Simms, GB
Graham John Simms, Reading GB
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20100236071 | Manually Actuable Liquid Dispensing Razor - The invention features a razor for dispensing a fluid during shaving. The razor includes a handle, a razor cartridge, and a fluid dispensing member joined to the cartridge. The handle includes a cavity for housing a fluid and a manually-actuated pump to displace the fluid from the cavity through a supply channel to an opening at the proximal end of the handle. The razor cartridge includes a cartridge connecting structure attached to the housing, at least one blade positioned in the housing, and an aperture that extends from the rear surface to the front surface of the housing. The fluid dispensing member has a dispensing channel with an opening at a supply end and an opening at a dispensing end. The supply end is configured to engage the opening in the supply channel. The dispensing end projects outwardly and extends to or adjacent to the aperture in the housing. | 09-23-2010 |
20100236072 | Manually Actuable Liquid Dispensing Razor - The invention features a razor for dispensing a fluid during shaving. The razor includes a razor cartridge that is engageable to a handle. The razor cartridge has a housing, a cartridge connecting structure attached to the housing; at least one blade positioned in the housing; and an aperture that extends from the rear surface to the front surface of the housing. The handle has a cavity for housing a fluid; a manually-actuated pump located along the length of the handle, and a fluid dispensing member having a channel in fluid communication with the pump and having an opening at a terminal end. The fluid dispensing member projects outwardly from the proximal end of the handle such that the terminal end extends to or adjacent to the aperture in the housing. Actuation of the pump displaces fluid from the cavity to or adjacent to the front surface of the housing. | 09-23-2010 |
20130067714 | METHOD OF MAKING A REPLACEABLE RAZOR CARTRIDGE FOR DISPENSING FLUID - The invention features method for making a replaceable razor cartridge for dispensing fluid. The method includes providing a cartridge housing having a guard, a lubricating member, and one or more blades. The cartridge housing has a top portion, a bottom portion, a front surface, a rear surface, and an aperture extending from the rear surface to the front surface. The method also includes integrally molding a cartridge connector and a fluid dispensing member. The cartridge connector has a pair of extending arms. The fluid dispensing member has a dispensing channel with an opening at a supply end and at least two openings at a dispensing end. The dispensing end projects outwardly to or adjacent to the aperture in the cartridge housing and the cartridge connecting structure is configured to releasably engage a handle. | 03-21-2013 |
20150360376 | Methods Of Manufacturing Silicon Blades For Shaving Razors - Methods are provided for the manufacture of razor blades from silicon material. In some implementations, the method includes aligning a mono-crystalline silicon wafer comprising a {100} surface at an angle where {111} planes intersect the {100} surface parallel and perpendicular to the wafer; etching the mono-crystalline silicon wafer to expose an {111} plane and a second plane to provide a blade edge having between about a 20 degree included blade angle and about a 35 degree included blade angle; applying a hard coating on the blade edge; providing a radius of curvature of the blade edge between about 20 nanometers and about 100 nanometers after deposition of the hard coating; applying a soft coating on the blade edge; and removing the razor blade from the mono-crystalline silicon wafer. | 12-17-2015 |
Graham John Simms, Berkshire GB
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20090019701 | Safety razors - The invention relates to safety razors that include a blade unit carried on a handle, a vibration device powered by a battery under control of a control device, and a switch, e.g., included in the handle, to switch on and off an electrical connection between the battery and the control device; a storage tray on which the razor is stored when not in use including a magnet so that the switch closes a connection between the battery and the control device when the razor is separated from the storage tray; and a timing device to interrupt the supply of power to the electrical arrangement if the razor is not returned to the razor holder within a predetermined time period after being removed from the razor holder. | 01-22-2009 |
Howard Simms, Lancashire GB
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20130109362 | TELEPHONE CALL BLOCKING | 05-02-2013 |
Howard John Simms, Altrincham GB
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20110103576 | TELEPHONE CALL HANDLING - A telephone handset is provided with a user interface which includes a display unit, audio output unit and various user actuable keys. A phone controller implements and responds to instructions from the user interface. Where the instructions from the user interface request the connection of a call, the phone controller connects the handset to a PSTN via one of a plurality of connection means provided. Similarly, in the event of an incoming call connection request received via any one of the connection means, the phone controller enables the connection of the call. The user may choose to accept or reject the connection using the interface. The handling of an incoming or outgoing call is determined by a connection routing engine. The connection routing engine comprises an identification unit, a rules unit, a comparison unit and an enabling unit. | 05-05-2011 |
Mark J. Simms, Bristol GB
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20090074562 | NOZZLE GUIDE VANES - A turbine nozzle guide vane | 03-19-2009 |
Mark John Simms, Derby GB
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20160090866 | SHROUD SEGMENT RETAINER - A gas turbine, including: axially adjacent first and second components each having a gas path facing surface within an engine casing, inter-component cavity located between first and second components on the gas path outboard side, an axial-restrictor within the inter component cavity for restricting movement of the first or second component relative to at least one other first and second component or engine casing, wherein the axial-restrictor is radially located in the engine casing or other first and second component and includes a radially facing surface; a retaining element, including a body having circumferential length extending around the gas turbine engine and axial length extending between axially adjacent first and second components when in use; an obstructing portion between the radially facing surface of the axial-restrictor and opposing second radial surface of the other first or second component or engine casing to restrict radial movement of in use axial-restrictor. | 03-31-2016 |
Mark John Simms, Bristol GB
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20110236185 | INTERSTAGE SEAL - An interstage seal is provided for installation between forward and aft stage discs of a turbine section of a gas turbine engine. The seal has a forward annular portion, which extends forward to contribute to an air seal at the outer periphery of the forward stage disc, and an aft annular portion, which extends rearward to contribute to an air seal at the outer periphery of the aft stage disc. The seal has a peripheral slot into which static vane inner rails are loadable. The seal includes a first component, which provides the forward annular portion, and a second component, which provides the aft annular portion. The second component is separably connectable to the first component such that the first and second components, when connected, cooperate to form the peripheral slot. Loading the static vane inner rails into the slot prevents the second component separating from the first component. | 09-29-2011 |
20140341707 | SHROUD ARRANGEMENT FOR A GAS TURBINE ENGINE - A seal segment of a shroud arrangement for bounding a hot gas flow path within a gas turbine engine, including: a plate having an inboard hot gas flow path facing side and an outboard side; a bulkhead extending from the outboard side of the plate which defines a fore portion and an aft portion; a first cooling circuit within the plate for cooling a first portion of the plate; a second cooling circuit within the plate for cooling a second portion of the plate; wherein the first cooling circuit is in fluid communication with the fore portion and the second cooling circuit is in fluid communication with the aft portion and the first and second cooling circuits are fluidically isolated from one another. Also described is a method of cooling a seal segment in a gas turbine engine. | 11-20-2014 |
20140341721 | SHROUD ARRANGEMENT FOR A GAS TURBINE ENGINE - Described is a shroud arrangement for a gas turbine engine, comprising: a seal segment for bounding a hot gas flow path within the gas turbine engine, the seal segment being attached to a casing of the engine via at least one fore attachment and at least one aft attachment, the fore and aft attachment restricting radial movement of the seal segment relative to the engine casing; and, an axial restrictor which prevents axial movement of the seal segment relative to the engine casing, the axis being the principal rotational axis of the engine, wherein the fore and aft retention features are slidably engaged with a carrier segment or engine casing from a common direction. Also described is a gas turbine engine having the shroud arrangement. | 11-20-2014 |
Michael James Simms, High Peak GB
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20140114040 | SEMICONDUCTOR COMPOUNDS - This invention comprises a semiconducting polymer having a permittivity greater than 3.4 at 1000 Hz and a charge mobility in the pure state greater than 10 | 04-24-2014 |
Nick Simms, Bexley GB
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20130043053 | Power Tool for Falsework Assemblies - A power tool is provided for turning the screw collars | 02-21-2013 |
Nigel Simms, Milton Keynes GB
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20130040166 | LAYERED COATING SYSTEM WITH A MCRALX LAYER AND A CHROMIUM RICH LAYER AND A METHOD TO PRODUCE IT - A layer system and a method for producing a component having such a layer system are provided. The layer system includes a substrate a substrate, at least one MCrX layer on the substrate, and a chromium-rich layer on or in the at least one MCrX layer. X includes at least one element selected from the group consisting of yttrium (Y), silicon (Si), aluminum (Al) and boron (B). M includes at least one element selected from the group consisting of nickel (Ni) and cobalt (Co). | 02-14-2013 |
Norwin Simms, Belfast GB
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20090103559 | Method and Apparatus for Communicating Data Over a Data Network - A management device for automatically provisioning a Broadband Remote Access Server (BRAS) for use in connecting Customer Premises Equipment (CPE) to an Internet Protocol (IP) network via a Digital Subscriber Line (DSL) a Digital Subscriber Line Access Multiplexor (DSLAM) and the BRAS, the management device comprising: a first interface for receiving from time to time data readings from the DSLAM indicative of the current or recent line rate of the DSL; a processor unit for calculating from the received data readings a consistent rate indicative of a consistent line rate of the DSL based on a plurality of data readings for the DSL from the DSLAM; and a second interface for transmitting provisioning messages to the BRAS for provisioning the BRAS to restrict data flowing to the DSL to a maximum rate selected by the management device in accordance with the calculated consistent rate. | 04-23-2009 |
20090262647 | Method and Apparatus for Communication Data Over a Data Network - A Digital Subscriber Line Access Multiplexer (DSLAM) is modified to monitor when a line synchronizes (i.e. sets up a DSL connection) and to automatically generate a notification to be sent to a management device of the access network if the rate has changed from the last time the line synchronized. | 10-22-2009 |
Paul Simms, Leicester GB
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20130058775 | CATCHER RING ASSEMBLY - A catcher ring assembly ( | 03-07-2013 |
Paul Simms, Hathern GB
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20110274546 | BACK-UP FEATHERER - A back-up featherer is provided for an engine arrangement having a main hydraulic actuator which operates a pitch change mechanism to angularly displace propellers of a propeller assembly of the engine arrangement, the pitch change mechanism and main hydraulic actuator rotating with the propeller assembly. The back-up featherer has one or more back-up hydraulic actuators located on a static structure of the engine arrangement. The back-up featherer further has one or more load application members which are located on the static structure of the engine arrangement and which are movable by the back-up hydraulic actuators. When moved by the back-up hydraulic actuators, the load application members bear against an engagement portion of the pitch change mechanism across a rotating interface formed therebetween to apply a load to the pitch change mechanism which results in angular displacement of the propellers. | 11-10-2011 |
20120294718 | VARIABLE PITCH PROPELLER ROTOR - A bladed rotor comprises a rotor body | 11-22-2012 |
Paul Simms, Melton Mowbray GB
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20100024434 | Gas turbine engine arrangement - A gas turbine engine arrangement ( | 02-04-2010 |
Richard Simms, Cambridgeshire GB
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20100106588 | DISPLAY SYSTEM - A display system | 04-29-2010 |
Stephen Simms, Dunfermline GB
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20100315307 | Radome and Shroud Enclosure for Reflector Antenna - An enclosure for the open end of a reflector antenna includes a cylindrical shroud coupled to a distal end of the reflector antenna, the shroud generally coaxial with a longitudinal axis of the reflector antenna. A retaining band is coupled to an inner diameter of the shroud, proximate a distal end of the shroud. The retaining band is provided with a retaining groove open radially inward towards the longitudinal axis. The retaining groove provided with a bottom extending radially outward beyond an outer diameter of the shroud. A radome is seated within the retaining groove. | 12-16-2010 |
20110291914 | SEGMENTED ANTENNA REFLECTOR WITH SHIELD - An antenna reflector includes a central segment with a peripheral coupling portion and a plurality of peripheral segments, each provided with a reflector portion and a shield portion. A proximal portion of each shield portion is dimensioned to couple with the peripheral coupling portion, a reflector portion edge of each peripheral segment is dimensioned to couple with adjacent reflector portion edges and a shield portion edge of each peripheral segment is dimensioned to couple with adjacent shield portion edges. The central segment and the reflector portion of the peripheral segments together form a reflector dish. The shield portions together provide a circumferential shield extending from a periphery of the reflector dish along an antenna boresight of the reflector dish. | 12-01-2011 |
Stephen W. Simms, Dunferminline GB
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20130057445 | LOW SIDELOBE REFLECTOR ANTENNA - A front feed reflector antenna with a dish reflector has a reflector focal length to reflector diameter ratio of less than 0.25. A wave guide is coupled to a proximal end of the dish reflector, projecting into the dish reflector along a longitudinal axis. A dielectric block is coupled to a distal end of the waveguide and a sub-reflector is coupled to a distal end of the dielectric block. A shield is coupled to the periphery of the dish reflector. The sub-reflector diameter is dimensioned to be 2.5 wavelengths or more of a desired operating frequency. | 03-07-2013 |