Ring gear for an aircraft mechanical gearbox
A ring gear for an aircraft mechanical gearbox, the ring gear having an annular shape about an axis and having an internal toothing at its internal periphery, an external annular flange or splines at its external periphery, and an annular web extending between the internal toothing and the external flange or splines. The web can include an annular row of arms which are distributed about the axis, these arms connecting the internal toothing to the external flange or splines and being formed in a single piece with the internal toothing and the external flange or splines.
1. A ring gear for an aircraft mechanical gearbox, the ring gear having an annular shape about an axis and comprising:
an internal toothing at its internal periphery;
an external annular flange or splines at its external periphery; and
an annular web extending between the internal toothing and the external flange or splines,
wherein the web includes an annular row of arms which are distributed around the axis, the arms connecting the internal toothing to the external flange or splines and being formed in a single piece with the internal toothing and the external flange or splines.
2. The ring gear of claim 1 , wherein the arms are separated from one another by spaces, or delimit spaces between them.
3. The ring gear of claim 2 , wherein each of or at least a portion of the spaces is generally parallelepipedal, trapezoidal, triangular, or diamond-shaped.
4. The ring gear of claim 2 , wherein the spaces are formed by circular or oblong orifices.
5. The ring gear of claim 4 , wherein the web has a first annular row of orifices located on a first circumference, and a second annular row of orifices located on a second circumference whose diameter is greater than that of the first circumference, the orifices of the first row being located circumferentially between the orifices of the second row.
6. The ring gear of claim 2 , wherein the spaces are empty.
7. The ring gear of claim 2 , wherein the spaces are filled by blocks made of a material different from the main material of the ring gear.
8. The ring gear of claim 7 , wherein the blocks are made of a polymer material.
9. The ring gear of claim 1 , wherein the arms are inclined obliquely to a radial direction and have an inclination orientation in the same circumferential direction.
10. The ring gear of claim 1 , wherein a first series of the arms is oriented in a first way, and a second series of the arms is oriented in a second way different from the first way.
11. The ring gear as claimed in claim 10 , wherein the arms of the first series are intertwined with the arms of the second series.
12. The ring gear of claim 1 , wherein the arms are all located in the same plane perpendicular to the axis.
13. The ring gear of claim 1 , wherein the number of arms is greater than 2, greater than 5 or 10, greater than 20, or between 20 and 100.
14. The ring gear of claim 1 , wherein the arms are all oriented in the same way, and in particular they are all inclined with respect to the radii of the axis.
15. A mechanical gearbox for an aircraft, the gearbox comprising:
a sun gear movable in rotation about an axis;
a ring gear according to claim 1 mounted around the sun gear and the axis; and
planet gears mounted between the sun gear and the ring gear and meshed with the sun gear and the ring gear, the planet gears having axes of rotation parallel to the axis.
16. A turbomachine for an aircraft having at least one ring gear according to claim 1 .
17. A turbomachine for an aircraft having at least one mechanical gearbox according to claim 15 .
18. A drive system for driving a wheel of a landing gear of an aircraft, the drive system having at least one ring gear according to claim 1 .
19. A drive system for driving a wheel of a landing gear of an aircraft, the drive system having at least one mechanical gearbox according to claim 15 .