Patents by Inventor Christopher P Fell
Christopher P Fell has filed for patents to protect the following inventions. This listing includes patent applications that are pending as well as patents that have already been granted by the United States Patent and Trademark Office (USPTO).
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Publication number: 20240101553Abstract: The present invention relates to compounds that inhibit KRas G12C. In particular, the present invention relates to compounds that irreversibly inhibit the activity of KRas G12C, pharmaceutical compositions comprising the compounds and methods of use therefor.Type: ApplicationFiled: August 4, 2023Publication date: March 28, 2024Inventors: Matthew Arnold MARX, James Gail CHRISTENSEN, Christopher Ronald SMITH, James F. BLAKE, Laurence E. BURGESS, Mark Joseph CHICARELLI, Adam COOK, Jay Bradford FELL, John P. FISCHER, Macedonio J. MEJIA, Martha E. RODRIGUEZ, Pavel SAVECHENKOV, Tony P. TANG, Guy P.A. VIGERS
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Patent number: 7637156Abstract: A vibrator 10, which is formed in a silicon wafer 1 by means of MEMS technique, has eight beam portions (beams) 12 supported at a central portion 11 and extending in the radial direction while mutually keeping the same angle and has a ring portion 13 connected to the eight beam portions 12. Outside the ring portion 13, eight electrodes 21a to 21h for electrostatic actuation, capacitance detection, or the like are spaced uniformly with a gap 22 created between the ring portion 13 and the electrodes 21a to 21h. Inside the ring portion 13, sixteen electrodes 23 for frequency adjustment are spaced uniformly with a gap 24 created between the ring portion 13 and the electrodes 23.Type: GrantFiled: July 12, 2005Date of Patent: December 29, 2009Assignees: Sumitomo Precision Products, Atlantic Inertial Systems LimitedInventors: Ryuta Araki, Osamu Torayashiki, Toru Kitamura, Hiroshi Kawasaki, Tsuyoshi Takemoto, Koji Nakamura, Christopher P. Fell, Kevin Townsend, Ian Sturland
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Patent number: 7219529Abstract: Apparatus for measuring variation in scalefactor from a predetermined value for a vibrating structure gyroscope has a vibrating structure (R), fixed primary and fixed secondary drives (1, 13) for putting and maintaining the vibrating structure (R) in vibrating resonance, fixed primary and fixed secondary pick offs (2, 6) for detecting vibration of the vibrating structure (R), with the drives and pick offs (1, 13, 2, 6) being located radially around the vibrating structure (R), quadrature component and real component loop systems (7, 8), automatic gain control and phase locked loop systems (5, 22), a sin/cos pick off resolver (38) for receiving signals from the primary and secondary pick offs (2, 6) and for outputting signals to the quadrature component and real component loop systems (7, 8) and to the automatic gain control and phase locked loop systems (5, 22), a sin/cos drive resolver (37) for receiving output signals from the quadrature component and real component loop systems (7, 8) and from the automatiType: GrantFiled: November 12, 2003Date of Patent: May 22, 2007Assignee: BAE Systems plcInventors: Christopher P Fell, Kevin Townsend, Andrew Kazar
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Patent number: 6978674Abstract: A two axis gyroscope including a substantially planar vibratory resonator (5) having a substantially ring or hoop-like structure with inner and other peripheries extending around a common axis, carrier mode drive (22) for causing the resonator (5) to vibrate in a cosn? vibration mode, carrier mode pick-off (23) for sensing movement of the resonator (5) in response to the carrier mode drive (22), X-axis response mode pick-off (25) for detecting movement of the resonator in response to rotation about the X-axis, X-axis response mode drive (24) for nulling said motion, y-axis response mode pick-off (27) for detecting movement of the resonator in response to rotation about the y-axis, y-axis response mode drive (26) for nulling said motion, and a support (9) for flexibly supporting the resonator (5) and for allowing the resonator to vibrate relative to the support (9) in response to the carrier mode drive (22) and to applied rotation, wherein the support (9) comprises only L legs, where, when L is even: L=2N/K,Type: GrantFiled: September 6, 2002Date of Patent: December 27, 2005Assignee: BAE Systems plcInventors: Christopher P Fell, Rebecka Eley, Colin H. J. Fox, Stewart McWilliam
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Patent number: 6883374Abstract: A three axis rate sensor includes a substantially planar vibratory resonator having a substantially ring or hoop-like structure with inner and outer peripheries extending around a common axis, drive means for causing the resonator to vibrate in a Cos 2? vibration mode, carrier mode pick-off means for sensing movement of the resonator in response to the applied drive z-axis response mode, pick-off means for detecting movement of the resonator in response to rotation about the z-axis, z-axis response mode drive means for nulling said motion, x-axis response mode pick-off mean for detecting movement of the resonator in response to rotation about the x-axis, x-axis response mode drive means for nulling said motion, y-axis response mode pick-off mean for detecting movement of the resonator in response to rotation about the y-axis, y-axis response mode drive means for nulling said motion, and support means for flexibly supporting the resonator and for allowing the resonator to vibrate relative to the support meansType: GrantFiled: September 6, 2002Date of Patent: April 26, 2005Assignee: BAE Systems plcInventors: Christopher P Fell, Rebecka Eley, Colin H. J. Fox, Stewart McWilliam
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Patent number: 6848305Abstract: A three axis sensor including a substantially planar vibrator resonator or having a substantially ring or hoop like structure with inner and outer peripheries e tending around a common axis, drive means for causing the resonator to vibrate in an in lane cos 2? vibration mode, carrier mode pick-off means for sensing movement of the resonator in response to said drive means, pick-off means for sensing in plane sin 2? resonator motion induced by rotation about the z-axis, drive means for nulling said motion, pick-off means for sensing out of plane sin 3? resonator motion induced by rotation about the x-axis, drive means for nulling said motion, pick-off means for sensing out of plane cos 3? resonator motion induced by rotation about the y-axis, drive means for nulling said motion, and support means for flexibly supporting the resonator and for allowing the resonator to vibrate relative to the support means in response to the drive means and to applied rotations, wherein the support means comprises only L supportType: GrantFiled: September 6, 2002Date of Patent: February 1, 2005Assignee: BAE Systems plcInventors: Christopher P Fell, Rebecka Eley, Colin H. J. Fox, Stewart McWilliam
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Patent number: 6805007Abstract: A vibrating structure gyroscope comprises a resonant body, a drive transducer for driving resonant motion of the body, a pick-off for producing signals representative of the resonant motion, and a signal processor for extracting z-axis orientation information and x- and y-axis rate information from the signals. The resonant body is planar and the resonant motion takes place in a vibration mode pattern whose orientation angle with respect to the body varies in accordance with z-axis orientation of the body and couples energy into an out-of-plane response mode motion in accordance with rotation of the body about the x- or y-axis. The signal processor resolves the out-of-plane response mode motion with reference to a z-axis orientation signal to extract the x- and y-axis rate information.Type: GrantFiled: July 23, 2002Date of Patent: October 19, 2004Assignee: BAE Systems plcInventors: Christopher P Fell, Kevin Townsend
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Publication number: 20040144174Abstract: A three axis rate sensor includes a substantially planar vibratory resonator (5) having a substantially ring or hoop-like structure with inner (6) and outer peripheries extending around a common axis, drive means (22) for causing the resonator to vibrate in a Cos 2&thgr; vibration mode, carrier mode pick-off means (23) for sensing movement of the resonator (5) in response to the applied drive means, x-axis, y-axis and z-axis response mode, pick-off means (25, 27, 31) for detecting movement of the resonator in response to rotation about the x-axis, y-axis and z-axis, x-axis, y-axis and z-axis response mode drive means (24, 26, 30) for nulling said motion and support means (9) for flexibly supporting the resonator and for allowing the resonator (5) to vibrate relative to the support means (9) in response to the drive means (22) and the applied rotation wherein the support means (9) comprises only L support beams, where L≠2 k, and k=0, 1, 2 or 3.Type: ApplicationFiled: October 22, 2003Publication date: July 29, 2004Inventors: Christopher P Fell, Rebecka Eley, Colin H.J. Fox, Stewart McWilliam
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Publication number: 20040134278Abstract: A two axis gyroscope including a planar vibratory resonator (5) having a ring or hoop-like structure, carrier mode drive means (22) for causing the resonator (5) to vibrate in a cos n&thgr; vibration mode, carrier mode pick-off means (23) for sensing movement of the resonator (5), X-axis response mode pick-off means (25; 27) for detecting movement of the resonator in response to rotation about the x-axis and y-axis; x-axis and y-axis response mode drive means (24; 26) for nulling said motions and support means (9) for flexibly supporting the resonator (5) and for allowing the resonator to vibrate relative to the support means (9) in response to the drive means (22) and to applied rotation; wherein the support (9) means comprises only L legs, where, when L is even: L=2N/K, and where, when L is odd: L=N/K, where K is an integer, L>2 and N is the carrier mode order.Type: ApplicationFiled: October 16, 2003Publication date: July 15, 2004Inventors: Christopher P Fell, Rebecka Eley, Colin H J Fox, Stewart McWilliam
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Publication number: 20040118205Abstract: A single axis rate sensor including a substantially planar vibratory resonator (1) having a substantially ring or hoop-like structure with inner and outer peripheries (1a, 1b) extending around a common axis (z) drive means (6) for causing the resonator (1) to vibrate in a Cos 2&thgr; vibration mode, carrier mode pick-off means (7) for sensing movement of the resonator (1) in response to said drive means pick-off means (9) for detecting Sin 2&thgr; vibration mode motion induced by rotation around the Z-axis, Sin 2&thgr; vibration mode drive means (8) for nulling said motion and support means (2) for flexibly supporting the resonator (1) and for allowing the resonator (1) to vibrate relative to the support means (2) in response to the drive means, or to applied rotation wherein the support means comprises only L support beams, where L≠2K, and K=0, 1,2 or 3.Type: ApplicationFiled: October 16, 2003Publication date: June 24, 2004Inventors: Christopher P Fell, Rebecka Eley, Colin H J Fox
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Patent number: 6651499Abstract: A vibrating structure gyroscope having a vibrating structure (3) primary drive means (4) and secondary drive means (7) and primary pick-off means (2) an secondary pick-off means (6) is provided with a control system. The control system includes a primary closed control loop (1) for controllably varying the drive signal applied to the primary drive means (4), a secondary closed control loop (5) for controllably varying the drive signal applied to the secondary drive means (7) in order to maintain a null value of the secondary pick-off means (6) and means (30) for actively adjusting the scalefactor in the primary and secondary closed control loops (1, 5). The means (30) includes means (34) for dividing a rate response signal from the loop (5) by a signal indicative of the amplitude of the primary mode vibration. The output form the means (34) is filtered to provide an applied rate output.Type: GrantFiled: September 17, 2002Date of Patent: November 25, 2003Assignee: BAE Systems plcInventors: Christopher P Fell, Kevin Townsend
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Publication number: 20030074968Abstract: A vibrating structure gyroscope having a vibrating structure (3) primary drive means (4) and secondary drive means (7) and primary pick-off means (2) and secondary pick-off means (6) is provided with a control system. The control system includes a primary closed control loop (1) for controllably varying the drive signal applied to the primary drive means (4), a secondary closed control loop (5) for controllably varying the drive signal applied to the secondary drive means (7) in order to maintain a null value of the secondary pick-off means (6) and means (30) for actively adjusting the scalefactor in the primary and secondary closed control loops (1, 5). The means (30) includes means (34) for dividing a rate response signal from the loop (5) by a signal indicative of the amplitude of the primary mode vibration. The output form the means (34) is filtered to provide an applied rate output.Type: ApplicationFiled: September 17, 2002Publication date: April 24, 2003Inventors: Christopher P Fell, Kevin Townsend
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Publication number: 20030056588Abstract: A vibrating structure gyroscope comprises a resonant body, drive transducer means for driving resonant motion of the body, pick-off means for producing signals representative of the resonant motion, and signal processing means for extracting z-axis orientation information and x- and y-axis rate information from the signals. The resonant body is planar and the resonant motion takes place in a vibration mode pattern whose orientation angle with respect to the body varies in accordance with z-axis orientation of the body and couples energy into an out-of-plane response mode motion in accordance with rotation of the body about the x- or y-axis. Signal processing means resolves the out-of-plane response mode motion with reference to a z-axis orientation signal to extract the x- and y-axis rate information.Type: ApplicationFiled: July 23, 2002Publication date: March 27, 2003Inventors: Christopher P Fell, Kevin Townsend
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Publication number: 20030000306Abstract: An angular rate sensor device (10) such as a micro-machined vibrating structure gyroscope, comprises a resonator (16), drive means (18), sensing means (20) and associated electronic control means. The resonator (16), drive means (18), sensing means (20) and control means are fabricated from a layer of crystalline silicon (12) having a [100] principal crystal plane. In order to make the resonator (16) operate in this type of material without degrading its performance, the resonator (16) is arranged to be operated by the drive and sensing means (18, 20) under the control of the electronic control means with a vibration mode pair having modal parameters, such as Young's Modulus, matched to provide a consistent resonator response. In particular, the resonator (16) is arranged to be operated with a Sin 3&thgr;/Cos 3&thgr; (vibration mode pair providing degenerate carrier and response parameters.Type: ApplicationFiled: July 8, 2002Publication date: January 2, 2003Inventor: Christopher P Fell
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Patent number: 6471883Abstract: A vibrating structure gyroscope having a silicon substantially planar ring vibrating structure (1) capacitive means for imparting drive motion to and sensing motion of the vibrating structure (1), and a screen layer (15) surrounding the capacitive means is made by depositing photoresist material (9) on a glass or silicon substrate (7), hardening, patterning and developing the photoresist (9) to expose areas of the substrate (7), etching the exposed areas to form cavities (10) therein, stripping any remaining photoresist material (9) attaching a silicon layer (8) to the cavitated substrate (7) depositing a layer of aluminium on the silicon layer (8), depositing photoresist material on the aluminium layer, hardening, patterning and developing the photoresist layer to expose areas of the aluminium layer, etching the exposed areas of the aluminium layer to leave regions of aluminium on the silicon layer providing bond pads (11, 12, 13 and 14), stripping the remaining photoresist from the aluminium layer, depositiType: GrantFiled: December 22, 1999Date of Patent: October 29, 2002Assignee: BAE Systems PLCInventors: Christopher P Fell, Kevin Townsend, Ian Sturland
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Patent number: 6282958Abstract: An angular rate sensor or gyro includes a ring-like resonator (1) mounted by support beams (2) extending from the inner periphery of the ring (1) to a boss (4) on a base (3). The support beams (2) are flexible and allow the resonator (1) to vibrate in response to an electrostatic drive (6, 8) in a substantially undamped oscillation mode to permit the resonator to move relative to the support in response to turning rate. The support beams (2) and resonator (1) are made from crystalline silicon. Electrostatic sensors (7, 9) are provided for sensing movement of the resonator (1). The drive (6, 8) and sensors (7, 9) have plate-like elements made from crystalline silicon having surfaces located substantially normal to the plane of the resonator (1) at a spacing from the adjacent outer periphery of the resonator (1).Type: GrantFiled: October 13, 1999Date of Patent: September 4, 2001Assignee: BAE Systems plcInventors: Christopher P Fell, Kevin Townsend, Ian D Hopkin
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Patent number: 5739410Abstract: Vibration mode frequencies of a vibrating structure gyroscope sensing element are matched by removing and/or adding a desired variable amount of material from or to the sensing element (1) at at least one point (4) on or in the vicinity of the neutral axis (5).Type: GrantFiled: December 11, 1996Date of Patent: April 14, 1998Assignee: British Aerospace Public Limited CompanyInventor: Christopher P. Fell