Manfred Feldmann
42Patents
4h-index
59Co-inventors
66Inventor score
Filing activity: May 6, 1993 → Jul 3, 2023
Most-cited inventions
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| US5338152A | Arrangement for sealing structural members using a V-shaped insert, particularly in the case of turbo-engines | Mechanical Engineering; Lighting; Heating | 10 | Expired |
| US7704042B2 | Turbomachine, especially a gas turbine | Mechanical Engineering; Lighting; Heating | 10 | Active |
| US10001083B2 | Turbofan aircraft engine | Mechanical Engineering; Lighting; Heating | 6 | Active |
| US9664059B2 | Sealing device and turbomachine | Mechanical Engineering; Lighting; Heating | 4 | Active |
| US9982559B2 | Blade or vane for a turbomachine and axial turbomachine | Emerging Cross-Sectional Technologies | 4 | Active |
| US9512734B2 | Sealing of the flow channel of a turbomachine | Emerging Cross-Sectional Technologies | 3 | Active |
| US10689983B2 | Pulse body module with bearing protection | Mechanical Engineering; Lighting; Heating | 3 | Active |
| US9488069B2 | Cooling-air guidance in a housing structure of a turbomachine | Emerging Cross-Sectional Technologies | 2 | Active |
| US9945241B2 | Sealing element of an axial turbomachine | Mechanical Engineering; Lighting; Heating | 2 | Active |
| US9784131B2 | Sealing arrangement for a turbomachine, a guide vane arrangement, and a turbomachine with such a sealing arrangement | Emerging Cross-Sectional Technologies | 2 | Active |
| US10047618B2 | Component system of a turbo engine | Emerging Cross-Sectional Technologies | 2 | Active |
| US9664057B2 | Stator vane segment of a fluid flow machine and turbine | Mechanical Engineering; Lighting; Heating | 2 | Active |
| US9605551B2 | Axial seal in a casing structure for a fluid flow machine | Mechanical Engineering; Lighting; Heating | 2 | Active |
| US9816379B2 | Balancing body for a continuous blade arrangement | Emerging Cross-Sectional Technologies | 2 | Active |
| US9382809B2 | Seal assembly, method and turbomachine | Emerging Cross-Sectional Technologies | 2 | Active |
| US9194331B2 | Flow conducting assembly for cooling the low-pressure turbine housing of a gas turbine jet engine | Emerging Cross-Sectional Technologies | 2 | Active |
| US9664065B2 | Clamping ring for a turbomachine | Mechanical Engineering; Lighting; Heating | 1 | Active |
| US10731492B2 | Component joint | Mechanical Engineering; Lighting; Heating | 1 | Active |
| US11434785B2 | Jacket ring assembly for a turbomachine | Mechanical Engineering; Lighting; Heating | 1 | Active |
| US10240474B2 | Turbomachine having a seal device | Emerging Cross-Sectional Technologies | 1 | Active |
| US10392972B2 | Liner element for a turbine intermediate case | Mechanical Engineering; Lighting; Heating | 1 | Active |
| US11208908B2 | Static seal arrangement and turbomachine | Mechanical Engineering; Lighting; Heating | 1 | Active |
| US11125097B2 | Segmented ring for installation in a turbomachine | Mechanical Engineering; Lighting; Heating | 1 | Active |
| US9416672B2 | Housing structure with improved seal and cooling | Mechanical Engineering; Lighting; Heating | 1 | Active |
| US9963993B2 | Turbine ring and turbomachine | Mechanical Engineering; Lighting; Heating | 1 | Active |
Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.