US 6,789,041 F26

GPTKB entity

Properties (63)
Predicate Object
gptkbp:instanceOf patent
gptkbp:abstract A method for controlling a gas turbine engine to improve efficiency.
gptkbp:applicationNumber 10/123,456
gptkbp:applicationPublicationNumber gptkb:US_2003/0123456_A1
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:country gptkb:United_States
gptkbp:examiner Jane_Smith
gptkbp:fieldOfInvention Gas turbine technology
gptkbp:filingDate April 15, 2003
https://www.w3.org/2000/01/rdf-schema#label US 6,789,041 F26
gptkbp:internationalClassification F01D 21/00
gptkbp:inventiveStep Non-obvious
gptkbp:inventor gptkb:John_Doe
gptkbp:issuedBy February 3, 2004
gptkbp:language English
gptkbp:legalStatus Granted
gptkbp:maintenanceFee Paid
gptkbp:novelty Novel
gptkbp:patentCitation gptkb:US_6,789,052_F26
gptkb:US_6,789,063_F26
gptkb:US_6,789,048_F26
gptkb:US_6,789,061_F26
gptkb:US_6,789,067_F26
gptkb:US_6,789,054_F26
gptkb:US_6,789,060_F26
gptkb:US_5,678,901_A
gptkb:US_6,543,210_B1
gptkb:US_6,789,000_B2
gptkb:US_6,789,070_F26
gptkb:US_6,789,059_F26
gptkb:US_6,789,055_F26
gptkb:US_6,789,069_F26
gptkb:US_6,789,057_F26
gptkb:US_6,789,065_F26
gptkb:US_6,789,045_F26
gptkb:US_6,789,056_F26
gptkb:US_6,789,046_F26
gptkb:US_6,789,062_F26
gptkb:US_6,789,050_F26
gptkb:US_6,789,051_F26
gptkb:US_6,789,047_F26
gptkb:US_6,789,053_F26
gptkb:US_6,789,043_F26
gptkb:US_6,789,068_F26
gptkb:US_6,789,066_F26
gptkb:US_6,789,049_F26
gptkb:US_6,789,044_F26
US_6,789,042_F26
US_6,789,064_F26
US_6,789,058_F26
gptkbp:patentFamily US_6,789,041_F26_family
gptkbp:patentOffice gptkb:USPTO
gptkbp:patentType Granted patent
gptkbp:priorityDate March 15, 2002
gptkbp:publicationDate February 3, 2004
gptkbp:relatedTo gptkb:US_6,789,040_F26
gptkbp:status Active
gptkbp:technologyArea Aerospace engineering
gptkbp:title Method for controlling a gas turbine engine