Combined Energy Storage Turbine and Simple Cycle Peaker System

    公开(公告)号:US20230063511A1

    公开(公告)日:2023-03-02

    申请号:US18053792

    申请日:2022-11-09

    发明人: Robert J. Kraft

    摘要: A system comprises a gas turbine engine. The gas turbine engine has a flow diffuser system, a combustor, a modified compressor section, and a turbine coupled to a shaft. The system includes a low pressure intercooled compressor, a high pressure intercooled compressor, a recuperator, and a compressed air storage tank. The compressed air storage tank is in selective fluid communication with the low pressure intercooled compressor via the high pressure intercooled compressor, and the recuperator. The high pressure intercooled compressor is configured to selectively receive compressed air from the low pressure intercooled compressor and is further configured to selectively compress the compressed air to a highly compressed air for storage in the compressed air storage tank. Each of the compressed air storage tank and the low pressure intercooled compressor is selectively and fluidly coupled to the gas turbine engine.

    Combined energy storage turbine and simple cycle peaker system

    公开(公告)号:US11549435B1

    公开(公告)日:2023-01-10

    申请号:US17117110

    申请日:2020-12-10

    发明人: Robert J. Kraft

    摘要: In an embodiment, a gas turbine system is provided. The gas turbine system may include a supplementary air system and a flow diffuser configured to receive compressed air from the supplementary air system. The gas turbine system further comprises a gas turbine compressor downstream the flow diffuser, a combustor downstream the gas turbine compressor, a turbine downstream the combustor, and a turbine haft. The turbine shaft comprises a thrust bearing and a clutch. When the gas turbine system is operating, the gas turbine compressor does not consume electricity.