| 摘要 |
A turbojet engine (400) comprising:
an air breathing gas turbine engine (10) comprising:
a combustion chamber section (52);
a turbine section (16) surrounding the combustion chamber section so that the combustion chamber section is nested at least in part within the turbine section, a rotor portion of the turbine section forming at least part of the combustion chamber section; and
a compressor section (12) surrounding the turbine section;
wherein the compressor section has two or more spools, capable of rotation independent of one another.
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