Electric rotor motor
The motor with a semicircular shaft and top-mounted design addresses the issue of slipping and limited maneuverability by enabling independent wing rotation, improving glider control and maneuverability.
Patent Information
- Application Number
- JP2025000496U
- Authority / Receiving Office
- JP · JP
- Patent Type
- Utility models
- Current Assignee / Owner
- Filing Date
- 2025-01-29
- Publication Date
- 2025-08-15
- Estimated Expiration
- 2035-01-29
AI Technical Summary
Conventional motors lack a design that allows the rotating shaft axis to be located above the motor, leading to potential slipping of attached components and limited maneuverability in gliders.
The motor incorporates a semicircular rotating shaft and a top-mounted shaft to enable the motor itself to rotate, allowing it to be installed at the bases of glider wings and rotate them independently for turning and maneuvering.
This design enables gliders to turn and maneuver in the air by rotating the horizontal wings, enhancing control and maneuverability without the need for traditional wing movement.
Smart Images
Figure 0003252387000001_ABST
Abstract
Description
[Technical Field]
[0001] In this invention, a rotating plate CO is attached to a motor M (Fig. 2). The rotating plate CO has a rotating shaft SF2 of the motor M that is half-moon shaped (semicircular) to prevent the rotating plate CO from slipping when it rotates. Furthermore, a motor rotating shaft SF1 is attached to the top of the motor M (Fig. 2) so that the motor M itself can rotate. [Background technology]
[0002] Conventional motors have cylindrical rotating shafts, and there were no motors with the axis of the rotating shaft located above the motor where the motor itself rotates. Summary of the Invention [Problem to be solved by the invention]
[0003] In this invention, the rotating shaft SF2 (Fig. 2) of the motor is semicircular so that the fitted rotating plate CO can rotate without slipping. In addition, the shaft SF1 is attached to the top of the motor so that the motor itself rotates.
[0004] The means for solving the problem is to install a motor M (Fig. 2) at the bases P1 and P2 of the glider's main wings WR and WL (Fig. 1), connect the main wings WR and WL (Fig. 1) to a rotating plate CO, and rotate the motor M left and right.
[0005] For example, to rotate glider A to the left, the motor M (Fig. 2) of the main wing WR rotates the rotating plate COR to RU, LD. Then, for the opposite main wing WL, the motor M rotates the rotating plate COL to UR, DL. By doing so, the wing mechanism becomes as shown in Fig. 4, and glider A rotates to the left TR as shown in Fig. 5 (Fig. 5). Effects of the invention
[0006] In this invention, instead of turning the glider A (Figure 1) left and right by moving the horizontal wings up and down, motors MR and ML are attached to the base of the horizontal wings, and horizontal wings WR and WL are attached, so that the horizontal wings WR and WL themselves are rotated to turn the glider A left and right, allowing the glider A to turn in the air. [Brief explanation of the drawings]
[0007] [Figure 1] Glider perspective view [Figure 2] Motor perspective view [Figure 3] Perspective view of standard left and right main wings [Figure 4] Left turning motor perspective view [Figure 5] Front view of a glider turning left [Figure 6] Perspective view of the motor turning right [Figure 7] Front view of a glider turning right [Figure 8] Front view of a glider ascending [Figure 9] Front view of a glider descending [Figure 10] A perspective view of the motor itself rotating and the main wings retracted into the fuselage [Figure 11] A perspective view of a glider with its wings retracted DETAILED DESCRIPTION OF THE INVENTION
[0008] In Figure 1, the fuselage is equipped with main wings WR and WL, horizontal stabilizers RV and LV, and vertical stabilizers CV. The bottom of the fuselage is also equipped with hooks F and wheels RW and BW.
[0009] Motor M is attached to P1 and P2, which are the bases of the fuselage glider A of the main wings WR and WL.
[0010] 2, the motor M has a rotating plate CO fitted with a semicircular motor shaft SF2. Furthermore, a shaft SF1 is provided and received on the upper part of the motor M so that the motor M itself can rotate.
[0011] Referring to Figure 3, the right wing is made up of two parts. First, it is joined to the motor rotating plate COR. The wing WR is structured so that WR1 of wing 1 and WR2 of wing 2 can be deformed. When the wing is deformed, the retracted section HR is retracted (HR) when WR2 of wing 2 is folded in. The left wing is made up of two parts. First, it is joined to the motor rotating plate COL. The WL wing is structured so that WL1 of wing 1 and WL2 of wing 2 can be deformed. When the wing is deformed, the retracted section HL is retracted (HL) when WR2 of wing 2 is folded in.
[0012] Referring to Figure 4, the right wing is made up of two parts. First, it is joined to the rotating plate COR of the motor. The wing WR is structured so that WR1 of wing 1 and WR2 of wing 2 can deform. When the wing is deformed, the retracted part HR is retracted (HR) when WR2 of wing 2 is folded in. Then, the rotating part COR rotates to the RU and LD of the motor MR (Figure 2). The left wing is made up of two parts. First, it is joined to the motor rotating plate COL. The WL wing is structured so that WL1 of wing 1 and WL2 of wing 2 can be deformed. When the wing is deformed, the retracted section HL is retracted (HL) when WR2 of wing 2 is folded in. Then, the rotating part COL rotates in the UR and DL directions of the motor ML (Figure 2).
[0013] In Figure 5, there is a control stick inside the cockpit C, and when the glider turns right, the main axis is tilted UL (Figure 1) around the axis P1 of the main wing, and DR around the axis P2 of the main wing (Figure 5). By doing so, the right wing WR and the left wing WL tilt, and the glider turns right TR (Figure 5).
[0014] Referring to Figure 6, the right wing is made up of two parts. First, it is joined to the rotating plate COR of the motor. The wing WR is structured so that WR1 of wing 1 and WR2 of wing 2 can deform. When the wing is deformed, the retracted part HR is retracted (HR) when WR2 of wing 2 is folded in. Then, the rotating part COR rotates to the UR and DL of the motor MR (Figure 2). The left wing is made up of two parts. First, it is joined to the motor rotating plate COL. The WL wing is structured so that WL1 of wing 1 and WL2 of wing 2 can be deformed. When the wing is deformed, the retracted section HL is retracted (HL) when WR2 of wing 2 is folded in. Then, the rotating part COL rotates to the RU and LD of the motor ML (Figure 2).
[0015] In Figure 7, there is a control stick inside the cockpit C, and when the glider turns left, the main axis is tilted around the wing axis P1 to DR (Figure 1) and around the wing axis P2 to UL (Figure 7). By doing so, the right wing WR and the left wing WL tilt, and the glider turns right TL (Figure 7).
[0016] In Figure 8, there is a control stick inside the cockpit C, and when the glider ascends, the wings are tilted to UL (Figure 1) around the wing-to-fuselage axis P1, P2. By doing so, the right wing WR and left wing WL tilt, and the glider ascends U (Figure 8).
[0017] In Figure 9, there is a control stick inside the cockpit C, and when the glider descends, the wings are tilted to DL (Figure 1) around the wing-to-body axis P1, P2. By doing so, the right wing WR and left wing WL tilt, and the glider descends D (Figure 8).
[0018] Referring to Figure 10, the left motor ML and the right motor MR are rotated around the left shaft axis LSF1 and the right shaft axis RSF1 to fold the main wings WL and WR (Figure 10).
[0019] In Figure 11, the main wings WL and WR are completely folded. The motors ML and MR, whose shaft rotation axes LSF1 and RSF1 are inside the glider A, are inside the glider A and cannot be seen from the outside.
[0020] As such, the above-described embodiments are merely illustrative in all respects and should not be construed as limiting. Furthermore, all forms and modifications within the scope of the equivalents of the utility model registration claims are within the scope of the present invention. [Industrial Applicability]
[0021] Compared to ordinary motors, this invention has a semicircular motor shaft with a rotating shaft at the top of the motor, making it industrially applicable as a motor specifically for gliders. [Explanation of symbols]
[0022] A. Torso C Cockpit F hook FB Hook Base RW Front right wheel LW Front left wheel BW rear wheel WR1 First Right Wing WR2 Second right wing WL1 First left wing WL2 Second left wing BM power source CV vertical stabilizer RV right horizontal stabilizer LV left horizontal stabilizer HR right wing well HL left wing well HAR right fuselage compartment P1 Right wing-fuselage axis P2 left wing-fuselage axis Medium motor SF1 Motor rotating shaft SF2 Rotating shaft CO rotating plate UR Upper Right Rotation DL Lower Left Rotation RU Right upper rotation LD Lower Left Rotation ROL motor rotation range LSF1 Left motor rotating shaft ML Left Motor COL Left Rotating Plate RSF1 Right motor rotating shaft MR right motor COR Right Rotating Plate
Claims
1. In the drive unit, The rotation axis of the drive unit is semicircular. Rotating Electric Equipment
2. In the drive unit, A rotating plate is attached to the semicircular rotation axis of the drive unit. Rotating Electric Equipment
3. In the drive unit, A rotating shaft is provided on the top of the drive unit. The rotary electric motor according to claims 1 and 2