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公开(公告)号:US10106255B2
公开(公告)日:2018-10-23
申请号:US14712218
申请日:2015-05-14
摘要: A tiltrotor aircraft can include a pylon rotatable about a conversion axis. A first differential planetary assembly can include a first housing; a first ring gear; a first differential planetary gear having a first output portion; and a first differential sun gear. A second differential planetary assembly can include a second housing; a second ring gear; a second differential planetary gear having a second output portion; and a second differential sun gear. The first output portion is coupled to the second housing such that the second housing rotates at a first output speed. Further, the second output portion is coupled to the shaft, the shaft being coupled to the pylon such that rotation of the shaft rotates the pylon.
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公开(公告)号:US10816085B2
公开(公告)日:2020-10-27
申请号:US15874054
申请日:2018-01-18
发明人: Eric S. Olson , David R. Bockmiller
摘要: A system is provided in one example embodiment and may include a first reservoir for a lubricant; a second reservoir for the lubricant, wherein the first reservoir and the second reservoir are interconnected; a first pumping element to pump the lubricant from the first reservoir at a first flow rate; a second pumping element to pump the lubricant at a second flow rate, wherein the first flow rate and the second flow rate are different; and a gearbox coupled to the first pumping element and the second pumping element. The first reservoir may have a larger volume than the second reservoir and the first flow rate may be higher than the second flow rate.
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公开(公告)号:US20190219149A1
公开(公告)日:2019-07-18
申请号:US15874054
申请日:2018-01-18
发明人: Eric S. Olson , David R. Bockmiller
CPC分类号: F16H57/0442 , B64C27/04 , B64C27/32 , B64C29/0033 , B64C29/0091 , B64D35/00 , F16H57/0441 , F16H57/0449 , F16H57/045
摘要: A system is provided in one example embodiment and may include a first reservoir for a lubricant; a second reservoir for the lubricant, wherein the first reservoir and the second reservoir are interconnected; a first pumping element to pump the lubricant from the first reservoir at a first flow rate; a second pumping element to pump the lubricant at a second flow rate, wherein the first flow rate and the second flow rate are different; and a gearbox coupled to the first pumping element and the second pumping element. The first reservoir may have a larger volume than the second reservoir and the first flow rate may be higher than the second flow rate.
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公开(公告)号:US20150360774A1
公开(公告)日:2015-12-17
申请号:US14712218
申请日:2015-05-14
IPC分类号: B64C27/52
摘要: A tiltrotor aircraft can include a pylon rotatable about a conversion axis. A first differential planetary assembly can include a first housing; a first ring gear; a first differential planetary gear having a first output portion; and a first differential sun gear. A second differential planetary assembly can include a second housing; a second ring gear; a second differential planetary gear having a second output portion; and a second differential sun gear. The first output portion is coupled to the second housing such that the second housing rotates at a first output speed. Further, the second output portion is coupled to the shaft, the shaft being coupled to the pylon such that rotation of the shaft rotates the pylon.
摘要翻译: 倾斜旋翼飞机可以包括可围绕转换轴线旋转的挂架。 第一差速行星组件可以包括第一壳体; 第一个齿圈; 第一差速行星齿轮,具有第一输出部分; 和第一差速器太阳齿轮。 第二差速行星组件可包括第二壳体; 第二个齿圈; 具有第二输出部分的第二差速行星齿轮; 和第二差速器太阳齿轮。 第一输出部分联接到第二壳体,使得第二壳体以第一输出速度旋转。 此外,第二输出部分联接到轴,轴联接到塔架,使得轴的旋转使塔架旋转。
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