Raison
Bertrand Raison, Saint-Martin-D'Heres FR
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20140098450 | PROTECTION RELAY SYSTEM AGAINST SINGLE-PHASE FAULTS FOR MEDIUM-VOLTAGE DISTRIBUTION NETWORKS - The electrical power distribution network comprises a medium-voltage feeder having an upstream end intended to be connected to a power source. The feeder includes at least first and second consecutive protection relays positioned along the feeder and defining the ends of a first element to be monitored. The first protection relay includes a search module configured to trip a breaker to interrupt the electrical power distribution: | 04-10-2014 |
Fabien Raison, Plaisance Du Touch FR
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20100043450 | SYSTEM FOR ATTACHING AN ENGINE TO THE STRUCTURE OF AN AIRCRAFT, SUCH AS A SAIL WING AIRCRAFT - System for attaching an engine to the structure of an aircraft, such as a sail wing aircraft. The system includes an upper beam which is firmly fixed at its front end to a first frame mounted on the aircraft structure. The upper beam is in addition firmly fixed at its median part to a second frame located to the rear of the first frame. The engine is hooked beneath the upper beam. The system is orientated in relation to a longitudinal axis X, a transverse axis Y and a vertical axis Z. Two front engine attachment points are arranged symmetrically on either side of the vertical median plane of the engine. The front attachment points include a shaft ( | 02-25-2010 |
20100108802 | SAIL WING AIRCRAFT WHICH INCLUDES AN ENGINE MOUNTED ON A PYLON - Sail wing aircraft which includes a wing ( | 05-06-2010 |
20110036942 | ENGINE ATTACHMENT PYLON COMPRISING MEANS OF FASTENING SPARS AND PANELS LOCATED OUTSIDE THE INNER SPACE IN THE BOX - An engine attachment pylon for an aircraft including a rigid structure including a box including an upper spar and a lower spar, connected to each other through two lateral panels. At least one of the upper and lower ends of the web of at least one of the two lateral panels includes at least one assembly cleat projecting sideways from the web towards the outside of the box, and assembled to the spar on which it bears through an attachment mechanism located outside the inner space in the box. | 02-17-2011 |
20110036943 | AIRCRAFT ENGINE ATTACHMENT PYLON COMPRISING A BOX WITH A CIRCULAR OR ELLIPTICAL SHAPED SECTION - An engine attachment pylon for an aircraft, including a rigid structure including a box formed by one or plural hollow segments. The section of at least one hollow segment is circular or elliptical in shape. | 02-17-2011 |
20110290935 | METHOD OF MANUFACTURE BY SUPERPLASTIC FORMING AND BY FISHPLATING OF A RIB FOR AN AERODYNAMIC FAIRING OF AN AIRCRAFT ENGINE MOUNTING PYLON - The present invention relates to a method of manufacture of a stiffening transverse internal rib for an aerodynamic fairing of an engine mounting device, including: | 12-01-2011 |
20110290936 | METHOD OF MANUFACTURE BY SUPERPLASTIC FORMING AND BY FISHPLATING OF A RIB FOR AN AERODYNAMIC FAIRING OF AN AIRCRAFT ENGINE MOUNTING PYLON - The present invention relates to a method of manufacture of a group of transverse internal stiffening ribs ( | 12-01-2011 |
20130174572 | METHOD FOR COOLING A THERMAL PROTECTION FLOOR OF AN AFT AERODYNAMIC FAIRING OF A STRUCTURE FOR MOUNTING AN AIRCRAFT PROPULSION SYSTEM - A propulsion system for an aircraft, including a dual-flow turbojet and a mounting structure for mounting this turbojet on the wing surface or on the fuselage of an aircraft. The mounting structure includes an aft aerodynamic fairing including a thermal protection floor to protect the mounting structure from the heat of a primary airstream channelled by an exhaust nozzle of the turbojet, as well as an air inlet provided in a longitudinal aerodynamic wall washed by a secondary airstream of the turbojet and delimiting together with an other similar wall a cavity isolated from the secondary airstream for extracting a cooling airstream from the secondary airstream, and air circulation means fed by the air inlet and having at least one outlet aperture emerging in a space between the thermal protection floor and the exhaust nozzle. | 07-11-2013 |
20130320135 | AFT AERODYNAMIC FAIRING WITH IMPROVED THERMAL RESISTANCE FOR A PYLON FOR ATTACHING AN AIRCRAFT PROPELLING ASSEMBLY - An aft aerodynamic fairing for a pylon for attaching an aircraft propelling assembly, including a caisson structure, a heat-shield floor, as well as a support structure for this floor comprising linking parts arranged to link two side edges of this floor to the caisson structure. The linking parts of each side edge of the floor are configured so as to allow travelling motion of the side edge relative to the caisson structure in a corresponding direction included in a plane orthogonal to a longitudinal direction of the fairing. The linking parts form a sliding link between the floor and the caisson structure, reducing the stresses induced by the deformations of these elements in use. | 12-05-2013 |
Fabien Raison, Toulouse FR
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20130221157 | AIRCRAFT ENGINE PYLON AFT AERODYNAMIC FAIRING - An aircraft engine pylon aft aerodynamic fairing includes upper spars, transverse stiffening ribs, lower spars and a trailing edge where the upper spars and lower spars join together. In this fairing, a profiled structure is formed according to a profile open to the outside of the fairing. In a first end portion, the profiled structure comes to be enclosed between an end portion of the lower spars and the ends of at least one transverse stiffening ribs flush with the lower spars. This structure extends between the lower spars and the upper spars over a straight central portion inclined relative to the first end portion, and comes in a second end portion flush against a portion of the upper spars, parallel to the first end. | 08-29-2013 |
Martin Jean Raison, Stanford, CA US
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20140344265 | Personalizing Default Search Queries on Online Social Networks - In one embodiment, a method includes accessing a social graph that includes a plurality of nodes and edges. A first node corresponds to a first user associated with an online social network and second nodes correspond to a concept or a second user. The method further comprises scoring a first set of nodes of the second nodes based on user-engagement factors. The method further comprises identifying common nodes that are connected by edges to nodes of the first set of nodes that have a score greater than a threshold score. The method further comprises generating structured queries and sending the structured queries to the user, the sent structured queries being a personalized query. | 11-20-2014 |
Maxime Raison, Montreal CA
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20160045139 | METHOD AND SYSTEM FOR DECOMPOSING SUPERIMPOSED GROUND REACTION FORCES INTO INDIVIDUAL FORCE PROFILES - A method for decomposing a GRF into individual force profiles, comprising: receiving a global GRF measured while a subject performs at least one movement on the force platform, the movement comprising at least two motion configurations; identifying individual time regions contained in the time measurement of the global GRF and assigning a respective one of the at least two motion configurations to each time region using a logical order of motion configurations and an identification of a reference motion configuration; for each time region, determining an individual GRF for each one of the at least two support contacts using the identification of the motion configuration for the time region and the global GRF, thereby determining a contribution of each one of the at least two support contacts to the global GRF; and outputting the individual GRFs. | 02-18-2016 |
Paul Raison, Windham, NH US
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20110154440 | DYNAMIC HOST CONFIGURATION PROTOCOL (DHCP) AUTHENTICATION USING CHALLENGE HANDSHAKE AUTHENTICATION PROTOCOL (CHAP) CHALLENGE - A method performed by a Dynamic Host Configuration Protocol (DHCP) server comprising receiving a DHCP DISCOVER message from a DHCP client; generating a challenge in response to the DHCP DISCOVER message; sending the challenge to an authentication device; receiving a first challenge response from the authentication device; generating a DHCP OFFER message; sending the challenge to the DHCP client in the DHCP OFFER message; receiving a DHCP REQUEST message that includes a second challenge response from the DHCP client; comparing the first challenge response with the second challenge response; and authenticating the DHCP client when the first challenge response and the second challenge response match. | 06-23-2011 |
Robert L. Raison, New South Wales AU
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20120114555 | METHOD FOR TREATING IMMUNE DISORDERS - The present invention relates to the treatment of B-cell mediated immune disorders such as rheumatoid arthritis, systemic lupus erythromatomus, diabetes mellitus, and multiple sclerosis. In particular, the present invention relates to the treatment of B-cell mediated immune disorders using antibodies which bind to membrane-bound free light chain expressed on the surface of plasma cell precursors. | 05-10-2012 |
Robert Lindsay Raison, New South Wales AU
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20080199463 | METHOD FOR TREATING MULTIPLE MYELOMA - The present invention relates to methods for the treatment of multiple myeloma. More particularly, the present invention relates to a method for inducing apoptosis in myeloma cells by administration of a K121-like antibody. | 08-21-2008 |
20090263358 | METHOD FOR TREATING MULTIPLE MYELOMA - The present invention relates to methods for the treatment of multiple myeloma. More particularly, the present invention relates to a method for inducing apoptosis in myeloma cells by administration of a K121-like antibody. | 10-22-2009 |