TURBINE BLADE TRACK ASSEMBLY(10)
时间:2020-08-31 01:38 来源:网络整理 作者:bosi 点击:次
Yet another aspect of the present disclosure includes a gas turbine engine comprising a turbine section having at least one turbine rotor with a plurality of turbine blades; a plurality of blade tracks positioned circumferentially around the turbine blades; at least one dovetail shaped connecting member extending radially outward from each blade track; and a hanger connected to a structural member of the gas turbine engine and configured to releasably couple with the at least one dovetail shaped connecting member of a corresponding blade track. The blade track can be formed from a ceramic matrix composite material and the hanger can be formed from a metallic material in one form of the disclosure. While the invention has been illustrated and described in detail in the drawings and foregoing description, the same is to be considered as illustrative and not restrictive in character, it being understood that only the preferred embodiments have been shown and described and that all changes and modifications that come within the spirit of the inventions are desired to be protected. It should be understood that while the use of words such as preferable, preferably, preferred or more preferred utilized in the description above indicate that the feature so described may be more desirable, it nonetheless may not be necessary and embodiments lacking the same may be contemplated as within the scope of the invention, the scope being defined by the claims that follow. In reading the claims, it is intended that when words such as “a,” “an,” “at least one,” or “at least one portion” are used there is no intention to limit the claim to only one item unless specifically stated to the contrary in the claim. When the language “at least a portion” and/or “a portion” is used the item can include a portion and/or the entire item unless specifically stated to the contrary. (责任编辑:admin) |