US 12,297,777 B1
Jet engine
Xin Yuan, Shanghai (CN)
Assigned to XinY Structural Consultants, Shanghai (CN)
Filed by XinY Structural Consultants, Shanghai (CN)
Filed on Dec. 6, 2024, as Appl. No. 18/971,137.
Application 18/971,137 is a continuation of application No. PCT/CN2023/133925, filed on Nov. 24, 2023.
Claims priority of application No. 202311489141.X (CN), filed on Nov. 9, 2023.
Int. Cl. F02C 7/00 (2006.01); F01D 5/14 (2006.01); F01D 25/16 (2006.01); F02C 3/06 (2006.01); F02C 7/22 (2006.01)
CPC F02C 7/222 (2013.01) [F01D 5/141 (2013.01); F01D 25/16 (2013.01); F02C 3/06 (2013.01); F05D 2220/323 (2013.01); F05D 2240/30 (2013.01); F05D 2240/35 (2013.01); F05D 2240/52 (2013.01); F05D 2240/54 (2013.01); F05D 2240/61 (2013.01); F05D 2260/20 (2013.01)] 15 Claims
OG exemplary drawing
 
1. A jet engine, comprising:
an engine casing; and a core engine, wherein the core engine is arranged in the engine casing, has a core engine casing, and comprises a compressor, a turbine, and a combustion chamber arranged between the compressor and the turbine,
wherein,
the compressor is internally provided with a compressor blade, the turbine is internally provided with a turbine blade, radial outer edges of the compressor blade and the turbine blade are connected to the core engine casing, and a space constructed between the engine casing and the core engine casing forms an engine-mounted fuel tank for accommodating fuel, and
the engine-mounted fuel tank extends from the compressor to the turbine and fully encircles the compressor and the turbine.