Patent · US Active

Method for manufacturing micro gas turbine

US9149865B2 · kind B2 · utility

5Cited by
23References
2Claims
0Family size

Assignee

Inventors

Key dates

Filing dateJul 23, 2010
Grant dateOct 6, 2015
Priority date
Expiry dateMay 2, 2031

Classification

  • Technology area (CPC Y)Emerging Cross-Sectional Technologies
  • CPC primaryY10T29/49323
  • WIPO fieldMachine tools
  • WIPO sectorMechanical engineering

Abstract

A method for manufacturing an inexpensive micro gas turbine has an existing compressor-turbine unit divided into two separate parts being a compressor and a turbine. The compressor and turbine shafts are joined. Two existing bearing units are taken, wherein one of them may belong to the existing compressor-turbine unit. The rotor of an existing generator is mounted on the joined shaft. A generator housing is manufactured and connected to the bearing units. The stator of an existing generator is mounted into the generator housing. Energy input into the working cycle of the gas turbine can be implemented by adding either an internal burner or external burner with a heat exchanger. By using inexpensive and often mass produced off-the-shelf components, a cost effective micro gas turbine can be derived.

Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.