# US 10,309,303 B2 · Systems and methods of generating electrical power > Agents: this data is available as JSON from the patentgrep API and MCP server — see https://patentgrep.com/llms.txt - Number: US 10,309,303 B2 - Document ID: US10309303B2 - Status: Granted - Kind: B2 - Application number: 15/236,085 - Filed: 2016-08-12 - Published: 2018-02-15 - Granted: 2019-06-04 - Earliest claimed: 2016-08-12 - Assignees: Hamilton Sundstrand Corporation - Applicants: Hamilton Sundstrand Corporation - Inventors: Robert A. Bayles; Todd A. Spierling; Louis J. Bruno; Harold W. Hipsky - Web page: https://patentgrep.com/patent/US10309303B2 ## CPC - F02C 6/08: the gas being bled from the gas-turbine compressor - F01D 15/10: Adaptations for driving, or combinations with, electric generators - F02C 3/04: having a turbine driving a compressor (power transmission arrangements F02C7/36; control of working fluid flow F02C9/16) - F02C 7/32: Arrangement, mounting, or driving, of auxiliaries - H02K 7/1823: {structurally associated with turbines or similar engines} - F05D 2220/50: for auxiliary power units (APU's) - 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) - H02K: DYNAMO-ELECTRIC MACHINES (dynamo-electric relays H01H53/00; conversion of DC or AC input power into surge output power {H03K3/53}) - F05D: INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS ## Abstract A generator arrangement includes a generator and a pneumatic turbine. The pneumatic turbine is operably connected to the generator. A gas turbine engine compressor section is in fluid communication with the pneumatic turbine through a bleed air conduit to provide pressurized air to the pneumatic turbine for applying mechanical rotation to the generator. ## Claims ### Claim 1 A generator arrangement of a power system, comprising: a first generator assembly having a first pneumatic turbine operably connected to a first generator; a second generator assembly having a second pneumatic turbine operably connected to a second generator; a first bleed air conduit fluidly connecting a first gas turbine engine with the first generator assembly; a second bleed air conduit fluidly connecting a second gas turbine engine with the second generator assembly, a first and a second coolant conduits providing a bleed air flow of high pressure air discharged by the respective first and second gas turbine engine in the same direction to the first and second respective generator assemblies; a crossover conduit connected between the first bleed air conduit and the second bleed air conduit; and a crossover valve disposed along the crossover conduit configured to control the bleed air flow in the crossover conduit to selectively place both of the first and second generator assemblies in fluid communication with a common compressor section of the first and second gas turbine engines. ### Claim 2 (depends on 1) The generator arrangement as recited in claim 1, further comprising a fuselage, a belly fairing, or an engine fairing separating the first and second generator assemblies from the external environment. ### Claim 3 (depends on 1) The generator arrangement as recited in claim 1, further comprising a first shaft connecting the first pneumatic turbine with the first generator and a second shaft connecting the second pneumatic turbine with the second generator. ### Claim 4 (depends on 1) The generator arrangement as recited in claim 1, further comprising a gearbox connecting the first pneumatic turbine with the first generator and a second shaft connecting the second pneumatic turbine with the second generator. ### Claim 5 (depends on 1) The generator arrangement as recited in claim 1, further comprising at least one flow control valve in fluid communication with the first and second gas turbine engines. ### Claim 6 (depends on 1) The generator arrangement as recited in claim 1, further comprising a second crossover conduit in fluid communication with the first and second pneumatic turbines. ### Claim 7 (depends on 1) The generator arrangement as recited in claim 1, further comprising a second crossover valve disposed along the second crossover conduit configured to control fluid flow in the second conduit to selectively allow for fluid communication with the first pneumatic turbine, the second pneumatic turbine, or both the first and second pneumatic turbines. ### Claim 8 (depends on 1) The generator arrangement as recited in claim 1, further comprising a shutoff valve in fluid communication with the first and second pneumatic turbines. ### Claim 9 (depends on 1) The generator arrangement as recited in claim 1, wherein the first coolant conduit is fluidly connected to the first pneumatic turbine with the first generator, the coolant conduit providing an expanded bleed air flow discharged by the first pneumatic turbine as a coolant flow for cooling the first generator. ### Claim 10 (depends on 1) The generator arrangement as recited in claim 1, further comprising a high voltage direct current power converter in electrical communication with the first generator. ### Claim 11 (depends on 1) The generator arrangement as recited in claim 1, wherein the first pneumatic turbine is operably connected to the second generator. ### Claim 12 (depends on 1) The generator arrangement as recited in claim 1, further comprising a heat exchanger in fluid communication with the first pneumatic turbine through the first generator. ### Claim 13 (depends on 1) The generator arrangement as recited in claim 1, wherein the second pneumatic turbine in is fluid communication with the first pneumatic turbine and is operably connected to the second generator. ### Claim 14 (depends on 1) The generator arrangement as recited in claim 1, wherein the first coolant conduit is fluidly connected to the first pneumatic turbine with the first generator, the coolant conduit providing an expanded bleed air flow discharged by the first pneumatic turbine as a coolant flow for cooling the first generator; a high voltage direct current power converter in electrical communication with the first generator; and a heat exchanger in fluid communication with the first pneumatic turbine through the first generator, wherein the first pneumatic turbine is operably connected to the second generator. ### Claim 15 An electrical system, comprising: a first generator assembly having a first pneumatic turbine operably connected to a first generator; a second generator assembly baying a second pneumatic turbine operably connected to a second generator; a first gas turbine engine having a first compressor section; a second gas turbine engine having a second compressor section; a first bleed air conduit fluidly connecting the first gas turbine engine with the first generator assembly; a second bleed air conduit fluidly connecting the second gas turbine engine with the second generator assembly; a first and a second coolant conduits providing a bleed air flow of high pressure air discharged by the respective first and second gas turbine engines in the same direction to the first and second respective generator assemblies; a crossover conduit connected between the first bleed air conduit and the second bleed air conduit; and a crossover valve disposed along the crossover conduit configured to control the bleed air flow to either or both of the first and second pneumatic turbines; wherein the cross-bleed conduit is configured to provide the bleed air flow to either or both of the first and second pneumatic turbines, fluidly connect the first gas turbine compressor section with the second pneumatic turbine, and fluidly connects the second gas turbine compressor section with the first pneumatic turbine. ### Claim 16 (depends on 15) The electrical system a recited in claim 15, wherein the first generator is separated from the external environment by a first belly fairing, wherein the second generate is separated from the external environment by a second belly fairing. ### Claim 17 (depends on 15) The electrical system as recited in claim 15, further comprising a shutoff valve in fluid communication with the first pneumatic turbine and the second pneumatic turbine of the second generator arrangement.