Inventor
Werner Humhauser
Inventor
Moosburg, DE
Overview
Patents· 28 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%
F05DIndexing scheme for aspects relating to non-positive-displacement machines or engines, gas-turbines or jet-propulsion plants26%
F04DNon-positive-displacement pumps14%
Y02TClimate change mitigation technologies related to transportation14%
Y10TTechnical subjects covered by former us classification8%
F02CGas-turbine plants3%
B23KSoldering or unsoldering1%
B33YAdditive manufacturing, i.e. manufacturing of three-dimensional [3d] objects by additive deposition, additive agglomeration or additive layering, e.g. by 3d printing, stereolithography or selective laser sintering1%
F02KJet-propulsion plants1%
F05BIndexing scheme relating to wind, spring, weight, inertia or like motors, to machines or engines for liquids covered by subclasses f03b, f03d and f03g1%
PatentTitleYear
11,125,115Connecting device for a variable vane of a gas turbine202110,982,558Guide vane connection202110,876,425Lever connection of a guide vane adjustment for turbomachinery202010,830,084Housing for a gas turbine compressor202010,711,626Guide vane ring and turbomachine202010,502,084Module for a gas turbine201910,494,944Seal on the inner ring of a guide vane201910,494,942Inner ring system for an inlet guide vane cascade of a turbomachine201910,436,054Blade outer air seal for a gas turbine engine201910,364,827Guide vane ring, guide vane, inner ring and turbomachine201910,352,178Locking element and turbomachine201910,294,963Axially split inner ring for a fluid flow machine, guide vane ring, and aircraft engine201910,280,934Gas turbine compressor stage201910,174,628Axially divided inner ring for a turbomachine and guide vane ring201910,041,363Blade-disk assembly, method and turbomachine201810,001,083Turbofan aircraft engine20189,617,866'Blade outer air seal for a gas turbine engine'20179,605,549'Stationary blade ring, assembly method and turbomachine'20179,297,391'Flow device comprising a cavity cooling system'20168,764,390'Assembly mechanism comprising a tension anchor and corresponding method for a rotor system of an axial turbo engine'20148,356,741'Method for producing a blade plating on a blade for a turbomachine'20138,105,016'Damping arrangement for guide vanes'20128,061,965'Ring structure of metal construction having a run-in lining'20117,396,206'Arrangement for axially and radially fixing the guide vanes of a vane ring of a gas turbine'20086,537,020'Casing structure of metal construction'20036,431,830'Nozzle ring for a gas turbine'20026,119,339'Nozzle ring for a gas turbine and method of manufacture thereof'20005,601,407'Stator for turbomachines'1997Career & activity timeline
Assembled from patent assignee/location history and declaration credentials.
1997–2002Patents assigned to MTU MUENCHEN GMBH (3)· patent assignee history
1997–2021Based in Moosburg, DE· patent location history
2003–2016Patents assigned to MTU AERO ENGINES GMBH (7)· patent assignee history
2011–2017Patents assigned to HUMHAUSER WERNER (6)· patent assignee history
2017–2021Patents assigned to MTU Aero Engines AG (18)· patent assignee history
2017–2019Patents assigned to UNITED TECHNOLOGIES CORP (2)· patent assignee history
2018Based in Mossburg, DE· patent location history
Inventor activity
Assignee and location history derived from the patent record.
Assignees
| Assignee | Patents | Span |
|---|---|---|
| MTU Aero Engines AG | 18 | 2017–2021 |
| MTU AERO ENGINES GMBH | 7 | 2003–2016 |
| HUMHAUSER WERNERself | 6 | 2011–2017 |
| MTU MUENCHEN GMBH | 3 | 1997–2002 |
| UNITED TECHNOLOGIES CORP | 2 | 2017–2019 |
Locations
| Location | Patents | Span |
|---|---|---|
| Moosburg, DE | 27 | 1997–2021 |
| Mossburg, DE | 1 | 2018 |