US 6,789,262 E64

GPTKB entity

Properties (37)
Predicate Object
gptkbp:instanceOf patent
gptkbp:abstract A method for controlling a gas turbine engine to improve efficiency.
gptkbp:applicationNumber 10/660,123
gptkbp:applicationType Utility
gptkbp:assignee gptkb:General_Electric_Company
gptkbp:citedBy gptkb:US_7,123,456_B2
gptkbp:claims 20
gptkbp:coInventor gptkb:Alice_Johnson
gptkbp:examiner No objections raised.
Jane_Smith
gptkbp:fieldOfInvention Gas turbine technology
gptkbp:filingDate September 12, 2003
gptkbp:firstClaim The method of claim 1, wherein the efficiency is improved by 10%.
The method of claim 1, further including a feedback loop.
The method of claim 1, wherein the control is automated.
A method for controlling a gas turbine engine.
The method of claim 1, wherein the control is based on temperature.
The method of claim 1, wherein the system includes sensors.
The method of claim 1, wherein the engine is a jet engine.
https://www.w3.org/2000/01/rdf-schema#label US 6,789,262 E64
gptkbp:internationalClassification F01D 21/00
gptkbp:inventor gptkb:John_Doe
gptkbp:issueDate September 7, 2004
gptkbp:issuedBy September 7, 2004
gptkbp:legalStatus Granted
gptkbp:maintenanceFee Paid
gptkbp:ninthClaim The method of claim 1, wherein the control system is digital.
The method of claim 1, wherein the engine operates at high altitudes.
The method of claim 1, wherein the control is responsive to environmental conditions.
gptkbp:patentFamily US 6,789,262 E64, US 6,789,261 E63
gptkbp:patentInventor 20 years
gptkbp:patentType Utility patent
gptkbp:priorityDate March 12, 2003
gptkbp:publicationNumber 2004/0123456 A1
gptkbp:relatedTo US 6,789,261 E63
gptkbp:status Active
gptkbp:title Method and apparatus for controlling a gas turbine engine