Interlocking stage for airfoils
A technology of locking interface and shield, applied in the direction of engine elements, blade support elements, machines/engines, etc., can solve problems such as expensive and time-consuming
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[0040] Reference will now be made in detail to embodiments of the invention, one or more examples of which are illustrated in the accompanying drawings. The detailed description uses numerical and letter designations to refer to features in the drawings. The same or similar symbols have been used in the drawings and the specification to designate the same or similar parts of the present invention.
[0041] As used herein, the terms "first", "second" and "third" may be used interchangeably to distinguish one component from another and are not intended to indicate the position or importance of the various components.
[0042] The terms "forward" and "rearward" refer to relative positions within the gas turbine engine or vehicle, and to the normal operating attitude of the gas turbine engine or vehicle. For example, with respect to a gas turbine engine, forward refers to a location closer to the engine inlet, and aft refers to a location closer to the engine nozzle or exhaust. ...
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