Patent Application
20090321608
This application relates generally to gas turbine combustor technology and, more specifically, to a mounting arrangement for the forward end of a transition piece (or duct) that carries hot gases from a combustor to a first stage of the turbine.
The transition piece forward mounting bracket is a component of the turbine combustion system that supports a transition duct (commonly referred to as the “transition piece”), that extends between a combustor liner or casing and a first turbine stage in a can-annular gas turbine combustion configuration. The mounting bracket generally requires replacement after completion of a specified number of hours in operation (e.g., 8000 hours) because high stresses and wear in this area could possibly result in failure of the turbine. There are instances, however, where it would be desirable to increase the service life without significant cost increases.
This invention provides a two-piece forward transition piece mounting bracket assembly wherein one piece of the bracket assembly can be used for a shorter life cycle interval but, when it is desired to extend service life, the second piece of the bracket may be added. In other words, the mounting bracket assembly comprises two discrete components, one of which is useable alone to achieve one specified service life, and both of which are useable in combination to achieve a significantly greater specified service life.
Thus, in accordance with one aspect, the present invention relates to a mounting bracket assembly comprising: a first bracket component having a first pair of laterally spaced securement tabs; a second bracket component having a second pair of laterally spaced securement tabs; wherein the first and second bracket components are engageable with each other such that respective ones of each of the first and second pairs of securement tabs are located adjacent each other and adapted to engage corresponding pairs of recesses in a machine component.
In another aspect, the invention relates to a mounting bracket component for securing one machine component to another machine component, the mounting bracket component comprising a first base portion with a first pair of arms extending upwardly and outwardly from the first base portion, the arms having in-turned edges forming a first set of securement tabs receivable in recesses formed in the other machine component, and the first base portion having a first mounting flange axially projecting from one side of the first base portion.
In still another aspect, the invention relates to a method of securing a transition piece to a combustor casing without welding comprising: providing a first mounting bracket component for attaching the transition piece to a turbine combustor casing, the first mounting bracket formed with a first set of securement tabs; providing a second mounting bracket component that is usable with the first bracket component, the second mounting bracket component formed with a second set of securement tabs; and slidably engaging the transition piece with the first and second mounting bracket components, such that the first and second pairs of securement tabs are received within corresponding axially-aligned recesses provided on the transition piece, thereby permitting the transition piece to grow thermally relative to the first and second mounting bracket components.
The invention will now be described in greater detail in connection with the drawings identified below.
With reference initially to
The first bracket component 12 includes a substantially flat base 16 and a pair of upwardly and outwardly extending arms 18 and 20 extending from opposite ends of the base 16. The arm 18 includes a first angled portion 22 and a second angled portion 24, portion 24 extending at a relatively shallower angle relative to the base 16 than the first angled portion 22. At the remote end of arm 18, there is an axially extending securement tab 26.
Similarly, arm 20 has a first angled portion 28 and a second angled portion 30, along with an axially-extending securement tab 32 at its remote end. Thus, it will be appreciated that arms 18 and 20 are substantial mirror images of one another, and securement tabs 26 and 32 collectively form a first set of securement tabs.
The base portion 16 is also provided with an axially projecting flange or support platform 34 provided with mounting holes 36, 38. The flange or platform 34 is recessed relative to the lower surface of the base 16 but substantially flush with the upper surface thereof.
The second mounting bracket component 14 includes a relatively flat base 40 and pair of curved, mirror-image arms 41, 42 extending outwardly and upwardly from opposite ends of the base. The arms 41, 42 lie laterally outwardly of arms 18, 20, and the outer or remote ends of the arms 41, 42 are formed with inwardly projecting edges that form a second set of securement tabs 44, 46, respectively.
Within the base 40, there is a flange or mounting platform 48 which is recessed relative to the upper surface of the base 40, but flush with the lower surface of the base. The flange or platform 48 is provided with mounting holes 50, 52.
With specific reference to
As best seen in
With reference now to
As indicated earlier, the two piece mounting bracket assembly as described above may be used when an extended life of 24K hours is desired. However, in the event the 8K hours of service life is acceptable, the bracket component 14 may be used alone, with securement tabs 44, 46 located in the radially outer recesses 66 of the H-blocks.
The mounting bracket assembly 10 thus provides a degree of fexibility previously unknown in the support of transition pieces. In addition, elimination of current welding steps result in lower cost and longer life since welds are often a source of crack initiation. It will also be appreciated that the dual-component concept of the described mounting block assembly may be used with other machine components where service life and thermal expansion issues are extant.
While the invention has been described in connection with what is presently considered to be the most practical and preferred embodiment, it is to be understood that the invention is not to be limited to the disclosed embodiment, but on the contrary, is intended to cover various modifications and equivalent arrangements included within the spirit and scope of the appended claims.
