Engine cowl incorporating an equipment ventilation circuit
An aircraft propulsion engine including a fan case, and a cowl forming part of the nacelle of the engine and being designed to at least partially surround the case leaving a space between the cowl and the case, in which space at least one piece of equipment is mounted and extends along the axis of the engine, is provided. The cowl includes a wall and wall stiffeners fixed to the internal face of the wall. At least a part of the stiffeners of the cowl is arranged to form air guide ducts, the air guide ducts being assembled into an air distribution circuit to ventilate the equipment.
1. An aircraft propulsion engine comprising:
a case;
a cowl forming part of a nacelle of the engine, the cowl being designed to at least partially surround said case leaving a space between the cowl and the case; and
at least one piece of equipment which is mounted in the space and extends along an axis of said engine,
wherein the cowl comprises a wall and wall stiffeners fixed to an internal face of the wall,
wherein at least a part of the stiffeners is arranged to form air guide ducts, said air guide ducts being assembled into an air distribution system to ventilate said at least one piece of equipment,
wherein the air distribution system comprises air guiding stiffeners arranged in a longitudinal direction and air guiding stiffeners arranged in a transverse direction, connecting members joining the stiffeners together into an air distribution circuit,
wherein the air distribution system comprises an air bleed tap in contact with an outside of said cowl, a ventilation accessory situated inside said cowl, said ventilation accessory being connected with said bleed tap, said ventilation accessory being able to cause the air to circulate in said air distribution system,
wherein the ventilation accessory comprises a blower which is fixed to the internal face of the wall of the cowl,
wherein the air distribution circuit is made up of stiffener elements which are arranged to form air guide ducts and which are joined together in an airtight manner, and
wherein a part of said stiffeners forming air guide ducts comprises perforations for ventilating said equipment.
2. The engine as claimed in claim 1 , wherein said stiffeners have a cross section with an air guiding part and flanges for attaching to the wall.
3. The engine as claimed in claim 2 , wherein the air guiding part collaborates with the wall to form an air guide duct.
4. The engine as claimed in claim 3 , wherein said stiffeners have an omega-shaped cross section with a central air-guiding part and lateral flanges for attaching to the wall.
5. The engine as claimed in claim 1 , wherein the case is a fan case.
6. The engine as claimed in claim 1 , wherein the at least one piece of equipment is an actuator.
7. The engine as claimed in claim 6 , wherein the actuator operates a thrust reverser member.