Method and apparatus for cooling hot gas casings

Claim 2

Apparatus for cooling a hot gas casing of a gas turbine power plant comprising: a combustion chamber enclosing a combustion space; a hot gas casing connected downstream of said combustion chamber; guide means for guiding a stream of cooling air over an outer surface portion of said hot gas casing; a compressor for supplying cooling air to said guide means; a gas turbine which receives hot gas from said combustion chamber, said combustion chamber being fixed with respect to the gas turbine, said compressor and said gas turbine being mounted on a common shaft; said guide means including a shell which is spaced from and encompasses said hot gas casing to form a channel between the casing and the shell, openings in the surface of the shell to permit cooling air to enter said channel, separation means for separating air flowing into the channel from air flowing off the hot gas casing; and said hot gas casing including means for inducing a film cooling of an inner surface portion of said hot gas casing.

Claim 3

Apparatus in accordance with claim 1 wherein said separation means includes: at least one tube which extends through an opening in the surface of the shell to the interior of the air channel; and a perforated surface enclosing a space adjacent to said tube and within said channel.

Claim 4

Apparatus for cooling a hot gas casing of a gas turbine power plant comprising: a combustion chamber enclosing a combustion space; a hot gas casing connected downstream of said combustion chamber; guide means for guiding a stream of cooling air over an outer surface portion of said hot gas casing; a compressor for supplying cooling air to said guide means; a gas turbine which receives hot gas from said combustion chamber, said combustion chamber being fixed with respect to the gas turbine, said compressor and said gas turbine being mounted on a common shaft; said guide means including a shell which is spaced from and encompasses said hot gas casing to form a channel between the casing and the shell, openings in the surface of the shell to permit cooling air to enter said channel; said hot gas casing including means for inducing a film cooling of an inner surface portion of said hot gas casing; a housing enclosing said combustion chamber and forming a primary combustion air inlet passage between the housing and the combustion chamber; an outlet of said channel communicating with the primary air inlet passage; and a flow restrictor arranged between said housing and said hot gas casing at the outlet of said channel.

Claim 5

Apparatus for cooling a hot gas casing of a gas turbine power plant comprising: a combustion chamber enclosing a combustion space; a hot gas casing connected downstream of said combustion chamber; guide means for guiding a stream of cooling air over an outer surface portion of said hot gas casing; a compressor for supplying cooling air to said guide means; a gas turbine which receives hot gas from said combustion chamber, said combustion chamber being fixed with respect to the gas turbine, said compressor and said gas turbine being mounted on a common shaft; said guide means including a shell which is spaced from and encompasses said hot gas casing to form a channel between the casing and the shell, openings in the surface of the shell to permit cooling air to enter said channel; said hot gas casing including means for inducing a film cooling of an inner surface portion of said hot gas casing; a housing enclosing said combustion chamber and forming a primary combustion air inlet passage between the housing and the combustion chamber; an outlet of said channel communicating with the primary air inlet passage; and a flow restrictor arranged between said housing and said hot gas casing at the outlet of said channel.

Claim 6

Apparatus for cooling a hot gas casing of a combustion chamber comprising: a shaft; a compressor mounted on said shaft; a combustion chamber enclosing a combustion space; a housing enclosing said combustion chamber; a gas turbine, also mounted on said shaft, which receives hot gas from said combustion chamber, said combustion chamber being fixed with respect to said gas turbine; a hot gas casing connected downstream of said combustion chamber, said hot gas casing including means for inducing a film cooling of an inner surface portion of said hot gas casing, said combustion chamber having a primary combustion air inlet through which cooling air supplied by the compressor may enter the combustion space; and guide means for guiding a stream of said cooling air over an outer surface portion of said hot gas casing, said guide means including a shell which is spaced from and encompasses said hot gas casing to form a channel between the casing and the shell, an outlet of said channel, a flow restrictor arranged between said housing and said hot gas casing at the outlet of said channel, openings in the surface of the shell to permit cooling air to enter the interior of said channel, said cooling air being supplied to said air channel through the openings in the surface of the shell, separation means for separating air flowing into the channel from air flowing off the hot gas casing, said separation means including at least one tube which extends through one of the openings in the surface of the shell to the interior of the air channel and a perforated surface enclosing a space adjacent to said tube and within said channel, and at least one additional air inlet through which air flowing out of said channel may enter the combustion space.

Claim 7

Apparatus for cooling a hot gas casing of a combustion chamber comprising: a shaft; a compressor mounted on said shaft; a combustion chamber enclosing a combustion space; a housing enclosing said combustion chamber; a gas turbine, also mounted on said shaft, which receives hot gas from said combustion chamber, said combustion chamber being fixed with respect to said gas turbine; a hot gas casing connected downstream of said combustion chamber, said hot gas casing including means for inducing a film cooling of an inner surface portion of said hot gas casing, said combustion chamber having a primary combustion air inlet through which cooling air supplied by the compressor may enter the combustion space; and guide means for guiding a stream of said cooling air over an outer surface portion of said hot gas casing, said guide means including a shell which is spaced from and encompasses said hot gas casing to form a channel between the casing and the shell, an outlet of said channel, a flow restrictor arranged between said housing and said hot gas casing at the outlet of said channel, openings in the surface of the shell to permit cooling air to enter the interior of said channel, said cooling air being supplied to said air channel through the openings in the surface of the shell, separation means for separating air flowing into the channel from air flowing off the hot gas casing, said separation means including at least one tube which extends through one of the openings in the surface of the shell to the interior of the air channel and a perforated surface enclosing a space adjacent to said tube and within said channel, and at least one additional air inlet through which air flowing out of said channel may enter the combustion space.