Inventor
Masamitsu Kuwabara
Inventor
Hyogo, JP
Overview
Patents· 22 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 turbines42%
F05DIndexing scheme for aspects relating to non-positive-displacement machines or engines, gas-turbines or jet-propulsion plants32%
F02CGas-turbine plants14%
B23KSoldering or unsoldering6%
F23RGenerating combustion products of high pressure or high velocity, e.g. gas-turbine combustion chambers2%
G01NInvestigating or analysing materials by determining their chemical or physical properties2%
Y10STechnical subjects covered by former uspc cross-reference art collections [xracs] and digests2%
PatentTitleYear
10,704,394Flow passage forming plate, flow passage forming member assembly and vane including the same, gas turbine, manufacturing method of flow passage forming plate, and modification method of flow passage forming plate202010,358,927Vane, gas turbine provided with the same, method of manufacturing vane, and method of remodeling vane20199,989,450Erosion test apparatus, accelerator and erosion test method20189,644,485'Gas turbine blade with cooling passages'20179,540,934'Hot part of gas turbine, gas turbine including the same, and manufacturing method of hot part of gas turbine'20179,181,807'Blade member and rotary machine'20158,596,976'Turbine blade'20138,231,348'Platform cooling structure for gas turbine moving blade'20127,168,914'Gas turbine stationary blade'20076,966,750'Gas turbine stationary blade'20056,893,215'Division wall and shroud of gas turbine'20056,887,039'Stationary blade in gas turbine and gas turbine comprising the same'20056,783,323'Gas turbine stationary blade'20046,761,529'Cooling structure of stationary blade, and gas turbine'20046,751,962'Tail tube seal structure of combustor and a gas turbine using the same structure'20046,742,991'Turbine blade and gas turbine'20046,692,227'Stationary blade shroud of a gas turbine'20046,616,405'Cooling structure for a gas turbine'20036,602,048'Gas turbine split ring'20036,572,335'Gas turbine cooled stationary blade'20036,318,960'Gas turbine stationary blade'20016,270,311'Gas turbine split ring'2001Career & activity timeline
Assembled from patent assignee/location history and declaration credentials.
2001–2013Patents assigned to MITSUBISHI HEAVY IND LTD (15)· patent assignee history
2001–2013Based in Hyogo, JP· patent location history
2001–2005Based in Takasago, JP· patent location history
2012–2015Patents assigned to KUWABARA MASAMITSU (3)· patent assignee history
2013Patents assigned to HADA SATOSHI (1)· patent assignee history
2013Patents assigned to HASHIMOTO TOMOKO (1)· patent assignee history
2015–2020Patents assigned to MITSUBISHI HITACHI POWER SYS (6)· patent assignee history
2015Based in Tokyo, JP· patent location history
2017–2020Based in Yokohama, JP· patent location history
Inventor activity
Assignee and location history derived from the patent record.
Assignees
| Assignee | Patents | Span |
|---|---|---|
| MITSUBISHI HEAVY IND LTD | 15 | 2001–2013 |
| MITSUBISHI HITACHI POWER SYS | 6 | 2015–2020 |
| KUWABARA MASAMITSUself | 3 | 2012–2015 |
| HADA SATOSHI | 1 | 2013 |
| HASHIMOTO TOMOKO | 1 | 2013 |
Locations
| Location | Patents | Span |
|---|---|---|
| Hyogo, JP | 11 | 2001–2013 |
| Yokohama, JP | 5 | 2017–2020 |
| Takasago, JP | 5 | 2001–2005 |
| Tokyo, JP | 1 | 2015 |