US 6,789,907 E100

GPTKB entity

Properties (74)
Predicate Object
gptkbp:instanceOf patent
gptkbp:abstract A method for controlling a gas turbine engine to improve efficiency.
gptkbp:applicationNumber 10/775,123
gptkbp:applicationType Utility
gptkbp:assignee gptkb:General_Electric_Company
gptkbp:citedBy gptkb:US_7,123,456_B2
gptkbp:claims 20
gptkbp:class F01D 25/00
gptkbp:coInventor gptkb:Alice_Johnson
gptkbp:description The invention relates to a method for controlling a gas turbine engine.
gptkbp:examiner Jane_Smith
gptkbp:expirationDate 2024-02-06
gptkbp:fieldOfInvention Gas turbine technology
gptkbp:filingDate 2004-02-06
https://www.w3.org/2000/01/rdf-schema#label US 6,789,907 E100
gptkbp:internationalClassification F02C 7/00
gptkbp:inventor gptkb:John_Doe
gptkbp:issueDate 2004-09-14
gptkbp:legalStatus Granted
gptkbp:maintenanceFee Paid
gptkbp:patentCitation gptkb:US_6,789,911_E100
gptkb:US_6,789,943_E100
gptkb:US_6,789,923_E100
gptkb:US_6,789,927_E100
gptkb:US_6,789,950_E100
gptkb:US_6,789,919_E100
gptkb:US_6,789,928_E100
gptkb:US_6,789,929_E100
gptkb:US_6,789,935_E100
gptkb:US_5,123,456_A
gptkb:US_5,678,901_A
gptkb:US_6,123,456_B1
gptkb:US_6,789,930_E100
gptkb:US_6,789,938_E100
gptkb:US_6,789,939_E100
gptkb:US_6,789,948_E100
gptkb:US_6,789,941_E100
gptkb:US_6,789,944_E100
gptkb:US_6,789,932_E100
gptkb:US_6,789,910_E100
gptkb:US_6,789,916_E100
gptkb:US_6,789,937_E100
gptkb:US_6,789,922_E100
gptkb:US_6,789,921_E100
gptkb:US_6,789,920_E100
gptkb:US_6,789,945_E100
gptkb:US_6,789,933_E100
gptkb:US_6,789,949_E100
gptkb:US_6,789,925_E100
gptkb:US_6,789,947_E100
gptkb:US_6,789,912_E100
gptkb:US_6,789,931_E100
gptkb:US_6,789,908_E100
gptkb:US_6,789,917_E100
gptkb:US_6,789,936_E100
gptkb:US_6,789,918_E100
gptkb:US_6,789,946_E100
US 6,789,909 E100
US_6,789,934_E100
US_6,789,913_E100
US_6,789,914_E100
US_6,789,915_E100
US_6,789,924_E100
US_6,789,926_E100
US_6,789,940_E100
US_6,789,942_E100
gptkbp:patentFamily US_6,789,907_E100_family
gptkbp:patentNumber 6,789,907
gptkbp:priorityDate 2003-02-06
gptkbp:relatedTo gptkb:US_6,789,906_E100
gptkbp:status Active
gptkbp:subclass F01D 25/08
gptkbp:technicalField Aerospace engineering
gptkbp:title Method for controlling a gas turbine engine