ORC turbine and generator, and method of making a turbine

1. An axial turbine, comprising:

a turbine shaft;

a housing;

a plurality of rotor plates rotatably disposed in said housing, each of the plurality of rotor plates having a centerline, a first contact surface and a second contact surface, said first and second contact surfaces being substantially parallel and each of said first and second contact surfaces being flat in the range 0.00005″ to 0.020″, wherein said plurality of rotor plates are positioned proximate one another so that said centerlines thereof are mutually coaxial and are coaxial with a first axis of rotation so as to define rotor portions of a multi-stage rotor assembly, the multi-stage rotor assembly being releasably coupled to an end of the turbine shaft in an overhung configuration; and

a plurality of stator plates, each having a centerline, a first contact surface and a second contact surface, said first and second contact surfaces being substantially parallel and each of said first and second contact surfaces being flat in the range 0.00005″ to 0.020″, wherein said plurality of stator plates are positioned proximate one another so that said centerlines of said stator plates are mutually coaxial and are coaxial with said first axis of rotation so as to define stator portions of a multi-stage stator assembly, the multi-stage stator assembly forming a unitary cartridge that is releasably coupled to said housing.

2. An axial turbine according to claim 1 , wherein said plurality of stator plates includes a first stator plate having a plurality of vanes and a first vane pitch S and a second stator plate, said first stator plate being circumferentially clocked with respect to said second stator plate.

3. An axial turbine according to claim 1 , wherein said plurality of rotor plates includes a first rotor plate having a plurality of vanes and a first rotor vane pitch S and a second rotor plate, said first rotor plate being circumferentially clocked with respect to said second rotor plate.

4. An axial turbine according to claim 1 , wherein said first and second contact surfaces of said rotor plates are parallel to within 0.0001″ to 0.015″ and said first and second contact surfaces of said stator plates are parallel to within 0.0001″ to 0.015″.

5. An axial turbine according to claim 4 , wherein said first and second contact surfaces of said rotor plates are parallel to within 0.0005″ to 0.005″ and said first and second contact surfaces of said stator plates are parallel to within 0.0005″ to 0.005″.

6. An axial turbine according to claim 1 , wherein said plurality of rotor plates are secured with respect to one another and said plurality of stator plates are secured with respect to one another and positioned relative to said plurality of rotor plates.

7. An axial turbine according to claim 1 , wherein each of said plurality of rotor plates having a radially outermost portion and each of said plurality of stator plates having a radially innermost portion, the axial turbine further comprising a first plurality of brush seals and a second plurality of brush seals, each of said first plurality of brush seals positioned proximate said radially outermost portion of a corresponding respective one of said plurality of rotors and each of said second plurality of brush seals positioned proximate said radially innermost portion of a corresponding respective one of said plurality of stators.

8. A turbine according to claim 1 , wherein said plurality of rotor plates are positioned in alternating relationship with corresponding respective ones of said plurality of stator plates, further wherein at least one of said plurality of rotor plates includes a first plurality of vanes with an axial chord and an adjacent one of said plurality of stator plates includes a second plurality of vanes with an axial chord, wherein said first plurality of vanes is axially spaced from said second plurality of vanes to define a space having an axial dimension that is no more than two axial chords to ¼ of 1% of an axial chord, as measured with respect to the axial chord of the one of said rotor plate and stator plate immediately upstream of said space.

9. A turbine comprising:

a shaft, a housing;

at least one stator including a plurality of stator plates, the plurality of stator plates forming a stator assembly that is releasably secured to said housing; and

at least one rotor supported for rotational movement relative to said at least one stator about a rotational axis, said at least one rotor including a plurality of turbine rotor plates, the plurality of turbine rotor plates forming a rotor assembly that is releasably secured to said shaft;

wherein said turbine is designed and configured to be operably coupled to a generator, said turbine having a stage reaction that is designed and configured to be result in a thrust that is less than an available thrust capability of the generator.

10. A turbine according to claim 9 , wherein the rotor assembly is coupled to the shaft in an overhung configuration.

11. A turbine according to claim 9 , wherein the turbine further includes a stub shaft coupled to an end of the shaft, and wherein the rotor assembly has a first end facing the stub shaft and a second opposite end, wherein the first end of the rotor assembly is releasably coupled to the stub shaft, the rotor assembly configured to transmit a torque from the second end of the rotor assembly to the shaft via the rotor assembly and stub shaft.

12. A turbine according to claim 9 , wherein said stage reaction ranges from −0.1 to +0.3.

13. A turbine according to claim 9 , wherein said stage reaction ranges from −0.05 to +0.15.

14. A turbine according to claim 9 , wherein the plurality of stator plates and plurality of turbine rotor plates are configured as a unitary cartridge that is releasably coupled to said housing.

15. A turbine comprising:

a shaft, a housing;

at least one stator including a plurality of stator plates, the plurality of stator plates forming a stator assembly that is releasably secured to said housing; and

at least one rotor supported for rotational movement relative to said at least one stator about a rotational axis, said at least one rotor including a plurality of turbine rotor plates, the plurality of turbine rotor plates forming a rotor assembly that is releasably secured to said shaft, wherein the rotor assembly is coupled to the shaft and unsupported on one end in an overhung configuration.

16. A turbine according to claim 15 , wherein said turbine is designed and configured to be operably coupled to a generator, said turbine having a stage reaction that is designed and configured to result in a thrust that is less than an available thrust capability of the generator.

17. A turbine according to claim 16 , wherein said stage reaction ranges from −0.1 to +0.3.

18. A turbine according to claim 16 , wherein said stage reaction ranges from −0.05 to +0.15.

19. A turbine according to claim 15 , wherein the plurality of stator plates and plurality of turbine rotor plates are configured as a unitary cartridge that is releasably coupled to said housing.

20. A turbine comprising:

a shaft, a housing;

at least one stator including a plurality of stator plates, the plurality of stator plates forming a stator assembly that is releasably secured to said housing; and

at least one rotor supported for rotational movement relative to said at least one stator about a rotational axis, said at least one rotor including a plurality of turbine rotor plates, the plurality of turbine rotor plates forming a rotor assembly that is releasably secured to said shaft

wherein the turbine further includes a stub shaft coupled to an end of the shaft, and

wherein the rotor assembly has a first end facing the stub shaft and a second, opposite end, wherein the first end of the rotor assembly is releasably coupled to the stub shaft, the rotor assembly configured to transmit a torque from the second end of the rotor assembly to the shaft via the rotor assembly and the stub shaft.

21. A turbine according to claim 20 , wherein the plurality of stator plates and plurality of turbine rotor plates are configured as a unitary cartridge that is releasably coupled to said housing.