Invention Grant
- Patent Title: Gas turbine engine architecture with intercooled twin centrifugal compressor
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Application No.: US14209326Application Date: 2014-03-13
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Publication No.: US09752585B2Publication Date: 2017-09-05
- Inventor: Daniel B. Kupratis
- Applicant: United Technologies Corporation
- Applicant Address: US CT Farmington
- Assignee: United Technologies Corporation
- Current Assignee: United Technologies Corporation
- Current Assignee Address: US CT Farmington
- Agency: O'Shea Getz P.C.
- Main IPC: F04D17/12
- IPC: F04D17/12 ; F02C3/08 ; F02C7/143 ; F04D29/58 ; F01D9/02 ; F02K3/075 ; F02C3/107
Abstract:
A gas turbine engine includes an intercooled twin centrifugal compressor. A pipe diffuser extends from the intercooled twin centrifugal compressor into an airflow path.
Public/Granted literature
- US20140271121A1 GAS TURBINE ENGINE ARCHITECTURE WITH INTERCOOLED TWIN CENTRIFUGAL COMPRESSOR Public/Granted day:2014-09-18
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