response to a user query. An ontology is provided, defining relationships between a plurality of predefined concepts, and between each of the predefined concepts and one or more predefined context phrases. On receipt of a user query, portions of the received query are compared with the context phrases to identify one or more matching phrases and hence, from the predefined relationships with concepts in the ontology, one or more relevant concepts. Concepts identified in respect of the received user query are used to identify a relevant action using predefined relationships between concepts in the ontology and predefined actions, wherein an action comprises providing access to an information resource. | 09-25-2008 |