Patents by Inventor Peter Cleveland

Peter Cleveland 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).

  • Publication number: 20240150377
    Abstract: This disclosure provides modulators of Cystic Fibrosis Transmembrane Conductance Regulator (CFTR) having core structure (I), pharmaceutical compositions containing at least one such modulator, methods of treatment of CFTR mediated diseases, including cystic fibrosis, using such modulators and pharmaceutical compositions, combination pharmaceutical compositions and combination therapies employing those modulators, and processes and intermediates for making such modulators.
    Type: Application
    Filed: October 6, 2021
    Publication date: May 9, 2024
    Inventors: Jason MCCARTNEY, Alexander Russell ABELA, Sunny ABRAHAM, Corey Don ANDERSON, Vijayalaksmi ARUMUGAM, Jaclyn CHAU, Jeremy CLEMENS, Thomas CLEVELAND, Timothy Richard COON, Timothy A. DWIGHT, Lev Tyler Dewey FANNING, Bryan A. FRIEMAN, Peter GROOTENHUIS, Anton V. GULEVICH, Sara Sabina HADIDA RUAH, Yoshihiro ISHIHARA, Haripada KHATUYA, Paul KRENITSKY, Vito MELILLO, Mark Thomas MILLER, Prasuna PARASELLI, Fabrice PIERRE, Alina SILINA, Joe A. TRAN, Johnny UY, Lino VALDEZ, Troy VICKERS, Jinglan ZHOU
  • Publication number: 20230410024
    Abstract: A method for managing oilfield water. Oilfield water data is grouped into discrete and non-overlapping groups. Outliers are removed from the data. Features of the remaining data are analyzed to identify most discriminative feature. The data is separated into training data and testing data, and the training data is fit into a model that shows the best precision, accuracy and recall. The model is confirmed using the testing data. Upon confirmation of the accuracy of the model, the model is applied to data for a new proposed oilfield well, and a new proposed project is implemented or disapproved based on a result of the identified model that predicts water production of the new proposed oilfield well.
    Type: Application
    Filed: January 13, 2023
    Publication date: December 21, 2023
    Inventors: Forrest Charles WEBB, Wesley Peter CLEVELAND
  • Patent number: 11556882
    Abstract: A method for managing oilfield water. Oilfield water data is grouped into discrete and non-overlapping groups. Outliers are removed from the data. Features of the remaining data are analyzed to identify most discriminative feature. The data is separated into training data and testing data, and the training data is fit into a model that shows the best precision, accuracy and recall. The model is confirmed using the testing data. Upon confirmation of the accuracy of the model, the model is applied to data for a new proposed oilfield well, and a new proposed project is implemented or disapproved based on a result of the identified model that predicts water production of the new proposed oilfield well.
    Type: Grant
    Filed: June 17, 2021
    Date of Patent: January 17, 2023
    Assignee: SOURCEWATER, INC.
    Inventors: Forrest Charles Webb, Wesley Peter Cleveland
  • Publication number: 20210312349
    Abstract: A method for managing oilfield water. Oilfield water data is grouped into discrete and non-overlapping groups. Outliers are removed from the data. Features of the remaining data are analyzed to identify most discriminative feature. The data is separated into training data and testing data, and the training data is fit into a model that shows the best precision, accuracy and recall. The model is confirmed using the testing data. Upon confirmation of the accuracy of the model, the model is applied to data for a new proposed oilfield well, and a new proposed project is implemented or disapproved based on a result of the identified model that predicts water production of the new proposed oilfield well.
    Type: Application
    Filed: June 17, 2021
    Publication date: October 7, 2021
    Inventors: Forrest Charles WEBB, Wesley Peter CLEVELAND
  • Patent number: 10885798
    Abstract: Disclosed is an autopilot-coupled traffic alert and collision avoidance systems (AP TCAS). The AP TCAS includes a an AP/automatic flight control system (AFCS) that is configured to receive a vertical speed setting after the issuance of a preventive resolution advisory, wherein the aircraft vertical speed setting exceeds the maximum vertical speed allowed by the resolution advisory, the AP/AFCS being further configured to: (1) modify the aircraft vertical speed setting so as to be less than the maximum vertical speed, and relay the modified second aircraft vertical speed to an autopilot system of the aircraft to automatically cause the aircraft to fly at a vertical speed in accordance with the modified second vertical speed setting; and (2) relay a command to the autopilot system to initiate an automatic, corrective flight maneuver if a current vertical speed of the aircraft is within a predetermined amount of the maximum vertical speed.
    Type: Grant
    Filed: December 19, 2018
    Date of Patent: January 5, 2021
    Assignee: HONEYWELL INTERNATIONAL INC.
    Inventors: Ratan Khatwa, William Peter Cleveland, Bob D Crouse
  • Publication number: 20200184388
    Abstract: A method for managing oilfield water. Oilfield water data is grouped into discrete and non-overlapping groups. Outliers are removed from the data. Features of the remaining data are analyzed to identify most discriminative feature. The data is separated into training data and testing data, and the training data is fit into a model that shows the best precision, accuracy and recall. The model is confirmed using the testing data. Upon confirmation of the accuracy of the model, the model is applied to data for a new proposed oilfield well, and a new proposed project is implemented or disapproved based on a result of the identified model that predicts water production of the new proposed oilfield well.
    Type: Application
    Filed: February 14, 2020
    Publication date: June 11, 2020
    Inventors: Forrest Charles WEBB, Wesley Peter CLEVELAND
  • Patent number: 10565540
    Abstract: A method for managing oilfield water. Oilfield water data is grouped into discrete and non-overlapping groups. Outliers are removed from the data. Features of the remaining data are analyzed to identify most discriminative feature. The data is separated into training data and testing data, and the training data is fit into a model that shows the best precision, accuracy and recall. The model is confirmed using the testing data. Upon confirmation of the accuracy of the model, the model is applied to data for a new proposed oilfield well, and a new proposed project is implemented or disapproved based on a result of the identified model that predicts water production of the new proposed oilfield well.
    Type: Grant
    Filed: August 27, 2015
    Date of Patent: February 18, 2020
    Assignee: SOURCEWATER, INC.
    Inventors: Forrest Charles Webb, Wesley Peter Cleveland
  • Publication number: 20190114932
    Abstract: Disclosed is an autopilot-coupled traffic alert and collision avoidance systems (AP TCAS). The AP TCAS includes a an AP/automatic flight control system (AFCS) that is configured to receive a vertical speed setting after the issuance of a preventive resolution advisory, wherein the aircraft vertical speed setting exceeds the maximum vertical speed allowed by the resolution advisory, the AP/AFCS being further configured to: (1) modify the aircraft vertical speed setting so as to be less than the maximum vertical speed, and relay the modified second aircraft vertical speed to an autopilot system of the aircraft to automatically cause the aircraft to fly at a vertical speed in accordance with the modified second vertical speed setting; and (2) relay a command to the autopilot system to initiate an automatic, corrective flight maneuver if a current vertical speed of the aircraft is within a predetermined amount of the maximum vertical speed.
    Type: Application
    Filed: December 19, 2018
    Publication date: April 18, 2019
    Applicant: HONEYWELL INTERNATIONAL INC.
    Inventors: Ratan Khatwa, William Peter Cleveland, Bob D. Crouse
  • Patent number: 10192453
    Abstract: Disclosed is an autopilot-coupled traffic alert and collision avoidance systems (AP TCAS). The AP TCAS includes a an AP/automatic flight control system (AFCS) that is configured to receive a vertical speed setting after the issuance of a preventive resolution advisory, wherein the aircraft vertical speed setting exceeds the maximum vertical speed allowed by the resolution advisory, the AP/AFCS being further configured to: (1) modify the aircraft vertical speed setting so as to be less than the maximum vertical speed, and relay the modified second aircraft vertical speed to an autopilot system of the aircraft to automatically cause the aircraft to fly at a vertical speed in accordance with the modified second vertical speed setting; and (2) relay a command to the autopilot system to initiate an automatic, corrective flight maneuver if a current vertical speed of the aircraft is within a predetermined amount of the maximum vertical speed.
    Type: Grant
    Filed: July 13, 2016
    Date of Patent: January 29, 2019
    Assignee: HONEYWELL INTERNATIONAL INC.
    Inventors: Ratan Khatwa, William Peter Cleveland, Bob D Crouse
  • Publication number: 20180018885
    Abstract: Disclosed is an autopilot-coupled traffic alert and collision avoidance systems (AP TCAS). The AP TCAS includes a an AP/automatic flight control system (AFCS) that is configured to receive a vertical speed setting after the issuance of a preventive resolution advisory, wherein the aircraft vertical speed setting exceeds the maximum vertical speed allowed by the resolution advisory, the AP/AFCS being further configured to: (1) modify the aircraft vertical speed setting so as to be less than the maximum vertical speed, and relay the modified second aircraft vertical speed to an autopilot system of the aircraft to automatically cause the aircraft to fly at a vertical speed in accordance with the modified second vertical speed setting; and (2) relay a command to the autopilot system to initiate an automatic, corrective flight maneuver if a current vertical speed of the aircraft is within a predetermined amount of the maximum vertical speed.
    Type: Application
    Filed: July 13, 2016
    Publication date: January 18, 2018
    Applicant: HONEYWELL INTERNATIONAL INC.
    Inventors: Ratan Khatwa, William Peter Cleveland, Bob D. Crouse
  • Publication number: 20160063402
    Abstract: A method for managing oilfield water. Oilfield water data is grouped into discrete and non-overlapping groups. Outliers are removed from the data. Features of the remaining data are analyzed to identify most discriminative feature. The data is separated into training data and testing data, and the training data is fit into a model that shows the best precision, accuracy and recall. The model is confirmed using the testing data. Upon confirmation of the accuracy of the model, the model is applied to data for a new proposed oilfield well, and a new proposed project is implemented or disapproved based on a result of the identified model that predicts water production of the new proposed oilfield well.
    Type: Application
    Filed: August 27, 2015
    Publication date: March 3, 2016
    Applicant: DIGITAL H2O, INC.
    Inventors: Forrest Charles WEBB, Wesley Peter CLEVELAND
  • Publication number: 20060073014
    Abstract: An article of manufacture having a nominal profile substantially in accordance with Cartesian coordinate values of X, Y and Z set forth in a table. The table selected from the group of tables consisting of TABLES 1S-16S, 1R-17R, and IGV. Wherein X and Y are distances in inches which, when connected by smooth continuing arcs, define airfoil profile sections at each distance Z in inches. The profile sections at the Z distances being joined smoothly with one another to form a complete airfoil shape.
    Type: Application
    Filed: November 12, 2004
    Publication date: April 6, 2006
    Applicant: General Electric Company
    Inventors: Steven Tomberg, Roger Beharrysingh, Timothy DeJoris, William Miller, Paul Deivernois, Venkata Siva Chaluvadi, Adrian Mistreanu, Michael Dutka, Nathan Race, Jeffrey Boyd, Christopher McGowan, Peter Cleveland, Jason Harrell, Carl Schott, John Stampfli, Ronald Denmark, Steven Schirle, Jennifer Michenfelder, John Ryman
  • Publication number: 20050106025
    Abstract: A turbine bucket airfoil has a conical fillet about the intersection of the airfoil tip and tip shroud having a nominal profile in accordance with coordinate values of X and Y, offset 1, offset 2 and Rho set forth in Table I. The shape parameters of offset 1, offset 2 and Rho define the configuration of the fillet at the specified X and Y locations about the fillet to provide a fillet configuration accommodating high localized stresses. The fillet shape may be parabolic, elliptical or hyperbolic as a function of the value of the shape parameter ratio of D1 D1 + D2 at each X, Y location where D1 is a distance between an intermediate point along a chord between edge points determined by offsets O1 and O2 and a shoulder point on the fillet surface and D2 is a distance between the shoulder point and an apex location at the intersection of the airfoil tip and tip shroud.
    Type: Application
    Filed: September 5, 2003
    Publication date: May 19, 2005
    Applicant: General Electric Company
    Inventors: Daniel Snook, Peter Cleveland
  • Publication number: 20050031453
    Abstract: Third stage turbine buckets have airfoil profiles substantially in accordance with Cartesian coordinate values of X, Y and Z set forth Table I wherein X and Y values are in inches and the Z values are non-dimensional values from 0.03 span to 0.95 span convertible to Z distances in inches by multiplying the Z values by the height of the airfoil in inches. The X and Y values are distances which, when connected by smooth continuing arcs, define airfoil profile sections at each distance Z. The profile sections at each distance Z are joined smoothly to one another to form the bucket airfoil shape. The X, Y and Z distances may be scalable as a function of the same constant or number to provide a scaled up or scaled down airfoil section for the bucket. The nominal airfoil given by the X, Y and Z distances lies within an envelop of ±0.150 inches in directions normal to the surface of the airfoil.
    Type: Application
    Filed: August 4, 2003
    Publication date: February 10, 2005
    Inventors: Daniel Snook, Robert By, Bruce Smith, Gunnar Siden, Carlos Collado, Peter Cleveland
  • Publication number: 20050031449
    Abstract: A turbine stage one bucket has an airfoil having a plurality of cooling holes passing through the airfoil from 0% span to 100% span whereby cooling air exits the airfoil tip into the hot gas path. X and Y coordinate values are given in Table I, locating the holes relative to the airfoil profile at airfoil profile sections of 5%, 50% and 90% span, Table I also giving the hole diameters. In this manner, cooling hole optimization for this turbine bucket airfoil is achieved. The cooling holes are also located in relation to the profile of the bucket airfoil given by the X, Y and Z coordinate values of Table II, the two coordinate systems having the same origin.
    Type: Application
    Filed: August 7, 2003
    Publication date: February 10, 2005
    Inventors: Peter Cleveland, Thomas Beddard
  • Publication number: 20050013692
    Abstract: A turbine bucket includes a bucket airfoil having a tip shroud with leading and trailing edges defining leading and trailing edge profiles substantially in accordance with Cartesian coordinate values of X and Y at points 12-20 and 1-11, respectively, set forth in Table I. The X and Y values are distances in inches which, when respective points 12-20 and 1-11 are connected by smooth, continuing arcs, define the leading and trailing edge tip shroud profiles. An airfoil profile at 95% span is defined by Cartesian coordinate values of X, Y and Z in Table II having the same X, Y origin along the radial Z axis as the origin of Table I. The profiled leading and trailing edges of the tip shroud relative to the airfoil profile afford optimum tip shroud mass distribution which maximizes creep life of the bucket. Stage efficiency is also improved by providing a tip shroud covering the airfoil throat.
    Type: Application
    Filed: July 17, 2003
    Publication date: January 20, 2005
    Inventors: Daniel Snook, Peter Cleveland