초록 ▼

An axial flow positive displacement engine has an inlet axially spaced apart and upstream from an outlet. Inner and outer bodies have offset inner and outer axes extend from the inlet to the outlet through first, second, and third sections of a core assembly in serial downstream flow relationship. A

An axial flow positive displacement engine has an inlet axially spaced apart and upstream from an outlet. Inner and outer bodies have offset inner and outer axes extend from the inlet to the outlet through first, second, and third sections of a core assembly in serial downstream flow relationship. At least one of the bodies is rotatable about its axis. The inner and outer bodies have intermeshed inner and outer helical blades wound about the inner and outer axes respectively. The inner and outer helical blades extend radially outwardly and inwardly respectively. The helical blades have first, second, and third twist slopes in the first, second, and third sections respectively. The first twist slopes are less than the second twist slopes and the third twist slopes are less than the second twist slopes. A combustor section extends axially downstream through at least a portion of the second section.

대표청구항 ▼

What is claimed is: 1. An axial flow positive displacement machine comprising: an inlet axially spaced apart and upstream from an outlet, a core assembly including an inner body disposed within an outer body and the inner and outer bodies extending from the inlet to the outlet, the inner and outer

What is claimed is: 1. An axial flow positive displacement machine comprising: an inlet axially spaced apart and upstream from an outlet, a core assembly including an inner body disposed within an outer body and the inner and outer bodies extending from the inlet to the outlet, the inner and outer bodies having offset inner and outer axes respectively, at least one of the inner and outer bodies being rotatable about a corresponding one of the inner and outer axes, the inner and outer bodies having intermeshed inner and outer helical blades wound about the inner and outer axes respectively, the inner and outer helical blades extending radially outwardly and inwardly respectively, the inner helical blades extending radially outwardly from an inner hub of the inner body, the core assembly having first, second, and third sections in serial downstream flow relationship extending between the inlet and the outlet, the inner and outer helical blades having first, second, and third twist slopes in the first, second, and third sections respectively, the first twist slopes being less than the second twist slopes and the third twist slopes being less than the second twist slopes, and a combustor section extending axially downstream through at least a portion of the second section. 2. A machine as claimed in claim 1 further comprising the inner and outer helical blades in the first section having a sufficient number of turns to trap charges of air in the first section during the machine's operation. 3. A machine as claimed in claim 2 further comprising the number of turns being enough to mechanically trap the charges of air. 4. A machine as claimed in claim 2 further comprising the number of turns being enough to dynamically trap the charges of air. 5. A machine as claimed in claim 1 further comprising the outer body being rotatable about the outer axis and the inner body and being rotatable about the inner axis. 6. A machine as claimed in claim 4 further comprising the inner and outer bodies being geared together in a fixed gear ratio. 7. A machine as claimed in claim 6 further comprising the inner and outer helical blades in the first section having a sufficient number of turns to trap charges of air in the first section during the machine's operation. 8. A machine as claimed in claim 7 further comprising the number of turns being enough to mechanically trap the charges of air. 9. A machine as claimed in claim 7 further comprising the number of turns being enough to dynamically trap the charges of air. 10. A machine as claimed in claim 1 further comprising the outer body being rotatably fixed about the outer axis and the inner body being orbital about the outer axis. 11. A machine as claimed in claim 10 further comprising the inner and outer helical blades in the first section having a sufficient number of turns to trap charges of air in the first section during the machine's operation. 12. A machine as claimed in claim 11 further comprising the number of turns being enough to mechanically trap the charges of air. 13. A machine as claimed in claim 12 further comprising the number of turns being enough to dynamically trap the charges of air. 14. A gas turbine engine comprising: a gas generator connected in work producing relationship to a power consuming device, the gas generator including an inlet axially spaced apart and upstream from an outlet, a core assembly including an inner body disposed within an outer body and the inner and outer bodies extending from the inlet to the outlet, the inner and outer bodies having offset inner and outer axes respectively, at least one of the inner and outer bodies being rotatable about a corresponding one of the inner and outer axes, the inner and outer bodies having intermeshed inner and outer helical blades wound about the inner and outer axes respectively, the inner and outer helical blades extending radially outwardly and inwardly respectively, the inner helical blades extending radially outwardly from an inner hub of the inner body, the core assembly having first, second, and third sections in serial downstream flow relationship extending between the inlet and the outlet, the inner and outer helical blades having first, second, and third twist slopes in the first, second, and third sections respectively, the first twist slopes being less than the second twist slopes and the third twist slopes being less than the second twist slopes, and a combustor section extending axially downstream through at least a portion of the second section. 15. A machine as claimed in claim 14 further comprising the inner and outer helical blades in the first section having a sufficient number of turns to trap charges of air in the first section during the generator's operation. 16. A machine as claimed in claim 15 further comprising the number of turns being enough to mechanically trap the charges of air. 17. A machine as claimed in claim 15 further comprising the number of turns being enough to dynamically trap the charges of air. 18. A machine as claimed in claim 14 further comprising the outer body being rotatable about the outer axis and the inner body and being rotatable about the inner axis. 19. A machine as claimed in claim 15 further comprising the inner and outer bodies being geared together in a fixed gear ratio. 20. A machine as claimed in claim 19 further comprising the inner and outer helical blades in the first section having a sufficient number of turns to trap charges of air in the first section during the generator's operation. 21. A machine as claimed in claim 20 further comprising the number of turns being enough to mechanically trap the charges of air. 22. A machine as claimed in claim 20 further comprising the number of turns being enough to dynamically trap the charges of air. 23. A machine as claimed in claim 14 further comprising the outer body being rotatably fixed about the outer axis and the inner body being orbital about the outer axis. 24. A machine as claimed in claim 23 further comprising the inner and outer helical blades in the first section having a sufficient number of turns to trap charges of air in the first section during the generator's operation. 25. A machine as claimed in claim 24 further comprising the number of turns being enough to mechanically trap the charges of air. 26. A machine as claimed in claim 25 further comprising the number of turns being enough to dynamically trap the charges of air. 27. An aircraft gas turbine engine comprising: a fan section and a core engine including a gas generator downstream of the fan section, a turbine having at least one row of turbine rotor blades downstream of the gas generator, the turbine drivingly attached to at least one row of circumferentially spaced apart fan rotor blades in the fan section by a shaft, the gas generator including an inlet axially spaced apart and upstream from an outlet, a core assembly including an inner body disposed within an outer body and the inner and outer bodies extending from the inlet to the outlet, the inner and outer bodies having offset inner and outer axes respectively, at least one of the inner and outer bodies being rotatable about a corresponding one of the inner and outer axes, the inner and outer bodies having intermeshed inner and outer helical blades wound about the inner and outer axes respectively, the inner and outer helical blades extending radially outwardly and inwardly respectively, the inner helical blades extending radially outwardly from an inner hub of the inner body, the core assembly having first, second, and third sections in serial downstream flow relationship extending between the inlet and the outlet, the inner and outer helical blades having first, second, and third twist slopes in the first, second, and third sections respectively, the first twist slopes being less than the second twist slopes and the third twist slopes being less than the second twist slopes, and a combustor section extending axially downstream through at least a portion of the second section. 28. A machine as claimed in claim 27 further comprising the inner and outer helical blades in the first section having a sufficient number of turns to trap charges of air in the first section during the generator's operation. 29. A machine as claimed in claim 28 further comprising the number of turns being enough to mechanically trap the charges of air. 30. A machine as claimed in claim 28 further comprising the number of turns being enough to dynamically trap the charges of air. 31. A machine as claimed in claim 27 further comprising the outer body being rotatable about the outer axis and the inner body and being rotatable about the inner axis. 32. A machine as claimed in claim 28 further comprising the inner and outer bodies being geared together in a fixed gear ratio. 33. A machine as claimed in claim 32 further comprising the inner and outer helical blades in the first section having a sufficient number of turns to trap charges of air in the first section during the generator's operation. 34. A machine as claimed in claim 33 further comprising the number of turns being enough to mechanically trap the charges of air. 35. A machine as claimed in claim 33 further comprising the number of turns being enough to dynamically trap the charges of air. 36. A machine as claimed in claim 27 further comprising the outer body being rotatably fixed about the outer axis and the inner body being orbital about the outer axis. 37. A machine as claimed in claim 36 further comprising the inner and outer helical blades in the first section having a sufficient number of turns to trap charges of air in the first section during the generator's operation. 38. A machine as claimed in claim 37 further comprising the number of turns being enough to mechanically trap the charges of air. 39. A machine as claimed in claim 38 further comprising the number of turns being enough to dynamically trap the charges of air. 40. An aircraft gas turbine engine comprising: a fan section and a core engine including a gas generator downstream of the fan section, a turbine having at least one row of turbine rotor blades downstream of the gas generator, the turbine drivingly attached to at least one row of circumferentially spaced apart fan rotor blades in the fan section by a shaft, the gas generator including an inlet axially spaced apart and upstream from an outlet, a core assembly including an inner body disposed within an outer body and the inner and outer bodies extending from the inlet to the outlet, the inner and outer bodies having offset inner and outer axes respectively, the inner and outer bodies being rotatable about the inner and outer axes respectively, the inner and outer bodies having intermeshed inner and outer helical blades wound about the inner and outer axes respectively, the inner and outer helical blades extending radially outwardly and inwardly respectively, the inner helical blades extending radially outwardly from an inner hub of the inner body, the core assembly having first, second, and third sections in serial downstream flow relationship extending between the inlet and the outlet, the inner and outer helical blades having first, second, and third twist slopes in the first, second, and third sections respectively, the first twist slopes being less than the second twist slopes and the third twist slopes being less than the second twist slopes, and a combustor section extending axially downstream through at least a portion of the second section. 41. A machine as claimed in claim 40 further comprising the inner and outer helical blades in the first section having a sufficient number of turns to trap charges of air in the first section during the generator's operation. 42. A machine as claimed in claim 41 further comprising the number of turns being enough to mechanically trap the charges of air. 43. A machine as claimed in claim 40 further comprising the inner and outer bodies being geared together in a fixed gear ratio. 44. A machine as claimed in claim 43 further comprising the inner and outer helical blades in the first section having a sufficient number of turns to trap charges of air in the first section during the generator's operation and the number of turns being enough to mechanically trap the charges of air.