Heat recovery system, in particular for use on aircraft, using a two-phase fluid circuit
The system comprises at least one evaporator device arranged around a tube inside which a hot fluid flows and, for each evaporator device, a respective conduit connected at its opposite ends to the evaporator device so as to form with the latter a closed circuit containing a two-phase fluid. Each evaporator device comprises a casing, having an inner wall in contact with the respective tube and an outer wall enclosing a cavity with the inner wall, and a separating member of porous material arranged inside the casing so as to divide radially the cavity into an inner cavity, extending between the inner wall and the separating member, and an outer cavity extending between the separating member and the outer wall. Each conduit is in fluid communication at its opposite ends with the inner cavity and with the outer cavity, respectively, of the respective evaporator device so as to allow fluid in vapor phase to flow out from the evaporator device and the fluid in liquid phase to flow back into the evaporator device, respectively.
1. A heat recovery system for recovering heat from a hot fluid flowing in at least one tube, in particular from hot air drawn from a high-temperature compression stage of an aircraft engine, the system comprising at least one evaporator device arranged around said at least one tube and, for each evaporator device, a respective conduit connected at its opposite ends to the evaporator device so as to form with the latter a closed circuit containing a two-phase fluid,
wherein each evaporator device comprises a casing, having an inner wall in contact with the respective tube and an outer wall enclosing a cavity with the inner wall, and a separating member arranged inside the casing so as to divide radially the cavity into an inner cavity, extending between the inner wall and the separating member, and an outer cavity, extending between the separating member and the outer wall, the separating member being made of porous material so as to allow the fluid to flow radially by capillarity through the separating member in the direction from the outer cavity to the inner cavity,
wherein the inner wall and the outer wall of each evaporator device are cylindrical walls arranged coaxially with each other and coaxially with the respective tube,
wherein the separating member of each evaporator device extends over the entire length of the cavity and is interrupted circumferentially in a connection zone of the cavity, and
wherein each conduit is in fluid communication at its opposite ends with the inner cavity and the outer cavity, respectively, of the respective evaporator device so as to allow fluid in vapour phase to flow out of the evaporator device and fluid in liquid phase to flow back into the evaporator device, respectively.
2. The system of claim 1 , wherein the separating member of each evaporator device is formed as a tubular element having an axial slit.
3. The system of claim 1 , wherein each conduit is connected to the respective evaporator device at one end in the connection zone of the cavity and at the opposite end along the outer cavity, on the diametrically opposite side to the connection zone.
4. The system of claim 1 , wherein the outer cavity of each evaporator device is in direct fluid communication with the connection zone of the cavity.
5. The system of claim 1 , wherein each evaporator device comprises closure means arranged between the separating member and the outer wall so as to prevent direct fluid communication between the outer cavity and the connection zone of the cavity.