Turbocharger
A technology of turbocharger and turbine rotor, which is used in machine/engine, leakage prevention, engine components, etc., can solve the problems of seal ring wear, wear seal ring, aggravate bearing wear, etc., and achieve temperature reduction and contact area reduction. , to avoid the effect of carbon deposition in lubricating oil
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no. 1 example
[0025] Such as image 3 As shown, the turbocharger among the present invention includes a turbine rotor 1, a shaft 2, an intermediate housing 3, and a pinch wheel 4, and each part and the relationship between them are described in detail below:
[0026] Such as Figure 3 to Figure 5 As shown, at least a part of the turbine rotor 1 is located outside the intermediate casing 3. The turbine rotor 1 includes a hub 10, a plurality of first blades 11 that receive the pressure of the exhaust gas to rotate the hub, and receive the pressure of the exhaust gas to rotate the hub. A plurality of second blades 12, the first blades 11 and the second blades 12 are alternately arranged along the circumferential direction of the hub, one end of the second blade 12 is located on the same circumference of the hub 10 as one end of the first blade 11, the second blade 12 is smaller than the axial dimension of the first blade 11 along the hub 10, that is, the length of the second blade 12 is small...
no. 2 example
[0040] Such as image 3 and Figure 7 As shown, one end of the fixed shaft 2 of the turbine rotor 1 is provided with a first cavity 15, and a first barrier medium 16 for isolating the direct heat transfer between the turbine rotor 1 and the shaft 2 is sealed in the first cavity 15, so as to reduce exhaust gas The heat is transferred to the sealing assembly through the turbine rotor 1 and the shaft 2 , and the thermal conductivity of the first barrier medium 16 is smaller than that of the shaft 2 and the turbine rotor 1 . The rest of the structure is the same as that of the first embodiment, and will not be repeated here.
no. 3 example
[0042] Such as image 3 As shown, the difference from the first embodiment is that it also includes a heat insulation assembly that isolates the heat of the exhaust gas from being directly transmitted to one end of the intermediate casing, the heat insulation assembly is fixed at one end of the intermediate casing, and the heat insulation assembly is located on the turbine rotor 1 and the middle housing 3; the heat insulation assembly includes a first heat insulation component 5 and a second heat insulation component 6, and a second cavity 7 is formed between the first heat insulation component 5 and the second heat insulation component 6 , at least in the second cavity 7 is sealed a second barrier medium used to block the direct heat transfer between the exhaust gas and a part of the intermediate housing, so as to reduce the heat transfer of the exhaust gas to the sealing assembly through the intermediate housing 3 .
[0043] For the above several embodiments of the turbochar...
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