Two-duct turbojet engine with bearing cooling function
A jet engine and ducting technology, which is applied in the cooling of engine components, machines/engines, and engines, can solve the problems of short working life of rotating parts and difficulty in lubricants, so as to improve engine performance, reduce operating temperature, and prolong The effect of engine life
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[0020] The following will clearly and completely describe the technical solutions in the embodiments of the present invention with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only some, not all, embodiments of the present invention. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention.
[0021] The purpose of the present invention is to provide a two-duct turbojet engine with bearing cooling function, to reduce the temperature of the bearing working area when the engine is working, reduce the cost of the engine, prolong the life of the engine and improve the performance of the engine.
[0022] In order to make the above objects, features and advantages of the present invention more comprehensible, the present invention will be further described...
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