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Cartesian Coordinates

Cartesian Coordinates-related patent applications - as published by the U.S. Patent and Trademark Office (USPTO).


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Chronostratigraphic medeling and mapping system and method
March 08, 2018 - N°20180068037

A chronostratigraphic database comprising a plurality of discrete data points, wherein each data point comprises an x, y, z and t value, wherein x, y, and z are cartesian coordinates describing a position and t is a geologic time event relative to said position; a method to produce a chronostratigraphic database and to utilize the database; and a modeling system ...
Optimized aerodynamic profile for an arm of a structural casing of a turbine, and structural ...
Safran Aircraft Engines
January 18, 2018 - N°20180016940

When cold and in the non-coated state, the aerodynamic profile is substantially identical to a nominal profile determined by the cartesian coordinates x,y, zadim given in table 1, in which the coordinate zadim is the quotient d/h where d is the distance of the point under consideration from a first reference plane p0 situated at the base of the ...
Optimized aerodynamic profile for an arm of a structural casing of a turbine, and structural ...
Safran Aircraft Engines
January 18, 2018 - N°20180016926

When cold and in the non-coated state, the aerodynamic profile is substantially identical to a nominal profile determined by the cartesian coordinates x,y, zadim given in table 1, in which the coordinate zadim is the quotient d/h where d is the distance of the point under consideration from a first reference plane p0 situated at the base of the ...
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Optimized aerodynamic profile for a turbine blade, in particular for a rotary wheel of the ...
Safran Aircraft Engines
January 18, 2018 - N°20180016913

When cold and in the non-coated state, the aerodynamic profile is substantially identical to a nominal profile determined by the cartesian coordinates x,y, zadim given in table 1, in which the coordinate zadim is the quotient d/h where d is the distance of the point under consideration from a first reference plane p0 situated at the base of the ...
Optimized aerodynamic profile for a turbine blade, in particular for a rotary wheel of the ...
Safran Aircraft Engines
January 18, 2018 - N°20180016911

When cold and in the non-coated state, the aerodynamic profile is substantially identical to a nominal profile determined by the cartesian coordinates x,y, zadim given in table 1, in which the coordinate zadim is the quotient d/h where d is the distance of the point under consideration from a first reference plane p0 situated at the base of the ...
Optimized aerodynamic profile for a turbine blade, in particular for a rotary wheel of the ...
Safran Aircraft Engines
January 18, 2018 - N°20180016910

When cold and in the non-coated state, the aerodynamic profile is substantially identical to a nominal profile determined by the cartesian coordinates x,y, zadim given in table 1, in which the coordinate zadim is the quotient d/h where d is the distance of the point under consideration from a first reference plane p0 situated at the base of the ...
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Optimized aerodynamic profile for a turbine blade, in particular for a rotary wheel of the ...
Safran Aircraft Engines
January 18, 2018 - N°20180016908

When cold and in the non-coated state, the aerodynamic profile is substantially identical to a nominal profile determined by the cartesian coordinates x,y, zadim given in table 1, in which the coordinate zadim is the quotient d/h where d is the distance of the point under consideration from a first reference plane p0 situated at the base of the ...
Optimized aerodynamic profile for a turbine blade, in particular for a rotary wheel of the ...
Safran Aircraft Engines
January 18, 2018 - N°20180016907

When cold and in the non-coated state, the aerodynamic profile is substantially identical to a nominal profile determined by the cartesian coordinates x,y, zadim given in table 1, in which the coordinate zadim is the quotient d/h where d is the distance of the point under consideration from a first reference plane p0 situated at the base of the ...
Optimized aerodynamic profile for a turbine vane, in particular for a nozzle of the second ...
Safran Aircraft Engines
January 18, 2018 - N°20180016906

When cold and in the non-coated state, the aerodynamic profile is substantially identical to a nominal profile determined by the cartesian coordinates x,y, zadim given in table 1, in which the coordinate zadim is the quotient d/h where d is the distance of the point under consideration from a first reference plane p0 situated at the base of the ...
Optimized aerodynamic profile for a turbine vane, in particular for a nozzle of the sixth ...
Safran Aircraft Engines
January 18, 2018 - N°20180016905

When cold and in the non-coated state, the aerodynamic profile is substantially identical to a nominal profile determined by the cartesian coordinates x,y, zadim given in table 1, in which the coordinate zadim is the quotient d/h where d is the distance of the point under consideration from a first reference plane p0 situated at the base of the ...
Optimized aerodynamic profile for a turbine vane, in particular for a nozzle of the first ...
Safran Aircraft Engines
January 18, 2018 - N°20180016904

When cold and in the non-coated state, the aerodynamic profile is substantially identical to a nominal profile determined by the cartesian coordinates x,y, zadim given in table 1, in which the coordinate zadim is the quotient d/h where d is the distance of the point under consideration from a first reference plane p0 situated at the base of the ...
Optimized aerodynamic profile for a turbine blade, in particular for a rotary wheel of the ...
Safran Aircraft Engines
January 18, 2018 - N°20180016903

When cold and in the non-coated state, the aerodynamic profile is substantially identical to a nominal profile determined by the cartesian coordinates x,y, zadim given in table 1, in which the coordinate zadim is the quotient d/h where d is the distance of the point under consideration from a first reference plane p0 situated at the base of the ...
Rf system using pr-ask with orthogonal offset
Clairvoyant Technology Llc
January 11, 2018 - N°20180013469

An rf system using pr-ask with orthogonal offset is disclosed. In some embodiments, the system includes a pr-ask signal generator and an orthogonal offset generator. The pr-ask signal generator can produce a signal representing a sequence of symbols, for example, rfid symbols. The orthogonal offset generator can shift the pr-ask signal trajectory away from the origin while maintaining the time ...
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System and method for a robotic manipulator system
Kurion, Inc.
November 16, 2017 - N°20170326737

Systems and methods are disclosed herein for a robotic manipulator arm deployment and control system. The system comprises at least a vertical mast, a mast deployment system comprising at least two cams, an elbow, an arm wherein the arm is operable to deploy tools, and one or more sensors including a non-contact sensor and a dynamic measurement unit. The cams ...
Bipolar acoustic hyperlens for dual-string thru-casing ultrasonic sensors
October 19, 2017 - N°20170299752

Apparatus, systems, and methods for investigating a subsurface volume of interest from a borehole. Apparatus comprise an enclosure configured for conveyance along the borehole; an acoustic source in the enclosure configured to generate acoustic signals; a lens assembly disposed in the enclosure and next to the acoustic source, the lens assembly being formed of a plurality of lens elements; wherein ...
Gas turbine engine blade outer air seal profile
United Technologies Corporation
July 13, 2017 - N°20170198603

A blade outer air seal for a gas turbine engine includes a gas path surface exposed to exhaust gas flow, a first side extending radially outward from the gas path surface, a second side extending radially outward from the gas path surface, and a plurality of film cooling holes disposed on at least one of the gas path surface. The ...
Gas turbine engine blade outer air seal profile
United Technologies Corporation
July 13, 2017 - N°20170198599

A blade outer air seal for a gas turbine engine includes a gas path surface exposed to exhaust gas flow, a first side extending radially outward from the gas path surface, a second side extending radially outward from the gas path surface, and a plurality of film cooling holes disposed on at least one of the gas path surface. The ...
Gas turbine engine turbine blade airfoil profile
United Technologies Corporation
July 13, 2017 - N°20170198586

A turbine blade for a gas turbine engine according to an example of the present disclosure includes, among other things, an airfoil including leading and trailing edges joined by spaced apart pressure and suction sides to provide an exterior airfoil surface extending from a platform in a radial direction to a tip. The external airfoil surface is formed in substantial ...
Systems and methods for improving resolution in lensless imaging
Rambus Inc.
June 01, 2017 - N°20170153599

An infrared imaging system includes a phase grating overlying a two-dimensional array of thermally sensitive pixels. The phase grating comprises a two-dimensional array of identical subgratings that define a system of cartesian coordinates. The subgrating and pixel arrays are sized and oriented such that the pixels are evenly distributed with respect to the row and column intersections of the subgratings. ...
Lithographic apparatus and exposure method
Asml Netherlands B.v.
April 20, 2017 - N°20170108783

A method including determining a position of a first pattern in each of a plurality of target portions on a substrate, based on a fitted mathematical model, wherein the first pattern includes at least one alignment mark, wherein the mathematical model is fitted to a plurality of alignment mark displacements (dx, dy) for the alignment marks in the target portions, ...
Using cartesian coordinates for position detection with a magnetic sensor
Infineon Technologies Ag
March 30, 2017 - N°20170089726

A magnetic sensor, may sense a first magnetic field component corresponding to a first axis of a magnetic field produced by a magnet. The magnetic sensor may sense a second magnetic field component corresponding to a second axis of the magnetic field. The magnetic sensor may determine information that defines potential positions of a movable object associated with the magnet. ...
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