Combustion air flow rate adjusting device for gas turbine combustor

Claim 2

A combustion air flow rate generating device for a gas turbine, in which a cylindrical regulating ring fitted about an outer peripheral surface of an inner cylinder of a gas turbine combustor is translated along the outer peripheral surface of the inner cylinder to vary an opening area of air intake ports formed in said inner cylinder, thereby adjusting the combustion air flow rate, wherein an arcuately moving part at a forward end of a driving lever and a part linearly reciprocating together with said regulating ring are connected to each other by oppositely directed leaf spring-like members.

Claim 3

A combustion air flow rate adjusting device as defined in claim 1, characterized in that said leaf spring-like members are arranged in at least two in side by side relation widthwise thereof such that tension force is always applied to said leaf spring-like members during the linear reciprocating motion of said regulating ring.

Claim 4

A combustion air flow rate adjusting device as defined in claim 1, characterized in that said leaf spring-like members are arranged in plural in superposed relation in a thickness direction of said leaf spring-like members.

Claim 5

A combustion air flow rate adjusting device as defined in claim 1, characterized in that a columnar surface is formed on said arcuately moving part at the forward end of said driving lever, along the arc, and portions of the respective leaf spring-like members adjacent their respective one ends are attached in contact with said columnar surface.

Claim 6

A combustion air flow rate adjusting device as defined in claim 1, characterized in that said leaf spring-like members are interposed and connected under tension between said arcuately moving part at the forward end of said driving lever and said part linearly reciprocating together with said regulating ring.

Claim 7

A combustion air flow rate adjusting device for a gas turbine, in which a cylindrical regulating ring fitted about an outer peripheral surface of an inner cylinder of a gas turbine combustor is translated along the outer peripheral surface of the inner cylinder to vary an opening area of air intake ports formed in said inner cylinder, thereby adjusting the combustion air flow rate, wherein an arcuately moving part at a forward end of a driving lever and a part linearly reciprocating together with said regulating ring are connected to each other by leaf spring-like members, said arcuately moving part at the forward end of said driving lever is provided with a first engaging portion, and said part linearly reciprocating together with said regulating ring is provided with a second engaging portion, said first and second engaging portions being brought into engagement with each other only when said leaf spring-like members are broken, and said first and second engaging portions being maintained in disengagement from each other when said leaf spring-like members function normally.

Claim 8

A combustion air flow rate adjusting device for a gas turbine, in which a cylindrical regulating ring fitted about an outer peripheral surface of an inner cylinder of a gas turbine combustor is translated along the outer peripheral surface of the inner cylinder to vary an opening area of air intake ports formed in said inner cylinder, thereby adjusting the combustion air flow rate, wherein an arcuately moving part at a forward end of a driving lever and a part linearly reciprocating together with said regulating ring are connected to each other by leaf spring-like members, said arcuately moving part at the forward end of said driving lever is provided with a first engaging portion, and said part linearly reciprocating together with said regulating ring is provided with a second engaging portion, said first and second engaging portions being brought into engagement with each other only when said leaf spring-like members are broken, and said first and second engaging portions being maintained in disengagement from each other when said leaf spring-like members function normally.

Claim 9

A combustion air flow rate adjusting device for a gas turbine combustor comprising an inner cylinder, an outer cylinder surrounding said inner cylinder, first stage fuel nozzles arranged at a front side of said inner cylinder, second stage fuel nozzles arranged adjacent an intermediate portion of said inner cylinder, and air intake ports for air to be premixed with fuel from said second fuel nozzles, said combustion air flow rate adjusting device comprising: a regulating ring located outwardly of said air intake ports and arranged so as to surround said inner cylinder, said regulating ring being surrounded by said outer cylinder, said regulating ring being capable of being translated along an outer peripheral surface of said inner cylinder to vary an opening area of said air intake ports; a shaft extending through a peripheral wall of said outer cylinder; a lever located between said inner and outer cylinders and fixedly connected to said shaft; and oppositely directed leaf springs connected between a forward end of said lever and said regulating ring.

Claim 10

A combustion air flow rate adjusting device for a gas turbine combustor comprising an inner cylinder, an outer cylinder surrounding said inner cylinder, first stage fuel nozzles arranged at a front side of said inner cylinder, second stage fuel nozzles arranged adjacent an intermediate portion of said inner cylinder, and air intake ports for air to be premixed with fuel from said second fuel nozzles, said combustion air flow rate adjusting device comprising: a regulating ring located outwardly of said air intake ports and arranged so as to surround said inner cylinder, said regulating ring being surrounded by said outer cylinder, said regulating ring being capable of being translated along an outer peripheral surface of said inner cylinder to vary an opening area of said air intake ports; a shaft extending through a peripheral wall of said outer cylinder; a lever located between said inner and outer cylinders and fixedly connected to said shaft; and oppositely directed leaf springs connected between a forward end of said lever and said regulating ring.

Claim 11

A combustion air flow rate adjusting device as defined in claim 7, wherein said lever has an end formed into a columnar surface, and said leaf springs have their respective one ends fixedly connected to said lever, said leaf springs extending along said columnar surface and extending tangentially thereto, the respective other ends of said leaf springs being fixedly connected to said regulating ring.

Claim 12

In a gas turbine combustor comprising an inner cylinder defining therein a combustion chamber, fuel nozzles for supplying fuel into said inner cylinder, and air intake ports through which combustion air is introduced into said inner cylinder, a combustion air flow rate adjusting device comprising regulating means for varying an opening area of said air intake ports, guide means for guiding linear reciprocating motion of said regulating means, and driving means for reciprocally driving said regulating means, said driving means including a shaft, a lever angularly moving about an axis of said shaft, and oppositely directed resilient strip-like members connecting an end of said lever and said regulating means to each other.

Claim 13

In a gas turbine combustor comprising an inner cylinder defining therein a combustion chamber, fuel nozzles for supplying fuel into said inner cylinder, and air intake ports through which combustion air is introduced into said inner cylinder, a combustion air flow rate adjusting device comprising regulating means for varying an opening area of said air intake ports, guide means for guiding linear reciprocating motion of said regulating means, and driving means for reciprocally driving said regulating means, said driving means including a shaft, a lever angularly moving about an axis of said shaft, and oppositely directed resilient strip-like members connecting an end of said lever and said regulating means to each other.

Claim 14

A combustion air flow rate adjusting device as defined in claim 9 for the gas turbine combustor further comprising an outer cylinder surrounding said inner cylinder, wherein said regulating means, said resilient strip-like members and said lever are arranged in a space defined between said inner and outer cylinders.

Claim 15

A combustion air flow rate adjusting device as defined in claim 9, wherein said lever has a free end formed to have a columnar surface, and said resilient strip-like members have their respective one ends fixedly connected to said free end of said lever, said resilient strip-like members extending along said columnar surface and extending tangentially thereto, the respective other ends of said resilient strip-like members being fixedly connected to said regulating means.

Claim 16

A combustion air flow rate adjusting device as defined in claim 9, wherein said air intake ports are arranged in plural circumferentially of a wall surface of said inner cylinder, and said regulating member is in the form of a ring fitted about an outer peripheral surface of said inner cylinder.

Claim 17

A combustion air flow rate adjusting device for a gas turbine, comprising an inner cylinder, an outer cylinder surrounding said inner cylinder, first stage fuel nozzles arranged at a front side of said inner cylinder, second stage fuel nozzles arranged adjacent an intermediate portion of said inner cylinder, and air intake ports for air to be premixed with fuel from said second fuel nozzles, said combustion air flow rate adjusting device comprising: a regulating ring located outwardly of said air intake ports and arranged so as to surround said inner cylinder, said regulating ring being surrounded by said outer cylinder, said regulating ring being capable of being translated along an outer peripheral surface of said inner cylinder to vary an opening area of said air intake ports; a shaft extending through a peripheral wall of said outer cylinder; a lever located between said inner and outer cylinders and fixedly connected to said shaft, the forward end portion of the lever has a three-dimensionally columnar surface having a radius of curvature equal to a distance from the central axis of the shaft to the outer surface of the forward end portion; and leaf springs connected between a forward end of said lever and said regulating ring, said leaf springs having their respective one ends fixedly connected to said lever, said leaf springs extending along said columnar surface and extending tangentially thereto, the respective other ends of said leaf springs being fixedly connected to said regulating ring.

Claim 18

A combustion air flow rate adjusting device for a gas turbine, comprising an inner cylinder, an outer cylinder surrounding said inner cylinder, first stage fuel nozzles arranged at a front side of said inner cylinder, second stage fuel nozzles arranged adjacent an intermediate portion of said inner cylinder, and air intake ports for air to be premixed with fuel from said second fuel nozzles, said combustion air flow rate adjusting device comprising: a regulating ring located outwardly of said air intake ports and arranged so as to surround said inner cylinder, said regulating ring being surrounded by said outer cylinder, said regulating ring being capable of being translated along an outer peripheral surface of said inner cylinder to vary an opening area of said air intake ports; a shaft extending through a peripheral wall of said outer cylinder; a lever located between said inner and outer cylinders and fixedly connected to said shaft, the forward end portion of the lever has a three-dimensionally columnar surface having a radius of curvature equal to a distance from the central axis of the shaft to the outer surface of the forward end portion; and leaf springs connected between a forward end of said lever and said regulating ring, said leaf springs having their respective one ends fixedly connected to said lever, said leaf springs extending along said columnar surface and extending tangentially thereto, the respective other ends of said leaf springs being fixedly connected to said regulating ring.

Claim 19

A combustion air flow rate adjusting device according to claim 13, wherein the leaf springs are oppositely directed at the forward end of said lever.