Original Assignee United Technologies Corp Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.) Suciu Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.) Active Application number US15/292,472 Other versions US20170044992A1 Google Patents Turbine section of high bypass turbofanĭownload PDF Info Publication number US10060357B2 US10060357B2 US15/292,472 US201615292472A US10060357B2 US 10060357 B2 US10060357 B2 US 10060357B2 US 201615292472 A US201615292472 A US 201615292472A US 10060357 B2 US10060357 B2 US 10060357B2 Authority US United States Prior art keywords turbine fan engine compressor recited Prior art date Legal status (The legal status is an assumption and is not a legal conclusion. Google Patents US10060357B2 - Turbine section of high bypass turbofan US10060357B2 - Turbine section of high bypass turbofan

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