Inventor · Munich, DE

Alexander Boeck

38Patents
8h-index
22Co-inventors
75Inventor score

Filing activity: Mar 19, 1975 → Jun 8, 2021

Most-cited inventions

PatentTitleAreaCited byStatus
US3975280A Storage-stable, readily-soluble detergent additives, coating compositions and process Emerging Cross-Sectional Technologies 77 Expired
US5111855A Plant and apparatus for producing perfumes Performing Operations; Transporting 27 Expired
US6625989B2 Method and apparatus for the cooling of jet-engine turbine casings Emerging Cross-Sectional Technologies 21 Expired
US6568688B1 Hydraulic seal arrangement, more particularly on a gas turbine Emerging Cross-Sectional Technologies 18 Expired
US7258525B2 Guide blade fixture in a flow channel of an aircraft gas turbine Emerging Cross-Sectional Technologies 14 Expired
US6817189B2 Arrangement for the cooling of the casing of an aircraft gas turbine engine Emerging Cross-Sectional Technologies 14 Expired
US4526694A Acid-containing product for the treatment of moist wash in the mechanical clothes drier Emerging Cross-Sectional Technologies 11 Expired
US7516962B2 Spoke-centered brush seal arrangement for use in a gas turbine Mechanical Engineering; Lighting; Heating 10 Expired
US7220097B2 Gas turbine apparatus with actuators to counteract deformations of housing Emerging Cross-Sectional Technologies 8 Expired
US10550707B2 Turbomachine seal system Mechanical Engineering; Lighting; Heating 6 Active
US6173566A Casing construction on a gas turbine jet engine Emerging Cross-Sectional Technologies 5 Expired
US10060278B2 Guide vane for a turbomachine having a sealing device; stator, as well as turbomachine Mechanical Engineering; Lighting; Heating 4 Active
US9920645B2 Sealing system for a turbomachine Emerging Cross-Sectional Technologies 4 Active
US10151209B2 Sealing system made of ceramic fiber composite materials Emerging Cross-Sectional Technologies 3 Active
US9540946B2 Safety device for a bearing arrangement of a rotor of a turbomachine Mechanical Engineering; Lighting; Heating 3 Active
US6416246B1 Connecting arrangement for two rotor disks of an axial-flow turbomachine Emerging Cross-Sectional Technologies 3 Expired
US9739156B2 Gas turbinen rotor blade Emerging Cross-Sectional Technologies 3 Active
US11156127B2 Positioning element with recesses for a guide vane arrangement Mechanical Engineering; Lighting; Heating 2 Active
US9932847B2 Guide blade for a gas turbine Mechanical Engineering; Lighting; Heating 2 Active
US8128374B2 Securing element for fastening rotor blades Emerging Cross-Sectional Technologies 2 Active
US9797264B2 Rotating blade having a rib arrangement with a coating Mechanical Engineering; Lighting; Heating 2 Active
US6884024B2 Arrangement for the fastening of struts serving as bearing carriers for the rotor of an aeronautical gas turbine to the casing structure of the aeronautical gas turbine Mechanical Engineering; Lighting; Heating 2 Expired
US9982547B2 Guide mechanism for a gas turbine and gas turbine having such a guide mechanism Emerging Cross-Sectional Technologies 2 Active
US10738656B2 Sealing assembly for a gas turbine Emerging Cross-Sectional Technologies 2 Active
US6722119B2 Turbojet power plant with heat exchanger Emerging Cross-Sectional Technologies 1 Expired

Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.