Cover
AssigneeDowty Aerospace Gloucester Limited
InventorBrian G. Kirkman
Life of this patent
Estimating the term…
Abstract
A cover provided for covering a bladed rotor during a testing operation. The cover has a face plate of solid sheet like material having a centrally positioned orifice through which air is drawn by the action of part of blade adjacent to orifice. The remaining part of the blades is in a stalled condition and therefore relatively unloaded. The power required to turn the rotor is therefore reduced in comparison to that required if the cover was not present making testing easier. The cover also acts as a safety shroud preventing personnel coming into contact with the blades as they rotate and containing the rotor in the event of its disintegration.
Claims7
In combination with turbine equipment having a bladed rotor, a cover for use in the testing of said equipment, which cover includes:
- a face plate positioned so that in use any air drawn by the bladed rotor during testing encounters said face plate prior to the bladed rotor;
- a solidly formed side wall which circumferentially surrounds the bladed rotor, adjacent to tips of the bladed rotor, and to which said face plate is connected;
- and
- a meshed back plate positioned on the side of the bladed rotor opposite to said face plate and which is connected to said side wall;
- wherein said face plate covers a part of said rotor such that during testing over part of the blade length no air flow exists resulting in this part of the length of the blade experiencing stall characteristics, whilst over the remaining part of the blade length air flow exists enabling the turbine equipment to be accurately tested.
Dependencies are inferred from the claim text.