Optimized aircraft pylon fairing
Pylon fairings for an aircraft turbojet engine mounted below an aircraft wing are provided with inboard and outboard lateral faces which converge rearwardly to form a trailing edge of the pylon fairing and which are positioned so as to contact a portion of a cold flow exiting a fan duct of the turbojet engine, and a bottom face positioned above a hot exhaust flow exiting an exhaust nozzle of the turbojet engine. The trailing edge of the pylon fairing extends in an upward direction relative to an engine longitudinal axis of symmetry between a lower terminus at the bottom face and an upper terminus located at a lower surface of the aircraft wing. The lower terminus is coincident with a longitudinal midplane of the turbojet engine, and the upper terminus is offset in an inboard direction so that the trailing edge of the pylon fairing is cambered in the inboard direction between the lower terminus and the upper terminus.
1. A pylon fairing for an aircraft turbojet engine mounted below an aircraft wing, wherein the pylon fairing comprises:
inboard and outboard lateral faces which converge rearwardly to form a trailing edge of the pylon fairing and positioned so as to contact a portion of a cold flow exiting a fan duct of the turbojet engine, and a bottom face positioned above a hot exhaust flow exiting an exhaust nozzle of the turbojet engine, wherein
the trailing edge of the pylon fairing extends in an upward direction relative to the engine longitudinal axis between a lower terminus at the bottom face and an upper terminus located at a lower surface of the aircraft wing, and wherein
the lower terminus is coincident with the vertical mid-plane passing through the longitudinal axis of the turbojet engine, and the upper terminus is offset in an inboard direction so that the trailing edge of the pylon fairing is cambered in the inboard direction between the lower terminus and the upper terminus.
2. The pylon fairing as in claim 1 , wherein each of the inboard and outboard lateral faces is convex.
3. The pylon fairing as in claim 1 , wherein the bottom face is concave.
4. The pylon fairing as in claim 1 , wherein the trailing edge of the pylon fairing is linear between the lower terminus and the upper terminus thereof.
5. The pylon fairing as in claim 1 , wherein the trailing edge is concavely cambered in an inboard direction.
6. An aircraft comprising a fuselage, port and starboard wings extending laterally from the fuselage, and port and starboard turbojet engines mounted below the port and starboard wings, wherein each of the port and starboard turbojet engines comprises a pylon fairing as in claim 1 .
7. A pylon mounting assembly for below wing mounting of a turbojet engine comprising:
a mounting pylon for suspending the turbojet engine below the wing so that an intake of the turbojet engine is positioned forwardly of a leading edge of the wing; and
a pylon fairing for the mounting pylon comprising inboard and outboard lateral faces which converge rearwardly to form a trailing edge of the pylon fairing and positioned so as to contact a portion of a cold flow exiting a fan duct of the turbojet engine, and a bottom face positioned above a hot exhaust flow exiting an exhaust nozzle of the turbojet engine, wherein
the trailing edge of the pylon fairing extends in an upward direction relative to the engine longitudinal axis between a lower terminus at the bottom face and an upper terminus located at a lower surface of the aircraft wing, and wherein
the lower terminus is coincident with the vertical midplane passing through the longitudinal axis of the turbojet engine, and the upper terminus is offset in an inboard direction so that the trailing edge of the pylon fairing is cambered in the inboard direction between the lower terminus and the upper terminus.
8. The pylon mounting assembly as in claim 7 , wherein each of the inboard and outboard lateral faces is convex.
9. The pylon mounting assembly as in claim 7 , wherein the bottom face is concave.
10. The pylon mounting assembly as in claim 7 , wherein the trailing edge of the pylon fairing is linear between the lower terminus and the upper terminus thereof.
11. The pylon mounting assembly as in claim 7 , wherein the trailing edge is concavely cambered in an inboard direction.