Invention Application
- Patent Title: MULTI-ENGINE ARCHITECTURE WITH LINKAGES TO MULTIPLE SPOOLS
-
Application No.: US16431271Application Date: 2019-06-04
-
Publication No.: US20200032702A1Publication Date: 2020-01-30
- Inventor: Daniel Bernard Kupratis , Neil Terwilliger , Christopher J. Hanlon
- Applicant: United Technologies Corporation
- Main IPC: F02C3/06
- IPC: F02C3/06 ; F02C6/06 ; F02C7/32 ; F02C7/36
Abstract:
An aircraft gas turbine engine system comprises first and second gas turbine engines. The first gas turbine engine has first and second spools. A first power linkage connects the second gas turbine engine to the first spool of the gas turbine engine, and a second power linkage connects the second gas turbine engine to the second spool of the first gas turbine engine.
Public/Granted literature
- US11415044B2 Multi-engine architecture with linkages to multiple spools Public/Granted day:2022-08-16
Information query
IPC分类:
