Winglet trailing edge venting
Airfoil venting systems are provided which include an airfoil (e.g., a winglet or an aircraft wing) having leading and trailing edges and an internal channel adapted to being fluid-connected to an on-board aircraft system which in use requires air to be exhausted. A series of venting apertures are positioned on at least a portion of the trailing edge of the airfoil and fluid-connected to the internal channel whereby air from the on-board aircraft system can be exhausted therethrough.
1. A winglet airfoil venting system comprising:
a winglet airfoil having upper and lower airfoil surfaces defining leading and trailing edges, and a planar trailing edge surface joining the trailing edges of the upper and lower airfoil surfaces;
an internal channel adapted to being fluid-connected to an onboard aircraft system which in use requires air to be exhausted; and
a series of venting apertures fluid-connected to the internal channel, the venting apertures being formed in and linearly aligned along at least a portion of the planar trailing edge surface of the winglet airfoil, wherein
exhaust air from the onboard aircraft system is discharged rearwardly from the trailing edge surface of the winglet airfoil through the linearly aligned venting apertures.
2. The airfoil venting system according to claim 1 , further comprising an internal manifold cavity fluid connecting the internal channel to the venting apertures.
3. The airfoil venting system according to claim 1 , wherein the venting apertures are positioned along an inboard, an outboard and/or an intermediate section of the trailing edge surface of the winglet airfoil.
4. An aircraft comprising a winglet airfoil which includes the winglet airfoil venting system according to claim 1 .
5. An aircraft comprising:
an onboard aircraft system which in use requires air to be exhausted;
a winglet airfoil having upper and lower airfoil surfaces defining leading and trailing edges, and a planar trailing edge surface joining the trailing edges of the upper and lower airfoil surfaces; and
a venting system to vent exhaust air from the onboard aircraft system from the planar trailing edge surface of the winglet airfoil, wherein the venting system comprises:
(i) an internal channel internally provided in the winglet airfoil which is fluid-connected to the onboard aircraft system to receive exhaust air therefrom; and
(ii) a series of venting apertures fluid-connected to the internal channel, the venting apertures being formed in and linearly aligned along at least a portion of the planar trailing edge surface of the winglet airfoil, wherein
exhaust air from the onboard aircraft system is discharged rearwardly from the planar trailing edge surface of the winglet airfoil through the linearly aligned venting apertures.
6. The aircraft according to claim 5 , wherein the airfoil venting system further comprises an internal manifold cavity fluid connecting the internal channel to the venting apertures.
7. The aircraft according to claim 5 , wherein the venting apertures are formed in and linearly positioned along an inboard, an outboard and/or an intermediate section of the planar trailing edge surface of the winglet airfoil.