Device and method for slow turning of an aeroderivative gas turbine
A gas turbine and aeronautical modification technology, which is applied to gas turbine devices, jet propulsion devices, safety devices, etc., and can solve the problems of high energy consumption public facilities that cannot use starter motors, and no AC current.
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[0031] The following detailed description of the exemplary embodiments refers to the accompanying drawings. The same reference numbers in different drawings identify the same or similar elements. Furthermore, the drawings are not necessarily drawn to scale. In addition, the following detailed description does not limit the invention. Instead, the scope of the invention is defined by the appended claims.
[0032] Reference throughout this specification to "one embodiment" or "an embodiment" or "some embodiments" means that a particular feature, structure, or characteristic described in connection with the embodiment is included in at least one embodiment of the disclosed subject matter. Thus, appearances of the phrases "in one embodiment" or "in an embodiment" or "in some embodiments" in various places throughout this specification are not necessarily referring to the same embodiment. Furthermore, the particular features, structures, or characteristics may be combined in any...
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