Inventor
Abdul-Azeez Mohammed-Fakir
Inventor
Schenectady, NY, US
Overview
Patents· 25 as inventor
Public. Assignee & technology derived from the patent record. Each patent links to its LexDana page.
F01Dprimary
F01DNon-positive displacement machines or engines, e.g. steam turbines31%
F16JPistons30%
F02CGas-turbine plants19%
F23RGenerating combustion products of high pressure or high velocity, e.g. gas-turbine combustion chambers7%
F05DIndexing scheme for aspects relating to non-positive-displacement machines or engines, gas-turbines or jet-propulsion plants3%
F04DNon-positive-displacement pumps1%
F05BIndexing scheme relating to wind, spring, weight, inertia or like motors, to machines or engines for liquids covered by subclasses f03b, f03d and f03g1%
F16DCouplings for transmitting rotation1%
F23JRemoval or treatment of combustion products or combustion residues1%
Y10STechnical subjects covered by former uspc cross-reference art collections [xracs] and digests1%
PatentTitleYear
6,840,048'Dynamically uncoupled can combustor'20056,764,081'Supplemental seal for the chordal hinge seals in a gas turbine and methods of installation'20046,752,592'Supplemental seal for the chordal hinge seals in a gas turbine'20046,742,988'Composite tubular woven seal for steam turbine diaphragm horizontal joint interfaces'20046,719,295'Supplemental seal for the chordal hinge seals in a gas turbine'20046,659,472'Seal for gas turbine nozzle and shroud interface'20036,655,913'Composite tubular woven seal for an inner compressor discharge case'20036,652,231'Cloth seal for an inner compressor discharge case and methods of locating the seal in situ'20036,648,333'Method of forming and installing a seal'20036,641,144'Supplemental seal for the chordal hinge seals in a gas turbine'20036,637,752'Supplemental seal for the chordal hinge seal in a gas turbine'20036,637,753'Supplemental seal for the chordal hinge seals in a gas turbine'20036,637,751'Supplemental seal for the chordal hinge seals in a gas turbine'20036,609,886'Composite tubular woven seal for gas turbine nozzle and shroud interface'20036,609,885'Supplemental seal for the chordal hinge seal in a gas turbine'20036,599,089'Supplemental seal for the chordal hinge seal in a gas turbine'20036,595,745'Supplemental seal for the chordal hinge seals in a gas turbine'20036,572,331'Supplemental seal for the chordal hinge seals in a gas turbine'20036,568,903'Supplemental seal for the chordal hinge seals in a gas turbine'20036,547,256'Cloth ring seal'20036,537,023'Supplemental seal for the chordal hinge seal in a gas turbine'20036,502,825'Pressure activated cloth seal'20036,394,255'Rotary motion limiting arrangement'20026,250,062'Fuel nozzle centering device and method for gas turbine combustors'20016,216,442'Supports for connecting a flow sleeve and a liner in a gas turbine combustor'2001Career & activity timeline
Assembled from patent assignee/location history and declaration credentials.
2001–2005Patents assigned to GEN ELECTRIC (25)· patent assignee history
2001–2004Based in Schenectady, NY, US· patent location history
2004–2005Based in Guilderland, NY, US· patent location history
Inventor activity
Assignee and location history derived from the patent record.
Assignees
| Assignee | Patents | Span |
|---|---|---|
| GEN ELECTRIC | 25 | 2001–2005 |
Locations
| Location | Patents | Span |
|---|---|---|
| Schenectady, New York, US | 23 | 2001–2004 |
| Guilderland, New York, US | 2 | 2004–2005 |