Modularity of an aircraft turbomachine
US-2024003303-A1 · Jan 4, 2024 · US
US2016252136A1 · US · A1
| Field | Value |
|---|---|
| Publication number | US-2016252136-A1 |
| Application number | US-201615151744-A |
| Country | US |
| Kind code | A1 |
| Filing date | May 11, 2016 |
| Priority date | Feb 14, 2014 |
| Publication date | Sep 1, 2016 |
| Grant date | — |
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Official abstract text for this publication.
A device for transmitting a torque between an internal combustion engine and a generator has a motor-side shaft, a generator-side shaft, a separate transmission element for transmitting the torque between the two shafts, and a seal device. The motor-side shaft and the generator-side shaft are situated in each case substantially coaxially with respect to one another and are in each case connected by way of a shaft-hub connection to the transmission element, wherein a lubricant chamber which is situated radially outside the transmission element and between the motor-side shaft and the generator-side shaft and which couples the two shaft-hub connections with regard to a flow of lubricant is sealed off with respect to the outside by the seal device.
Opening claim text (preview).
What is claimed is: 1 . A device for transmitting a torque between an internal combustion engine and a generator, the device comprising: a motor-side shaft; a generator-side shaft; a separate transmission element that transmits torque between the motor-side shaft and the generator-side shaft, wherein the motor-side shaft and the generator-side shaft are arranged substantially coaxially with respect to one another and are connected in each case via a shaft/hub connection to the separate transmission element; a lubricant chamber is formed radially outside the transmission element between the motor-side shaft and the generator-side shaft, the lubricant chat b coupling the two shaft/hub connections in terms of lubricant flow; and a seal device configured to externally seal-off the lubricant chamber. 2 . The device according to claim 1 , further comprising: at least one lubricant intake provided in one of the motor-side shaft and the generator-side shaft. 3 . The device according to claim 2 , wherein at least one lubricant intake is provided in the motor-side shaft. 4 . The device according to claim 1 , wherein the lubricant chamber is fluidically connected to a lubricant circuit of the internal combustion engine. 5 . The device according to claim 1 , wherein: the seal device has a seal element, at one axial end of the seal element, the seal element overlaps with a tubular seal extension on one of the motor-side shaft and the generator-sides shaft, and the one axial end of the seal element bears against the tubular seal extension. 6 . The device according to claim 5 , wherein: the axial end of the seal element has a conical seat surface that overlaps with the seal extension, and the seal extension has a complementary conical counter-surface that contacts the conical seal surface. 7 . The device according to claim 1 , wherein: at least one of the motor-side shaft and the generator-side shaft has an axially projecting tubular shell part that extends around the transmission element and delimits the lubricant chamber radially outwardly at least in portions. 8 . The device according to claim 5 , wherein: at least one of the motor-side shaft and the generator-side shaft has an axially projecting tubular shell part that extends around the transmission element and delimits the lubricant chamber radially outwardly at least in portions. 9 . The device according to claim 7 , wherein: the tubular shell part is configured integrally with the generator-side shaft, and the seal element bears against and is guided on a radially inner surface of the tubular shell part. 10 . The device according to claim 8 , wherein the tubular shell part and the tubular seal extension overlap one another. 11 . The device according to claim 1 , wherein the seal device comprises a seal element axially tensioned between the motor-side shaft and the generator-side shaft. 12 . The device according to claim 1 , wherein the seal device comprises a spring supported on one of the motor-side shaft and the generator-side shaft, the spring pressing a seal element against the other one of the motor-side shaft and the generator-side shaft. 13 . The device according to claim 5 , wherein: the seal device has a spring supported on e of the motor-side shaft and the generator-side shaft that does not have a tubular seal extension, and the spring is configured to press the seal element with a force against the tubular seal extension on the other one of the motor-side shaft and the generator-side shaft. 14 . The device according to claim 5 , wherein the seal element is configured as a sleeve or an O-ring. 15 . The device according to claim 1 , wherein: at least one of the motor-side shaft or the generator-side shaft is configured as a hollow shaft having a torque transmission profile, the at least one of the two shafts being connected in a positive-locking manner to a complementary profile on the transmission element. 16 . The device according to claim 15 , wherein the torque transmission profile is a toothed profile.
for connecting two abutting shafts or the like · CPC title
Spline connection · CPC title
Details or arrangements of sealings not provided for in group F16D3/84 · CPC title
Lubrication details not provided for in group F16D13/74 · CPC title
Couplings for rigidly connecting two coaxial shafts or other movable machine elements (attachment of wheels to axles for railway carriages B60B; for attachment of cranks to their shafts F16C3/10) · CPC title
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