The invention discloses a
heat regeneration type gas
turbine, which belongs to the technical field of
gas turbines and comprises a
gas compressor, a
combustion chamber and a heat regenerator, the
gas compressor, the
combustion chamber and the heat regenerator are sequentially connected along a first direction, and the heat regenerator is provided with a hot gas inlet for hot gas to enter the heat regenerator. The heat regenerator is provided with a hot gas inlet, the hot gas inlet is formed in the end face, facing the
combustion chamber, of the heat regenerator and connected with a gas outlet of the
combustion chamber, and during work, high-temperature gas exhausted from the gas outlet of the
combustion chamber directly enters the heat regenerator to exchange heat with cold gas and then is exhausted from the heat regenerator. The
combustion chamber and the heat regenerator are connected without an additional connecting pipeline, and the heat regenerator, the
gas compressor and the combustion chamber are coaxially arranged, so that the
axial length and the radial size of the whole regenerative gas
turbine can be reduced, the weight of the whole regenerative gas
turbine can be reduced, and a higher fuel consumption rate can be obtained on the premise of a smaller overall size; and meanwhile,
cold air enters and exits from the same side of the heat regenerator, the
cold air passing through the heat regenerator does not need to be guided back to a combustion chamber through an additional channel structure, therefore, the structure is simple and compact, the overall dimension of the whole
machine can be further shortened, and the weight of the whole
machine can be further reduced.