20250215823. Gas Turbine Engine (General Electric)
GAS TURBINE ENGINE
Abstract: a gas turbine engine is provided. the gas turbine engine includes: a turbomachine having a compressor section, a combustion section, and a turbine section arranged in serial flow order, the compressor section having a high pressure compressor defining a high pressure compressor exit area (a) in square inches; wherein the gas turbine engine defines a redline exhaust gas temperature (egt) in degrees celsius, a total sea level static thrust output (fn) in pounds, and a corrected specific thrust, wherein the corrected specific thrust is greater than or equal to 42 and less than or equal to 90, the corrected specific determined as follows: fn�egt/(a�1000).
Inventor(s): Daniel Alan Niergarth, Jeffrey Donald Clements, Jeffrey S. Spruill, Erich Alois Krammer, Matthew Kenneth MacDonald, Scott Alan Schimmels, Paul Hadley Vitt
CPC Classification: F02C3/06 (GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS (construction of turbines ; jet-propulsion plants ; construction of compressors or fans ; generating combustion products of high pressure or high velocity ; using gas turbines in compression refrigeration plants ))
Search for rejections for patent application number 20250215823
- Patent Applications
- General Electric Company
- CPC F02C3/06
- Daniel Alan Niergarth of Norwood OH US
- Jeffrey Donald Clements of Mason OH US
- Jeffrey S. Spruill of Hillsboro OH US
- Erich Alois Krammer of West Chester OH US
- Matthew Kenneth MacDonald of Austin TX US
- Scott Alan Schimmels of Miamisburg OH US
- Paul Hadley Vitt of Liberty Township OH US