Assembly of blade and seal for blade pocket
A technology of seals and blades, applied in the field of rotor components, can solve problems such as improper installation of seals and affecting the efficiency of sealing action
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[0010] figure 1 Illustrated is a gas turbine engine 10 of the type preferably arranged for use in subsonic flight, which generally includes the following components in series communication, namely: a fan 12 through which ambient air is propelled; A compressor section 14; a combustor 16 in which compressed air is mixed with fuel and ignited to produce an annular flow of hot combustion gases; and a turbine section 18 for extracting energy from the combustion gases. One or more shafts 17 are in driving engagement with other rotating parts of engine 10 in compressor section 14 and turbine section 18 .
[0011] refer to figure 2 and image 3 , which partially illustrates an embodiment of a rotor assembly 20 for a gas turbine engine 10 . Rotor assembly 20 may be any suitable component of compressor section 14 or turbine section 18 that includes a rotor disk 30 (partially shown) and rotor blades 40 that revolve around axis 11( figure 1 ) of the axis 17 and rotates therewith. In...
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