Flying apparatus
A flying apparatus 10 includes an airframe base 14 ; a power supply unit; an arm 11 which extends from the airframe base 14 toward a periphery; a rotor 12 which is disposed on an end portion side of the arm 11 ; a motor 17 which rotationally drives the rotor 12 ; and a power converting unit 19 which converts electric power supplied from the power supply unit to the motor 17 . The power converting unit 19 is included inside the arm 11 below a rotation range 24 of the rotor 12 . The power converting unit 19 can be effectively cooled by downwash generated by the rotation of the rotor 12.
1 . A flying apparatus comprising:
an airframe base;
a power supply unit;
an arm which extends from the airframe base toward a periphery;
a rotor which is disposed on an end portion side of the arm;
a motor which rotationally drives the rotor; and
a power converting unit which converts electric power supplied from the power supply unit to the motor, wherein
the power converting unit is included inside the arm below a rotation range of the rotor,
the arm has a substantially tubular shape which extends toward the periphery,
the power converting unit is in contact with an inner surface of the arm, and
a portion with which the power converting unit is in contact in the inner surface of the arm is a flat surface.
2 . The flying apparatus according to claim 1 , wherein
the arm includes an internal space which extends along an axial direction, and
the power converting unit is housed in the internal space.
3 . The flying apparatus according to claim 1 , wherein
the power supply unit includes a power generator which generates an alternating-current power, and
the power converting unit includes: a converter unit which converts the alternating-current power to a direct-current power; and an inverter unit which converts the direct-current power to the alternating-current power having a predetermined frequency.
4 . The flying apparatus according to claim 1 , wherein a portion of the arm with which the power converting unit is in contact is thicker than another portion of the arm.
5 . The flying apparatus according to claim 1 , wherein
the arm includes an upper thin portion, a lower thin portion, and a thick portion provided between the upper thin portion and the lower thin portion, and
the power converting unit is disposed to be in contact with an inner surface of the thick portion.
6 . The flying apparatus according to claim 1 , further comprising a lower protruding portion which is formed by causing a lower end side of the arm to continuously protrude upward.
7 . The flying apparatus according to claim 1 , further comprising an upper protruding portion which is formed by causing an upper end side of the arm to continuously protrude downward.
8 . The flying apparatus according to claim 1 , wherein
a distance between an outer end portion of the power converting unit and a portion in which the airframe base is connected to the arm is ⅔ or less of a length of the arm.
9 . The flying apparatus according to claim 1 , wherein
the rotor includes an upper rotor and a lower rotor,
the power converting unit includes a plurality of power converting units provided to correspond to the upper rotor and the lower rotor, and
all the power converting units are incorporated in the arm.
10 . The flying apparatus according to claim 1 , wherein
the power converting unit includes a plurality of power converting units disposed away from each other below the rotation range of the rotor.
11 . The flying apparatus according to claim 1 , wherein the arm is formed of an extruded or pultruded metal.
12 . A flying apparatus comprising:
an airframe base;
a power supply unit;
an arm which extends from the airframe base toward a periphery and which has a substantially tubular shape;
a rotor which is disposed on an end portion side of the arm;
a motor which rotationally drives the rotor; and
a power converting unit which converts electric power supplied from the power supply unit to the motor, wherein
the power converting unit is included inside the arm below a rotation range of the rotor,
the arm includes:
an upper thin portion which is an upper portion of the substantially tubular shape;
a lower thin portion which is a lower portion of the substantially tubular shape; and
a thick portion which is provided between the upper thin portion and the lower thin portion, which is formed to be flatter than the upper thin portion and the lower thin portion, and which is thicker than the upper thin portion and the lower thin portion, and
the power converting unit is disposed inside the arm to be in surface-contact with an inner surface of the thick portion.
13 . A flying apparatus comprising:
an airframe base;
a power supply unit;
an arm which extends from the airframe base toward a periphery;
a rotor which is disposed on an end portion side of the arm;
a motor which rotationally drives the rotor; and
a power converting unit which converts electric power supplied from the power supply unit to the motor, wherein
the power converting unit is included inside the arm below a rotation range of the rotor, wherein
the power supply unit includes a power generator which generates an alternating-current power, and
the power converting unit includes: a converter unit which converts the alternating-current power to a direct-current power; and an inverter unit which converts the direct-current power to the alternating-current power having a predetermined frequency.
14 . A flying apparatus comprising:
an airframe base;
a power supply unit;
an arm which extends from the airframe base toward a periphery;
a rotor which is disposed on an end portion side of the arm;
a motor which rotationally drives the rotor; and
a power converting unit which converts electric power supplied from the power supply unit to the motor, wherein
the power converting unit is included inside the arm below a rotation range of the rotor, wherein a portion of the arm with which the power converting unit is in contact is thicker than another portion of the arm.
15 . A flying apparatus comprising:
an airframe base;
a power supply unit;
an arm which extends from the airframe base toward a periphery;
a rotor which is disposed on an end portion side of the arm;
a motor which rotationally drives the rotor; and
a power converting unit which converts electric power supplied from the power supply unit to the motor, wherein
the power converting unit is included inside the arm below a rotation range of the rotor, wherein
the arm includes an upper thin portion, a lower thin portion, and a thick portion provided between the upper thin portion and the lower thin portion, and
the power converting unit is disposed to be in contact with an inner surface of the thick portion.
16 . A flying apparatus comprising:
an airframe base;
a power supply unit;
an arm which extends from the airframe base toward a periphery;
a rotor which is disposed on an end portion side of the arm;
a motor which rotationally drives the rotor; and
a power converting unit which converts electric power supplied from the power supply unit to the motor, wherein
the power converting unit is included inside the arm below a rotation range of the rotor, wherein
a distance between an outer end portion of the power converting unit and a portion in which the airframe base is connected to the arm is ⅔ or less of a length of the arm.
17 . A flying apparatus comprising:
an airframe base;
a power supply unit;
an arm which extends from the airframe base toward a periphery;
a rotor which is disposed on an end portion side of the arm;
a motor which rotationally drives the rotor; and
a power converting unit which converts electric power supplied from the power supply unit to the motor, wherein
the power converting unit is included inside the arm below a rotation range of the rotor, wherein
the arm has a substantially tubular shape which extends toward the periphery,
the power converting unit is in contact with an inner surface of the arm, and
the power converting unit is disposed inside the arm to be in surface-contact with the inner surface of the arm.