Motor-integrated fluid machine and vertical take-off and landing aircraft
A motor-integrated fan 1 including one or more motors integrated therein comprises: a shaft part 11 which serves as a supporting system disposed at the center of a rotational axis; a rotation part 12 which is a rotating system rotating about the shaft part 11 ; a duct 13 which serves as a supporting system provided on the outer periphery of the shaft part 11 ; and a motor 14 which rotates the rotation part 12 , wherein the rotation part 12 comprises: a plurality of blades 32 rotatably supported at least on the shaft part 11 and rotating thereabout, the blades 32 being arranged in a circumferential direction of the rotational axis I; and a rotation support ring 33 connected on one side of each of the blades 32 in a radial direction of the rotational axis, the rotation support ring 33 supporting the plurality of blades 32.
1. A motor-integrated fluid machine in which one or more motors are integrally provided, the motor-integrated fluid machine comprising:
a shaft part at a center of a rotational axis and serving as a first portion of a supporting system;
a rotation part to be rotated about the shaft part and serving as a rotating system;
an outer peripheral part on an outer periphery of the shaft part and serving as a second portion of the supporting system; and
a motor configured to rotate the rotation part,
wherein the rotation part is rotatably supported by at least the shaft part and is rotated by the motor, and the rotation part includes a plurality of blades arranged in a circumferential direction of the rotational axis and a rotation support member connected to one side of each of the plurality of blades in a radial direction of the rotational axis and supporting the plurality of blades,
wherein the outer peripheral part is a duct formed in an annular shape and configured to generate a thrust due to the rotation of the rotation part,
wherein the duct includes an upstream portion on an inflow side into which fluid flows, a downstream portion on an outflow side out of which the fluid flows, and a midstream portion between the upstream portion and the downstream portion,
wherein at least an inner peripheral surface of the upstream portion has a predetermined radius of curvature in a cross section taken along a plane orthogonal to the circumferential direction of the rotational axis,
wherein an inner peripheral surface of the midstream portion has a linear portion in the cross section,
wherein an inner peripheral surface of the downstream portion is tapered so as to spread radially from the inflow side toward a downstream side,
wherein an inflow side surface of the rotation part is perpendicular to the axial direction of the rotational axis and forms a plane of rotation, and a relationship between a diameter D of the plane of rotation and the predetermined radius of curvature r is 0.03D≤r≤0.09D,
wherein the inner peripheral surface of the downstream portion is linear in a cross-sectional view viewed from a direction perpendicular to the axial direction of the rotational axis,
wherein the inner peripheral surface of the downstream portion is tapered to form an angle between the inner peripheral surface of the downstream portion and a direction of the inner peripheral surface of the midstream portion in a range of 30° or less,
wherein the motor includes a rotor-side magnet on an outer peripheral side of the rotation support ring in the radial direction and a stator-side magnet on an inner peripheral side of the outer peripheral part and arranged to face the rotor-side magnet, and
wherein opposing surfaces of the rotor-side magnet and the stator-side magnet are perpendicular to the axial direction of the rotational axis.
2. The motor-integrated fluid machine according to claim 1 ,
wherein the motor is an outer periphery drive motor configured to supply power to the rotation part from the outer peripheral part to rotate the rotation part, and
wherein the rotation support member of the rotation part is a rotation support ring having an annular shape centered on the rotational axis and being connected to an outer peripheral side of the plurality of blades in the radial direction of the rotational axis.
3. The motor-integrated fluid machine according to claim 2 , wherein the rotor-side magnet and the stator-side magnet face each other in an axial direction of the rotational axis.
4. The motor-integrated fluid machine according to claim 1 , wherein the rotation part is on an inflow side of the shaft part into which fluid flows in an axial direction of the rotational axis.
5. The motor-integrated fluid machine according to claim 1 , further comprising:
an aerodynamic device on an inner peripheral surface of the duct on an outflow side of the rotation part, the aerodynamic device being configured to suppress separation of fluid flowing along the inner peripheral surface,
wherein the aerodynamic device is on a boundary side of at least the midstream portion at a boundary between the midstream portion and the downstream portion.
6. The motor-integrated fluid machine according to claim 1 , wherein an inflow-side plane formed by inflow-side end portions of the plurality of blades orthogonal to an axial direction of the rotational axis during the rotation of the plurality of blades is positioned at the midstream portion in the axial direction.
7. The motor-integrated fluid machine according to claim 1 , further comprising a rectification plate on an outflow side of the rotation part, the rectification plate connecting the shaft part to the outer peripheral part, and being configured to recitify a flow of fluid flowing from the rotation part.
8. A vertical take-off and landing aircraft comprising:
the motor-integrated fluid machine according to claim 1 ; and
an airframe moved by a thrust generated from the motor-integrated fluid machine.
9. A motor-integrated fluid machine in which one or more motors are integrally provided, the motor-integrated fluid machine comprising:
a shaft part at a center of a rotational axis and serving as a first portion of a supporting system;
a rotation part to be rotated about the shaft part and serving as a rotating system;
an outer peripheral part on an outer periphery of the shaft part and serving as a second portion of the supporting system; and
a motor configured to rotate the rotation part,
wherein the rotation part is rotatably supported by at least the shaft part and is rotated by the motor, and the rotation part includes a plurality of blades arranged in a circumferential direction of the rotational axis and a rotation support member connected to one side of each of the plurality of blades in a radial direction of the rotational axis and supporting the plurality of blades,
wherein the outer peripheral part is a duct formed in an annular shape and configured to generate a thrust due to the rotation of the rotation part,
wherein the duct includes an upstream portion on an inflow side into which fluid flows, a downstream portion on an outflow side out of which the fluid flows, and a midstream portion between the upstream portion and the downstream portion,
wherein at least an inner peripheral surface of the upstream portion has a predetermined radius of curvature in a cross section taken along a plane orthogonal to the circumferential direction of the rotational axis,
wherein an inner peripheral surface of the midstream portion has a linear portion in the cross section,
wherein an inner peripheral surface of the downstream portion is tapered so as to spread radially from the inflow side toward a downstream side
wherein an inflow side surface of the rotation part is perpendicular to the axial direction of the rotational axis and forms a plane of rotation, and a relationship between a diameter D of the plane of rotation and the predetermined radius of curvature r is 0.03D≤r≤0.09D,
wherein the inner peripheral surface of the downstream portion is linear in a cross-sectional view viewed from a direction perpendicular to the axial direction of the rotational axis,
wherein the inner peripheral surface of the downstream portion is tapered to form an angle between the inner peripheral surface of the downstream portion and a direction of the inner peripheral surface of the midstream portion in a range of 30° or less,
wherein the motor-integrated fluid machine further comprises an aerodynamic device on an inner peripheral surface of the duct on an outflow side of the rotation part, the aerodynamic device being configured to suppress separation of fluid flowing along the inner peripheral surface,
wherein the aerodynamic device is on a boundary side of at least the midstream portion at a boundary between the midstream portion and the downstream portion,
wherein the motor-integrated fluid machine further comprises a control unit configured to control the aerodynamic device, and
wherein the control unit is configured to operate the aerodynamic device until the rotation part reaches a predetermined rotation speed.