Fuel feed passages for an attritable engine
An additively manufactured attritable engine includes a compressor section, a combustion section, a turbine section, and an engine case wall, which surrounds the compressor section, the combustion section, and the turbine section. The engine case wall includes a first cavity embedded in the engine case wall that defines an injector that is in fluid communication with the combustion section. The engine case wall includes a second cavity embedded within the engine case wall and defines a fuel feed passage that is in thermal communication through the exterior surface of the engine case wall.
1. A method of testing a fluid dispensing system in an engine that includes a fuel line and an N number of injectors, the method comprising:
applying cooling to an exterior surface adjacent each fuel feed passage for each of (N−1) injectors;
inducing a phase change to a flow test fluid in each of (N−1) fuel feed passages, preventing flow through each of (N−1) injectors; and
measuring a flow rate of the flow test fluid through a single unblocked injector.
2. The method of claim 1 , further comprising:
applying cooling to an exterior surface adjacent the single unblocked injector;
inducing a phase change to a flow test fluid in the fuel feed passage in fluid communication with the single unblocked injector, preventing flow through the single unblocked injector;
inducing a phase change to a flow test fluid in one of the (N−1) fuel feed passages, allowing flow through one of the (N−1) injectors; and
measuring a flow rate of the flow test fluid through one of the (N−1) injectors.
3. The method of claim 1 , wherein
the engine includes a compressor section, a combustion section, a turbine section and an engine case wall surrounding the compressor section, the combustion section and the turbine section;
the engine case wall extends radially between an interior surface of the engine case wall and the exterior surface; and
the injectors and the fuel feed passages are formed by and embedded within material of the engine case wall.
4. The method of claim 3 , wherein the fuel line is formed by and embedded within the material of the engine case wall.
5. The method of claim 4 , wherein the fuel line extends circumferentially around the engine case wall.
6. The method of claim 3 , wherein the engine case wall comprises a nickel alloy.
7. The method of claim 3 , wherein
the combustor section includes a combustor and a combustor wall forming a radial outer boundary of the combustor; and
the engine case wall is separated from the combustor wall by an air channel.
8. The method of claim 1 , wherein the fuel feed passages are parallel to the exterior surface.
9. The method of claim 1 , wherein
the engine includes a combustor section and an engine case wall housing the combustor section;
the engine case wall comprises the fuel line, the fuel feed passages and the injectors;
the fuel line extends circumferentially about an axis within material of the engine case wall;
the fuel feed passages extend axially within the material of the engine case wall; and
the injectors extend within the material of the engine case wall.
10. A testing method, comprising:
providing a structure of an engine, the structure including a fuel line, a first injector, a second injector, a first fuel feed passage and a second fuel feed passage, the first fuel feed passage extending from the fuel line to the first injector, and the second fuel feed passage extending from the fuel line to the second injector;
disposing a flow test fluid in the first fuel feed passage;
cooling an exterior surface of the structure adjacent the first fuel feed passage to induce a phase change in the flow test fluid in the first fuel feed passage and thereby block fluid flow through the first injector, wherein the second injector remains unblocked; and
measuring a flow rate of the flow test fluid through the second injector.