Hydrogen-oxygen gas turbine engine
US-2024026816-A1 · Jan 25, 2024 · US
US9109510B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9109510-B2 |
| Application number | US-201213599651-A |
| Country | US |
| Kind code | B2 |
| Filing date | Aug 30, 2012 |
| Priority date | Feb 27, 2012 |
| Publication date | Aug 18, 2015 |
| Grant date | Aug 18, 2015 |
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Official abstract text for this publication.
A gas turbine according to the present invention includes: a strut which passes through an outer diffuser and an inner diffuser, and connects an exhaust chamber wall and a bearing housing; a strut cover which covers the strut along the extending direction of the strut; a partitioning wall which is arranged between the inside of the inner diffuser in the radial direction and the outside of the bearing housing in the radial direction, of which the upstream side portion is sealed between the bearing housing and the partitioning wall, of which the downstream side portion is sealed between the inner diffuser and the partitioning wall, and in which a strut through-hole through which the strut passes is formed; and a hole seal member which seals a gap between the strut through-hole and the strut.
Opening claim text (preview).
The invention claimed is: 1. A gas turbine comprising: a rotor which rotates around a rotation axis; an exhaust chamber wall which forms a cylindrical shape around the rotation axis; an outer diffuser which forms a cylindrical shape around the rotation axis and is provided along an inner periphery of the exhaust chamber wall; an inner diffuser which forms a cylindrical shape around the rotation axis, is arranged in an inside of the outer diffuser in a radial direction, and f…
Mechanical Engineering · mapped topic
Mechanical Engineering · mapped topic
Mechanical Engineering · mapped topic
Mechanical Engineering · mapped topic
Mechanical Engineering · mapped topic
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