Non-uniform and bi-tri stator spacing for swirl recovery vane (SRV) open rotor engines
A swirl recovery vane (SRV) open rotor engine include an engine core, a rotor having a plurality of rotor blades mounted to an end of the engine core and a plurality of stators mounted adjacent to the rotor. The stators are spaced in a non-uniform spacing to reduce a forcing function created by movement of the rotor blades past the stators.
1 . A swirl recovery vane (SRV) open rotor engine comprising:
an engine core;
a rotor having a plurality of rotor blades mounted to an end of the engine core; and
a plurality of stators mounted downstream of the rotor;
wherein the stators are spaced in a non-uniform spacing to create a negative reinforcement of a forcing function created by movement of the rotor blades past the stators, and
wherein the stators are spaced in a bi-tri spacing configuration comprising a first group of three groups of stators in a first spacing and a second group of three groups of stators in a second spacing different from the first spacing, wherein the groups of stators are arranged such that each group of the stators of the first group is circumferentially adjacent a pair of groups of stators of the second group.
2 . The SRV open rotor engine of claim 1 , wherein the stators are spaced to reduce an acoustic signature of the SRV open rotor engine with respect to a uniform spacing of the stators.
3 . The SRV open rotor engine of claim 1 , wherein the non-uniform spacing prevents interference with connection of the SRV open rotor engine to an engine pylon for connecting the engine to a wing.
4 . The SRV open rotor engine of claim 3 , wherein the non-uniform spacing comprises a local spacing adjustment to prevent interference with airflow.
5 . The SRV open rotor engine of claim 1 , wherein the non-uniform spacing enables air to flow between at least a portion of the stators and past an engine pylon connecting the SRV open rotor engine to a wing.
6 . The SRV open rotor engine of claim 1 , wherein the non-uniform spacing provides a positive resonance with respect to a first portion of the stators and a negative resonance with respect to a second portion of the stators.
7 . The SRV open rotor engine of claim 1 , wherein the stators comprise a predetermined number of stators to create a negative reinforcement of the forcing function for a given number of rotor blades.
8 . A swirl recovery vane (SRV) open rotor engine comprising:
an engine core;
a rotor having a plurality of rotor blades mounted to a front end of the engine core; and
a plurality of stators mounted aft of the rotor;
wherein the stators are spaced in a bi-tri spacing configuration to create a negative reinforcement of a forcing function created by movement of the rotor blades past the stators;
wherein the bi-tri spacing configuration of the stators provides a positive resonance with respect to a first portion of the stators and a negative resonance with respect to a second portion of the stators; and
wherein the bi-tri spacing configuration comprises a first group of three groups of stators in a first spacing and a second group of three groups of stators in a second spacing different from the first spacing, wherein the groups of stators are arranged such that each group of the stators of the first group is circumferentially adjacent a pair of groups of stators of the second group.
9 . The SRV open rotor engine of claim 8 , wherein the stators are further spaced to reduce an acoustic signature of the SRV open rotor engine with respect to a uniform spacing of the stators.
10 . The SRV open rotor engine of claim 8 , wherein the bi-tri spacing configuration prevents interference with connection of the SRV open rotor engine to an engine pylon for connecting the SRV open rotor engine to a wing.
11 . The SRV open rotor engine of claim 8 , wherein the bi-tri spacing configuration enables air to flow between at least a portion of the plurality of stators and past an engine pylon connecting the SRV open rotor engine to a wing.
12 . The SRV open rotor engine of claim 8 , wherein a number of the stators are selected to create a negative reinforcement of the forcing function for a given number of rotor blades.
13 . A propulsion system comprising:
an engine core;
a rotor having a plurality of rotor blades mounted to a front end of the engine core; and
a plurality of stators mounted aft of the rotor, wherein the stators are spaced in a bi-tri spacing configuration comprising a first group of three groups of stators in a first spacing and a second group of three groups of stators in a second spacing different from the first spacing, wherein the groups of stators are arranged such that each group of the stators of the first group is circumferentially adjacent a pair of groups of stators of the second group; and
wherein the stators are spaced in a non-uniform spacing about the engine core.
14 . The propulsion system of claim 13 , wherein the non-uniform spacing reduces an acoustic signature of the propulsion system with respect to a uniform spacing of the stators.
15 . The propulsion system of claim 13 , wherein the non-uniform spacing prevents interference with connection of the propulsion system to an engine pylon for connecting the propulsion system to a wing.
16 . The propulsion system of claim 13 , wherein the non-uniform spacing enables air to flow between at least a portion of the stators and past an engine pylon connecting the propulsion system to a wing.
17 . The propulsion system of claim 13 , wherein the non-uniform spacing provides a positive resonance with respect to a first portion of the stators and a negative resonance with respect to a second portion of the stators.
18 . The propulsion system of claim 13 , wherein the bi-tri spacing configuration is configured to create a negative reinforcement of a forcing function created by movement of the rotor blades past the stators.