Propfan engine
The present disclosure relates to a propfan engine comprising: one or more rotor stages comprising a plurality of rotors; and an outer wall comprising an outer profile, at least a portion of the outer profile defining a substantially circular cross-section, wherein the diameter of the substantially circular cross-section increases in the direction of flow over the outer wall and downstream of a leading edge of the rotors, and the diameter increases at substantially all points defining the circumference of the substantially circular cross-section.
1. A propfan engine comprising:
one or more rotor stages comprising a plurality of rotors; and
an outer wall comprising an outer profile, at least a portion of the outer profile comprising a substantially circular cross-section, wherein
the diameter of the substantially circular cross-section increases in the direction of flow over the outer wall and downstream of a leading edge of the rotors, and the diameter increases at substantially all points defining the circumference of the substantially circular cross-section, wherein the diameter increases at an increasing rate in a first part of the portion of the outer profile, and the diameter increases at a decreasing rate in a second part of the portion of the outer profile.
2. The propfan engine of claim 1 , wherein the second part is downstream of the first part of the portion of the outer profile and there is a point of inflection in the outer profile between the first and second parts of the portion of the outer profile.
3. The propfan engine of claim 1 , wherein the radius of the curvature in the first part of the portion of the outer profile is substantially 20% of a maximum diameter of the propfan outer wall.
4. The propfan engine of claim 1 , wherein in a third part of the portion of the outer profile the diameter of the substantially circular cross-section reduces in the direction of flow over the outer wall.
5. The propfan engine of claim 4 , wherein the radius of the curvature of the second and/or third parts of the portion of the outer profile is in the range of substantially 40% to substantially 130% of a maximum diameter of the propfan outer wall.
6. The propfan engine of claim 1 ,
wherein in a third part of the portion of the outer profile the diameter of the substantially circular cross-section reduces in the direction of flow over the outer wall, and
wherein the third part is downstream of the first part and/or second part of the portion of the outer profile and there is a local maximum in the cross-section diameter in the outer profile between the third part and the first and/or second parts of the portion of the outer profile.
7. The propfan engine of claim 6 , wherein the radius of the curvature of the second and/or third parts of the portion of the outer profile is in the range of substantially 40% to substantially 130% of a maximum diameter of the propfan outer wall.
8. The propfan engine of claim 2 , wherein the radius of the curvature of the second and/or third parts of the portion of the outer profile is substantially 40% of a maximum diameter of the propfan outer wall.
9. The propfan engine of claim 2 , wherein the radius of the curvature of the second and/or third parts of the portion of the outer profile is substantially 40% of a maximum diameter of the propfan outer wall.
10. The propfan engine of claim 1 , wherein the diameter of the substantially circular cross-section starts to increase upstream of a trailing edge of the rotors.
11. The propfan of claim 1 , wherein a cross-section of the outer profile comprises a maximum diameter at a point upstream of a leading edge of the rotors, the diameter reducing between the maximum diameter and the leading edge of the rotors, and wherein the outer profile comprises a point of inflection between the maximum diameter and the leading edge of the rotors.
12. The propfan of claim 1 , wherein the propfan engine comprises a first rotor stage and a second rotor stage, each rotor stage having associated with it an increase in the diameter of the substantially circular cross-section downstream of the respective rotor leading edges.
13. A propfan engine comprising:
one or more rotor stages comprising a plurality of rotors; and
an outer wall comprising an outer profile, the outer profile defining a cross-section, wherein
the cross-section of the outer profile comprises a maximum diameter at a point upstream of a leading edge of the rotors, the diameter reducing between the maximum diameter and the leading edge of the rotors, and wherein
the outer profile comprises a point of inflection between the maximum diameter and the leading edge of the rotors.
14. The propfan engine of claim 13 , wherein the reduction in the diameter between the maximum diameter and the leading edge of the rotors finishes substantially in line with the leading edge of the rotors, and a first part of the reduction in the diameter between the maximum diameter and the leading edge of the rotors reduces at an increasing rate.
15. The propfan engine of claim 14 , wherein the first part of the reduction in the diameter between the maximum diameter and the leading edge of the rotors comprises a radius of curvature substantially 130% of the maximum diameter of the propfan outer wall.
16. The propfan engine of claim 13 , wherein a second part of the reduction in the diameter between the maximum diameter and the leading edge of the rotors reduces at a decreasing rate, and the reduction in the diameter between the maximum diameter and the leading edge of the rotors comprises a radius of curvature substantially 25% of the maximum diameter of the propfan outer wall.
17. A propfan engine comprising:
one or more rotor stages comprising a plurality of rotors; and
an outer wall comprising an outer profile, at least a portion of the outer profile comprising a substantially circular cross-section, wherein
the diameter of the substantially circular cross-section increases in the direction of flow over the outer wall and downstream of a leading edge of the rotors, and the diameter increases at substantially all points defining the circumference of the substantially circular cross-section, wherein a cross-section of the outer profile comprises a maximum diameter at a point upstream of a leading edge of the rotors, the diameter reducing between the maximum diameter and the leading edge of the rotors, and wherein the outer profile comprises a point of inflection between the maximum diameter and the leading edge of the rotors.