Invention Application
- Patent Title: HIGH THRUST GEARED GAS TURBINE ENGINE
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Application No.: PCT/US2014/046781Application Date: 2014-07-16
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Publication No.: WO2015050619A3Publication Date: 2015-04-09
- Inventor: SCHWARZ, Frederick M. , HASEL, Karl L. , MERRY, Brian D.
- Applicant: UNITED TECHNOLOGIES CORPORATION
- Applicant Address: One Financial Plaza Hartford, Connecticut 06101 US
- Assignee: UNITED TECHNOLOGIES CORPORATION
- Current Assignee: UNITED TECHNOLOGIES CORPORATION
- Current Assignee Address: One Financial Plaza Hartford, Connecticut 06101 US
- Agency: OLDS, Theodore W.
- Priority: US61/867,659 20130820
- Main IPC: F02C7/00
- IPC: F02C7/00 ; F02C7/32
Abstract:
A ratio of an outer diameter of a fan hub at a leading edge of the blades to an outer tip diameter of the blades at the leading edge is greater than or equal to about 0.24 and less than or equal to about 0.38. The fan tip diameter is greater than or equal to about 84 inches (213.36 centimeters) and a fan tip speed is less than or equal to about 1050 ft / second (320.04 meters / second). A bypass ratio, a gear ratio and an AN2 value are also claimed. The fan drive turbine has between three and six stages.
Information query
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