Heat removal structure of aircraft main landing gear bay

1. A heat removal structure of an aircraft main landing gear bay comprising:

a fairing which covers a lower part of a fuselage having a main landing gear bay formed therein into which a main landing gear having a wheel is retracted, and defines a ventilation cavity communicating with the main landing gear bay between the fairing and the main landing gear bay; and

a heat removal system which removes heat generated from the main landing gear retracted inside the main landing gear bay to the outside of the main landing gear bay by suctioning/discharging air through an inlet port and an outlet port leading to external air, wherein

the fairing defines a wheel opening through which the wheel of the main landing gear enters and exits, and defines a lower ventilation port which functions as one of the inlet port and the outlet port, the lower ventilation port defined by a space between the fairing and an outer peripheral part of the wheel which is exposed from the wheel opening to the lower side of the main landing gear bay when the main landing gear is retracted; and

the outlet port is located in a position different from a position where the inlet port is located.

2. The heat removal structure of an aircraft main landing gear bay according to claim 1 , wherein the inlet port is located closer to a nose of the aircraft than the wheel opening, and the lower ventilation port, which functions as the outlet port, is located closer to an empennage side of the aircraft than the inlet port.

3. The heat removal structure of an aircraft main landing gear bay according to claim 2 , wherein the fairing defines the inlet port in a front end part of the fairing or in the vicinity thereof.

4. The heat removal structure of an aircraft main landing gear bay according to claim 2 , wherein the inlet port is depressed from a surface of the fairing and has an opening cross-sectional area that increases from an inlet of the inlet port to an outlet of the inlet port.

5. The heat removal structure of an aircraft main landing gear bay according to claim 1 , further comprising a main landing gear door which covers an opening part of a wing bay which is a region of the main landing gear bay formed in a main wing, and opens as the main landing gear is deployed, wherein the main landing gear door defines a ventilation port which pairs with the lower ventilation port and functions as one of the inlet port and the outlet port.

6. The heat removal structure of an aircraft main landing gear bay according to claim 5 , wherein the ventilation port is depressed from a surface of the main landing gear door and has an opening cross-sectional area that increases from an inlet of the ventilation port to an outlet of the ventilation port.

7. The heat removal structure of an aircraft main landing gear bay according to claim 1 , further comprising a shutter which can open/close at least one of the inlet port and the outlet port.

8. The heat removal structure of an aircraft main landing gear bay according to claim 7 , further comprising:

a driving unit which drives the shutter;

a temperature sensor which detects the temperature around the retracted main landing gear; and

a controller which sends a control signal for operation of the shutter to the driving unit on the basis of the temperature detected by the temperature sensor.

9. An aircraft comprising the heat removal structure of a main landing gear bay according to claim 1 .