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A multipoint combustion system for a gas turbine engine includes a housing defining a pressure vessel. A master injector is mounted to the housing for injecting fuel along a central axis. A plurality of slave injectors are each disposed outward of the master injector for injecting fuel and air in an

A multipoint combustion system for a gas turbine engine includes a housing defining a pressure vessel. A master injector is mounted to the housing for injecting fuel along a central axis. A plurality of slave injectors are each disposed outward of the master injector for injecting fuel and air in an ignition plume radially outward of fuel injected through the master injector. The master injector and slave injectors are configured and adapted so the injection plume of the master injector intersects with the ignition plumes of the slave injectors. A primary manifold is included within the pressure vessel for distributing fuel to the slave injectors. An auxiliary manifold is in fluid communication with the auxiliary nozzles of the slave injectors for issuing an auxiliary flow of fuel from the auxiliary nozzles that is separate from the fuel flow of the primary manifold.

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1. An injector for a low-calorific value fuel combustion system comprising: a nozzle body defining a fuel circuit for injecting low-calorific value fuel; andan auxiliary nozzle mounted to the nozzle body and defining a fuel circuit for injecting at least one of natural gas and liquid fuel;an inner s

1. An injector for a low-calorific value fuel combustion system comprising: a nozzle body defining a fuel circuit for injecting low-calorific value fuel; andan auxiliary nozzle mounted to the nozzle body and defining a fuel circuit for injecting at least one of natural gas and liquid fuel;an inner set of injection ports defined at an outlet of the nozzle body, wherein the inner set is configured to inject a flow of fuel;an intermediate set of injection ports defined radially outward from the inner set at an outlet of an air circuit, wherein the intermediate set is aligned to inject a converging, swirling flow of air, which intersects the flow of fuel from the innermost set; andan outer set of injection ports defined radially outward from the intermediate set at the outlet of the air circuit, wherein the outermost set is aligned to inject a converging, non-swirling flow of air, which converges into the flows of gas and air from innermost and intermediate sets,wherein the nozzle body includes an inner wall and an outer wall outboard of and spaced apart from the inner wall, wherein the fuel circuit of the nozzle body passes through the inner and outer walls, andwherein the auxiliary nozzle is inboard of and spaced apart from the inner wall of the nozzle body. 2. An injector as recited in claim 1, wherein the auxiliary nozzle is mounted to the nozzle body with a floating seal to accommodate a differential in thermal expansion between the auxiliary nozzle and the nozzle body. 3. An injector as recited in claim 1, wherein the fuel circuit of the nozzle body is annular and wherein the nozzle body defines an outer air circuit outboard of the fuel circuit of the nozzle body. 4. An injector as recited in claim 1, wherein the outer wall defines at least one aperture configured for passage of fuel from a fuel manifold into the nozzle body for selective injection of at least natural gas and LCV fuel gas in a proportional mix. 5. An injector as recited in claim 1, wherein the nozzle body and auxiliary nozzle define a common longitudinal axis, and wherein the auxiliary nozzle and nozzle body each include a respective fuel outlet, and wherein the fuel outlet of the auxiliary nozzle is upstream relative to the outlet of the nozzle body along the longitudinal axis. 6. An injector as recited in claim 1, wherein the auxiliary nozzle includes a fuel outlet configured and adapted to issue a spray of fuel that diverges away from a longitudinal axis defined by the auxiliary nozzle. 7. A multipoint combustion system for a gas turbine engine, comprising: a housing defining a pressure vessel;a master injector mounted to the housing for injecting fuel in an injection plume along a central axis defined through the pressure vessel;a plurality of slave injectors each disposed outward of and substantially parallel to the master injector for injecting fuel and air in an ignition plume radially outward of fuel injected through the master injector, wherein the master injector and slave injectors are configured and adapted so the injection plume of the master injector intersects with the ignition plumes of the slave injectors, wherein each of the slave injectors is an injector as recited in claim 1;a primary manifold within the pressure vessel for distributing fuel to the slave injectors; and an auxiliary manifold in fluid communication with the auxiliary nozzles of the slave injectors for issuing an auxiliary flow of fuel from the auxiliary nozzles that is separate from fuel I flow of the primary manifold, wherein the pressure vessel includes a pressure dome, wherein the auxiliary manifold and primary manifold are on opposing sides of the pressure dome, and wherein the primary and auxiliary manifolds are thermally isolated from one another. 8. A multipoint combustion system as recited in claim 7, wherein the pressure dome includes a central aperture and a central inlet fitting mounted to the central aperture of the pressure dome. 9. A multipoint combustion system as recited in claim 7, wherein the auxiliary nozzles of the slave injectors are mounted to the pressure vessel in a floating sealing engagement to accommodate thermal expansion differentials between the pressure vessel and the auxiliary manifold. 10. A multipoint combustion system as recited in claim 7, wherein the auxiliary manifold is flexible. 11. A multipoint combustion system as recited in claim 7, wherein the auxiliary manifold is configured and adapted to issue at least one of natural gas and liquid fuel to the auxiliary nozzles of the slave injectors. 12. A multipoint combustion system as recited in claim 7, wherein the auxiliary manifold is operatively connected to an external valve to permit purging of the auxiliary manifold and auxiliary nozzles with engine air for complete shutdown of the auxiliary manifold and nozzles. 13. A multipoint combustion system as recited in claim 7, further comprising an outlet bulkhead mounted to outlets of each of the master and slave injectors, the outlet bulkhead having an outlet opening sealed around an outlet of each injector. 14. A combustor system as recited in claim 13, wherein a floating collar is movably mounted to each outlet opening to seal between the outlet of each respective injector and the outlet bulkhead to accommodate relative thermal expansion and contraction of the injectors and outlet bulkhead.