# US 10,480,408 B2 · Energy weapon system having a gas turbine generator with idle assist > Agents: this data is available as JSON from the patentgrep API and MCP server — see https://patentgrep.com/llms.txt - Number: US 10,480,408 B2 - Document ID: US10480408B2 - Status: Granted - Kind: B2 - Application number: 15/250,436 - Filed: 2016-08-29 - Published: 2018-09-06 - Granted: 2019-11-19 - Earliest claimed: 2016-08-29 - Assignees: Rolls-Royce North American Technologies Inc. - Applicants: Rolls-Royce North American Technologies, Inc. - Inventors: Erik A. Munevar - Web page: https://patentgrep.com/patent/US10480408B2 ## CPC - F02C 6/14: Gas-turbine plants having means for storing energy, e.g. for meeting peak loads - F01D 15/10: Adaptations for driving, or combinations with, electric generators - F02C 3/10: with another turbine driving an output shaft but not driving the compressor - F02C 7/32: Arrangement, mounting, or driving, of auxiliaries - F02C 9/28: Regulating systems responsive to plant or ambient parameters, e.g. temperature, pressure, rotor speed (F02C9/30 - F02C9/38, F02C9/44 take precedence) - F02C 9/50: with control of working fluid flow - F41H 13/005: {the high-energy beam being a laser beam} - F05D 2220/76: an electrical generator - F05D 2260/4031: as in toothed gearing - F05D 2270/303: Temperature - F05D 2270/331: Mechanical loads - F02C: GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS (construction of turbines F01D; jet-propulsion plants F02K; construction of compressors or fans F04; generating combustion products of high pressure or high velocity F23R; using gas turbines in compression refrigeration plants F25B11/00) - F01D: NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES (machines or engines for liquids F03; non-positive displacement pumps F04D) - F41H: ARMOUR; ARMOURED TURRETS; ARMOURED OR ARMED VEHICLES; MEANS OF ATTACK OR DEFENCE, e.g. CAMOUFLAGE, IN GENERAL - F05D: INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS ## Abstract A system platform includes a gas turbine engine coupled to a high power generator. The high power generator, driven by the gas turbine engine, supplies power to high power subsystems of the platform. ## Claims ### Claim 1 A weapon system platform comprising a high-energy beam unit configured to discharge high-energy beams, a gas turbine engine configured to provide power for the high-energy beam unit, the gas turbine engine including a compressor, a combustor, and a turbine, the combustor adapted to combine air received from the compressor with fuel and to burn the fuel to supply high pressure gasses toward the turbine to rotate an output shaft of the gas turbine engine, the gas turbine engine adapted to operate between an idling output level and a main power generation output level higher than the idling output level, a generator coupled to the output shaft of the gas turbine engine and adapted to generate electricity when driven by the gas turbine engine, an energy storage unit coupled to the generator and configured to store the electricity generated by the generator, a load applicator coupled to the gas turbine engine and configured to apply at least one of an electrical load on the energy storage unit and a mechanical load on the gas turbine engine, and a system controller configured to selectively operate the load applicator to increase an output level of the gas turbine engine above the idling output level and below the main power generation output level to cause an increase in an exhaust temperature of the gas turbine engine when the exhaust temperature is below a threshold level. ### Claim 2 (depends on 1) The system platform of claim 1, wherein the system controller is further configured to selectively increase the output of the gas turbine engine when an amount of electricity stored in the energy storage unit is below a threshold level. ### Claim 3 (depends on 2) The system platform of claim 2, wherein the load applicator is coupled to the energy storage unit and is configured to draw electricity from the energy storage unit. ### Claim 4 A weapon system platform comprising a high-energy beam unit configured to discharge high-energy beams, a gas turbine engine configured to provide power for the high-energy beam unit, the gas turbine engine including a compressor, a combustor, and a turbine, the combustor adapted to combine air received from the compressor with fuel and to burn the fuel to supply high pressure gasses toward the turbine to rotate an output shaft of the gas turbine engine, a generator coupled to the output shaft of the gas turbine engine and adapted to generate electricity when driven by the gas turbine engine, an energy storage unit coupled to the generator and configured to store the electricity generated by the generator, a load applicator coupled to the gas turbine engine, and a system controller configured to selectively operate the load applicator to apply a load on the gas turbine engine to increase an output level of the gas turbine engine to cause an increase in an exhaust temperature of the gas turbine engine, wherein the load applicator is configured to engage with a rotating component of the gas turbine engine to resist rotation of the rotating component. ### Claim 5 (depends on 2) The system platform of claim 2, wherein the load applicator is coupled to the energy storage unit and is configured to draw electricity from the energy storage unit. ### Claim 6 (depends on 1) The system platform of claim 1, further comprising a load shaft gearbox coupled to the output shaft and the generator, wherein the load shaft gearbox is configured to transfer rotation of the output shaft to the generator. ### Claim 7 (depends on 6) The system platform of claim 6, wherein the energy storage unit is a high power energy storage unit configured to power the high-energy beam unit, and wherein the generator is a high power generator configured to produce electricity to charge the high power energy storage unit during operation of the high-energy beam unit. ### Claim 8 (depends on 7) The system platform of claim 7, wherein the output of the gas turbine engine is selectively increased when the high-energy beam unit is operated. ### Claim 9 (depends on 7) The system platform of claim 7, further comprising a low power generator coupled to the load shaft gearbox and configured to generate electricity when driven by the gas turbine engine, and a low power energy storage unit coupled to the low power generator and configured to store the electricity generated by the low power generator. ### Claim 10 (depends on 9) The system platform of claim 9, wherein the load applicator is coupled to the low power energy storage unit. ### Claim 11 A method of operating a weapon system platform, the method comprising rotating a generator with a gas turbine engine to produce electricity, the gas turbine engine adapted to operate between an idling output level and a main power generation output level higher than the idling output level, storing the electricity produced by the generator in an energy storage unit, selectively providing electricity from the energy storage unit to a high-energy beam unit to cause an energized beam to be discharged, and selectively applying at least one of an electrical load on the energy storage unit and a mechanical load on the gas turbine engine with a load applicator to increase an output level of the gas turbine engine above the idling output level and below the main power generation output level to cause an increase in an exhaust temperature of the gas turbine engine when the exhaust temperature is below a threshold level. ### Claim 12 (depends on 11) The method of claim 11, wherein the output of the gas turbine engine is selectively increased when an amount of electricity stored in the energy storage unit is below a threshold level. ### Claim 13 (depends on 12) The method of claim 12, wherein the load applicator is coupled to the energy storage unit and is configured to draw electricity from the energy storage unit. ### Claim 14 (depends on 12) The method of claim 12, wherein the load applicator is configured to engage with a rotating component of the gas turbine engine to resist rotation of the rotating component. ### Claim 15 (depends on 14) The method of claim 14, wherein the load applicator is coupled to the energy storage unit and is configured to draw electricity from the energy storage unit. ### Claim 16 (depends on 11) The method of claim 11, wherein a load shaft gearbox is coupled to the output shaft and the generator, and wherein the load shaft gearbox is configured to transfer rotation of the output shaft to the generator. ### Claim 17 (depends on 16) The method of claim 16, wherein the energy storage unit is a high power energy storage unit configured to power the high-energy beam unit, and wherein the generator is a high power generator configured to produce electricity to charge the high power energy storage unit during operation of the high-energy beam unit. ### Claim 18 (depends on 17) The method of claim 17, wherein the output of the gas turbine engine is selectively increased when the high-energy beam unit is operated. ### Claim 19 (depends on 17) The method of claim 17, wherein a low power generator is coupled to the load shaft gearbox and configured to generate electricity when driven by the gas turbine engine, and wherein a low power energy storage unit is coupled to the low power generator and configured to store the electricity generated by the low power generator. ### Claim 20 (depends on 19) The method of claim 19, wherein the load applicator is coupled to the low power energy storage unit.