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208 results about "Decreased diameter" patented technology

Turbine cooling air centrifugal particle separator

A centrifugal particle separator (202) is provided for removing particles such as dust particles from the compressed airflow (110) prior to reaching and cooling the turbine blades (122, 124, 126) of a turbine engine (100). A particle separator structure (208) has a side facing the axis (118) about which it rotates, the side including a plurality of pocket dividers (214) defining a plurality of pockets (216), and further defining an entrance cavity (206) for receiving the compressed air (110) containing particles. An inner flowpath coupling (218) includes a side opposed to the axis (118) that is positioned adjacent the particle separator structure (208) to define an airflow path (220) having an entrance communicating with the entrance cavity (212) and an exit (222), wherein the diameter (226) of the airflow outer flowpath (224) decreases from the entrance to the exit, and wherein a centrifugal force created by the centrifugal particle separator assembly (202) rotating around the axis (118) and the decreasing diameter (226) of the airflow path (224) which accelerates the rotational velocity of the air, forces the particles (228) to collect within the plurality of pockets (216) and the remaining compressed air is provided to cool turbine blades (122, 124, 126). A plurality of optional air accelerator fins (210) may be positioned within the entrance cavity (212). The combination of quickly accelerating air from non-rotating to rotating velocity, for example, by accelerator fins (210), and further subjecting the air and entrained particles to increasing rotational velocity resulting in an increasing centrifugal force field as particles (228) progress from the entrance (212) to the exit (222) of the separator assembly (202), efficiently removes the particles (228) from the air.
Owner:HONEYWELL INT INC

Seal head heat insulating layer forming method and mold of filament winding engine heat insulating structure

ActiveCN105437521AOvercome stabilityOvercome the defect of low bonding strengthDomestic articlesVulcanizationEngineering
The invention discloses a seal head heat insulating layer forming method of a filament winding engine heat insulating structure. A cover layer and a bottom layer of a seal head heat insulating layer are firstly and independently formed in a vulcanization and compression manner and then overall formed in a vulcanization and compression manner, and the defect that the forming quality stability and consistency of manual SMT technology products are low is overcome. A release agent is sprayed or release cloth is pasted in the direction with the decreasing diameter at the crack arrest point, a proper tackiness agent is adopted in other lining layers, and the releasing effect of the cover layer and the bottom layer of the manufactured seal head heat insulating layer is good. In addition, when the seal head heat insulating layer is a rear seal head heat insulating layer, an EPDM heat insulating material wrapping structure is adopted in a T-1 anti-elation layer, and therefore the seal head heat insulating layer is isolated from a high-strength aluminum alloy connector. According to a provided integral forming mold, two sets of tools of the integral forming mold and a bottom layer forming mold can be achieved only by replacing an upper integral mold and an upper bottom layer mold, the structure is simple, and cost is low. Meanwhile, locating and mold releasing can be achieved well, and mold stripping of products is facilitated.
Owner:湖北三江航天江北机械工程有限公司
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