Robert Alexander Goehlich
31Patents
5h-index
32Co-inventors
65Inventor score
Filing activity: Nov 18, 2008 → Nov 16, 2018
Most-cited inventions
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| US10144126B2 | Robot system and method of operating a robot system | Physics | 116 | Active |
| US10214275B2 | Method of installing a fixture | Mechanical Engineering; Lighting; Heating | 108 | Active |
| US8100316B2 | Method for joining aircraft fuselage elements by friction stir welding (fsw) | Performing Operations; Transporting | 11 | Active |
| US9090328B2 | Fuselage segment and method for manufacturing a fuselage segment | Emerging Cross-Sectional Technologies | 9 | Active |
| US8356772B2 | Lightweight structure | Emerging Cross-Sectional Technologies | 6 | Active |
| US9868549B2 | Method for the assembly of an aircraft fuselage and fuselage manufacturing station | Emerging Cross-Sectional Technologies | 5 | Active |
| US8740144B2 | Passenger supply arrangement for an aeroplane | Emerging Cross-Sectional Technologies | 4 | Active |
| US10232926B2 | Integrated lamination process for manufacturing a shell element | Emerging Cross-Sectional Technologies | 3 | Active |
| US9333703B2 | Method and device for bonding parts to be joined, as well as component | Emerging Cross-Sectional Technologies | 3 | Active |
| US9138958B2 | Lightweight structure, particularly primary aircraft structure or subassembly, as well as method for the manufacture thereof | Emerging Cross-Sectional Technologies | 3 | Active |
| US9775411B2 | System for mounting of components | Emerging Cross-Sectional Technologies | 3 | Active |
| US8087621B2 | Holder for fixing components, in particular lines, inside an aircraft without using holes | Electricity | 2 | Active |
| US9517829B2 | Aircraft fuselage structure | Mechanical Engineering; Lighting; Heating | 2 | Active |
| US8844870B2 | Fuselage segment, and method for the production of a fuselage segment | Emerging Cross-Sectional Technologies | 2 | Active |
| US8925864B2 | Component, in particular a shell component, which can be joined thermally and/or mechanically, for building a fuselage section of an aircraft | Emerging Cross-Sectional Technologies | 2 | Active |
| US8741090B2 | Method and device for joining adherends, as well as component | Emerging Cross-Sectional Technologies | 2 | Active |
| US10596627B2 | Method of installing a fixture and associated apparatus | Emerging Cross-Sectional Technologies | 2 | Active |
| US8765042B2 | Fuselage section of an aircraft and method for the production of the fuselage section | Emerging Cross-Sectional Technologies | 1 | Active |
| US9169016B2 | Method and device for the installation of systems, and a freight loading system | Emerging Cross-Sectional Technologies | 1 | Active |
| US9463865B2 | Fuselage cell for an aircraft, particularly an airplane | Electricity | 1 | Active |
| US9487285B2 | Aircraft fuselage structure | Performing Operations; Transporting | 1 | Active |
| US9561617B2 | Devices for bonding parts to be joined | Emerging Cross-Sectional Technologies | 1 | Active |
| US9375781B2 | Riveting device and riveting method | Emerging Cross-Sectional Technologies | 1 | Active |
| US10857665B2 | Mobile manufacturing module | Performing Operations; Transporting | 0 | Active |
| US9452561B2 | Method of producing a composite shell element, composite shell element, means of transport and use | Emerging Cross-Sectional Technologies | 0 | Active |
Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.