Transition duct with vanes in gas turbine engine

The present invention relates to a transition duct relates to a transition duct (transition duct) the vane (vane) in a gas turbine engine is installed, the vanes by providing a more particularly to a vane in the transition duct of the internal gas turbine installed in the center of the duct . Transition ducts are installed in the vane in a gas turbine engine in accordance with the present invention and delivering gases in between the compressor and the turbine or compressor and the turbine; In includes an outer duct and an inner duct is formed of a metal, and a gas turbine engine with a transition duct configured to flow, substantially cylindrical inlet connection and, substantially cylindrical outlet connection between the duct and the duct, the transition duct the vane is installed in the intermediate portion, it characterized in that the gas turbine engine is made compact. The provision of the vanes in a gas turbine of the inner transition duct according to the present invention, the transition duct and the vanes are mixed because it can be converted also circumferential velocity as well as to change the length of the gas flow path through the vanes, and finally the length of the vane the length of the engine may be reduced by as much. Further, simply can not be shortened by the length of the vane engine shaft, such as the case of the overall engine length becomes shorter so it reduces the weight of the engine through. The transition duct, the transition duct, a gas turbine, the vane