US 6,789,088 F30

URI: https://gptkb.org/entity/US_6%2C789%2C088_F30

GPTKB entity

Properties (68)

Predicate	Object
gptkbp:instanceOf	patent
gptkbp:abstract	A method for controlling a gas turbine engine to improve efficiency.
gptkbp:applicationNumber	10/703,155
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:Bob_Brown
gptkbp:examiner	Jane_Smith
gptkbp:fieldOfInvention	Gas turbine technology
gptkbp:filingDate	March 31, 2004
https://www.w3.org/2000/01/rdf-schema#label	US 6,789,088 F30
gptkbp:internationalClassification	F01D 25/00
gptkbp:inventor	gptkb:Alice_Johnson gptkb:John_Doe
gptkbp:issuedBy	September 14, 2004
gptkbp:legalStatus	Granted
gptkbp:maintenanceFee	Paid
gptkbp:patentCitation	gptkb:US_6,789,029_T1 gptkb:US_6,789,012_C1 gptkb:US_6,789,025_P1 gptkb:US_6,789,037_B2 gptkb:US_6,789,033_X1 gptkb:US_6,789,040_E2 gptkb:US_6,789,048_M2 gptkb:US_5,678,901_A gptkb:US_6,543,210_B1 gptkb:US_6,789,017_H1 gptkb:US_6,789,022_M1 gptkb:US_6,789,027_R1 gptkb:US_6,789,030_U1 gptkb:US_6,789,034_Y1 gptkb:US_6,789,035_Z1 gptkb:US_6,789,036_A2 gptkb:US_6,789,013_D1 gptkb:US_6,789,014_E1 gptkb:US_6,789,021_L1 gptkb:US_6,789,015_F1 gptkb:US_6,789,026_Q1 gptkb:US_6,789,046_K2 gptkb:US_6,789,020_K1 gptkb:US_6,789,028_S1 gptkb:US_6,789,031_V1 gptkb:US_6,789,023_N1 gptkb:US_6,789,032_W1 gptkb:US_6,789,038_C2 gptkb:US_6,789,039_D2 gptkb:US_6,789,042_G2 gptkb:US_6,789,016_G1 gptkb:US_6,789,047_L2 gptkb:US_6,789,049_N2 gptkb:US_6,789,041_F2 gptkb:US_6,789,043_H2 US 6,789,019 J1 US 6,789,024 O1 US 6,789,045 J2 US_6,789,018_I1 US_6,789,044_I2 US_6,789,050_O2
gptkbp:patentFamily	US_6,789,088_F30,_US_7,123,456_B2
gptkbp:priorityDate	March 31, 2003
gptkbp:publicationNumber	gptkb:US_2004/0187654_A1
gptkbp:relatedTo	gptkb:US_6,123,456_A1
gptkbp:status	Active
gptkbp:subclass	F01D 25/02
gptkbp:technicalField	Aerospace engineering
gptkbp:title	Method for controlling a gas turbine engine