Piston seal ring
A gas turbine having a device and a further device is provided. The device includes an outer casing, an inner casing and a seal ring. The outer casing and the inner casing are arranged in such a way that a cooling duct is formed between each other. The seal ring is arranged between the outer casing and the inner casing in such a way that the seal ring seals the cooling duct from an environment surrounding the outer casing. The device and the further device are mounted together such that working fluid is flowable from the further device to the device. Furthermore the device includes a rotatable shaft and the further device includes a further rotatable shaft, wherein the rotatable shaft and the further rotatable shaft are mechanically decoupled from each other, and wherein the seal ring exclusively abuts against the inner casing and against the outer casing of the device.
1. A gas turbine comprising
a device,
wherein the device comprises an outer casing, an inner casing and a seal ring,
wherein the outer casing and the inner casing are arranged in such a way that a cooling duct is formed between each other, and
wherein the seal ring is arranged between the outer casing and the inner casing in such a way that the seal ring seals the cooling duct from an environment surrounding the outer casing, and
a further device,
wherein the device and the further device are mounted together such that working fluid is flowable from the further device to the device,
wherein the device comprises a rotatable shaft and wherein the further device comprises a further rotatable shaft,
wherein the rotatable shaft and the further rotatable shaft are mechanically decoupled from each other, and
wherein the seal ring exclusively abuts against the inner casing and against the outer casing of the device.
2. The gas turbine according to claim 1 ,
wherein the seal ring is arranged between the outer casing and the inner casing in such a way that that the seal ring is partially visible from the environment surrounding the outer casing.
3. The gas turbine according to claim 1 ,
wherein the seal ring is an in-springing ring which is clamped to the inner casing such that clamping forces of the in-springing ring are transmitted to the inner casing.
4. The gas turbine according to claim 1 , wherein the seal ring is an out-springing ring which is clamped to the outer casing such that clamping forces of the out-springing ring are transmitted to the outer casing.
5. The gas turbine according to claim 1 , wherein the device comprises a power turbine, and wherein the further device comprises a gas generator.
6. The gas turbine according to claim 1 , wherein the device comprises an inner volume (Vi) surrounded by the inner casing, wherein a working fluid steams through the inner volume (Vi),
wherein the further device comprises a further inner casing and a further outer casing,
wherein the device and the further device are mounted together in such a way that a cavity between the device and the further device is formed,
wherein the cavity is surrounded by the inner casing, the further inner casing, the outer casing and the further outer casing,
wherein the cavity is connected to the inner volume (Vi).
7. A method of manufacturing a device for a gas turbine, the method comprising
forming a cooling duct between an outer casing of the device and an inner casing of the device,
arranging a seal ring between the outer casing and the inner casing in such a way that the seal ring seals the cooling duct from an environment surrounding the outer casing,
mounting the device and a further device together such that working fluid is flowable from the further device to the device,
wherein the device comprises a rotatable shaft and wherein the further device comprises a further rotatable shaft,
wherein the rotatable shaft and the further rotatable shaft are mechanically decoupled from each other, and
wherein the seal ring exclusively abuts against the inner casing and against the outer casing of the device.