Gary G Larson

US Patent:

8293911, Oct 23, 2012

Filed:

Aug 22, 2007

Appl. No.:

11/894877

Inventors:

Jean-Michel Vernier - Laguna Niguel CA, US
Martha Alicia De La Rosa - San Diego CA, US
Huanming Chen - Irvine CA, US
Jim Zhen Wu - Aliso Viejo CA, US
Gary Lee Larson - Cypress CA, US
Ian Wayne Cheney - Mission Viejo CA, US

Assignee:

Valeant Pharmaceuticals International - Aliso Viejo CA

International Classification:

C07D 217/02
C07D 217/22
A61K 31/472

US Classification:

546144, 514307, 514309, 546141

Abstract:

This invention provides a compound of formula IA.

US Patent:

20110003850, Jan 6, 2011

Filed:

Feb 1, 2010

Appl. No.:

12/698070

Inventors:

Jean-Michel Vernier - Laguna Niguel CA, US
Martha Alicia De La Rosa - Durham NC, US
Huanming Chen - Irvine CA, US
Jim Zhen Wu - Shanghai, CN
Gary Lee Larson - Cypress CA, US
Ian Wayne Cheney - Mission Viejo CA, US

Assignee:

Valeant Pharmaceuticals International, Inc. - Aliso Viejo CA

International Classification:

A61K 31/472
C07D 217/04
A61P 43/00

US Classification:

514307, 546144

Abstract:

This invention provides a compound of formula IAwhere X=0 or S; Y is 0 or S; q=1 or 0; and other substituents are defined herein. Such compounds can affect the opening of, or otherwise modulate, voltage-gated potassium channels. Such compounds useful for the treatment and prevention of diseases and disorders which are affected by activation or modulation of potassium ion channels. One such condition is seizure disorders.

US Patent:

20220349406, Nov 3, 2022

Filed:

Apr 30, 2021

Appl. No.:

17/246479

Inventors:

- El Segundo CA, US
GARY L. LARSON - SEAL BEACH CA, US
ROBERT W. DELLER - ST. GEORGE UT, US

Assignee:

Federal Industries, Inc. - El Segundo CA

International Classification:

F04D 13/04
B64D 39/02
F04D 15/00

Abstract:

A fuel pump system for an aerial refueling system including: a variable displacement motor operable to be driven by a hydraulic fluid pressure; a fuel pump operable to be driven by the variable displacement motor; and a drive system controller (DSC) connected to the variable displacement motor, wherein the DSC is operable to direct an operation of the fuel pump in modes comprising: a flow control mode operable to maintain an output fuel flow rate from the fuel pump to a predetermined maximum inlet pressure at a reception coupling for a receiver aircraft; a fuel pressure control mode operable to regulate the output fuel flow rate to not exceed the predetermined maximum inlet pressure; and a priority mode operable to reduce the output fuel flow rate in response to a decrease in the hydraulic pressure. Also a method of refueling a receiver aircraft.