Inventor
Friedrich O. Soechting
Inventor
Tequesta, FL, US
Overview
Patents· 27 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 turbines36%
F05DIndexing scheme for aspects relating to non-positive-displacement machines or engines, gas-turbines or jet-propulsion plants28%
F02CGas-turbine plants10%
Y10TTechnical subjects covered by former us classification7%
Y02TClimate change mitigation technologies related to transportation6%
B23PMetal-working not otherwise provided for4%
G01BMeasuring length, thickness or similar linear dimensions3%
G01MTesting static or dynamic balance of machines or structures3%
B22CFoundry moulding1%
F23RGenerating combustion products of high pressure or high velocity, e.g. gas-turbine combustion chambers1%
PatentTitleYear
7,552,647'Turbine blade fatigue life evaluating method'20097,033,138'Ring segment of gas turbine'20066,994,514'Turbine blade and gas turbine'20066,988,872'Turbine moving blade and gas turbine'20066,983,659'Turbine blade creep life evaluating method, turbine blade creep elongation strain measuring apparatus, and turbine blade'20066,887,039'Stationary blade in gas turbine and gas turbine comprising the same'20056,860,108'Gas turbine tail tube seal and gas turbine using the same'20056,761,529'Cooling structure of stationary blade, and gas turbine'20046,758,651'Gas turbine'20046,742,991'Turbine blade and gas turbine'20046,722,138'Vane platform trailing edge cooling'20046,514,042'Method and apparatus for cooling a wall within a gas turbine engine'20036,419,446'Apparatus and method for inhibiting radial transfer of core gas flow within a core gas flow path of a gas turbine engine'20026,402,470'Method and apparatus for cooling a wall within a gas turbine engine'20026,280,140'Method and apparatus for cooling an airfoil'20016,247,896'Method and apparatus for cooling an airfoil'20016,210,112'Apparatus for cooling an airfoil for a gas turbine engine'20016,164,912'Hollow airfoil for a gas turbine engine'20006,050,777'Apparatus and method for cooling an airfoil for a gas turbine engine'20006,004,100'Trailing edge cooling apparatus for a gas turbine airfoil'19995,931,638'Turbomachinery airfoil with optimized heat transfer'19995,720,431'Cooled blades for a gas turbine engine'19985,645,397'Turbine vane assembly with multiple passage cooled vanes'19975,599,166'Core for fabrication of gas turbine engine airfoils'19975,419,039'Method of making an air cooled vane with film cooling pocket construction'19955,405,242'Cooled vane'19955,392,515'Method of manufacturing an air cooled vane with film cooling pocket construction'1995Career & activity timeline
Assembled from patent assignee/location history and declaration credentials.
1995–2004Patents assigned to UNITED TECHNOLOGIES CORP (17)· patent assignee history
1995–2004Based in Tequesta, FL, US· patent location history
2004–2009Patents assigned to MITSUBISHI HEAVY IND LTD (9)· patent assignee history
2004Patents assigned to MITSHUBISHI HEAVY IND LTD (1)· patent assignee history
2004–2009Based in Miami, FL, US· patent location history
Inventor activity
Assignee and location history derived from the patent record.
Assignees
| Assignee | Patents | Span |
|---|---|---|
| UNITED TECHNOLOGIES CORP | 17 | 1995–2004 |
| MITSUBISHI HEAVY IND LTD | 9 | 2004–2009 |
| MITSHUBISHI HEAVY IND LTD | 1 | 2004 |
Locations
| Location | Patents | Span |
|---|---|---|
| Tequesta, Florida, US | 17 | 1995–2004 |
| Miami, Florida, US | 10 | 2004–2009 |