Method and apparatus for heating a variable pitch propeller mechanism
OwnerSteven F. Schneidewindinventor
Life of this patent
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Abstract
A method and apparatus for heating a variable pitch propeller mechanism for turbo-prop aircraft is provided. Using the apparatus and method it is possible to perform inspection, troubleshooting and maintenance on hydraulic variable pitch propeller mechanisms that are located in a cold environment, without damaging the seals that are in a non-compliant condition due to being cold. The method and apparatus facilitate the performance of such inspection, troubleshooting and maintenance without the need for relocating the aircraft to a hanger and waiting a number of hours for the variable pitch propeller mechanism to reach a suitable temperature.
Claims5
A method for heating a stationary variable pitch propeller mechanism that is located in a cavity defined by a spinner, where the front of the spinner has a hole, comprising the steps of:
- a) taking a supply of warm forced air;
- b) providing a facility to direct the supply of forced air into the cavity defined by the spinner;
- wherein the facility to direct the supply of forced air comprises
- a flexible hose,
- a tubular construction where one end of the tubular construction fits into the hole in the front of the spinner and the other end of the tubular construction is fastened to an end of the flexible hose;
- and
- c) directing the supply of warm forced air through the hole in the front of the spinner.
A method for heating a stationary variable pitch propeller mechanism that is located in a cavity defined by a spinner, where the front of the spinner has a hole, comprising the steps of:
- a) providing a facility to create a supply of warm forced air;
- b) providing a facility to direct the supply of warm forced air into the cavity defined by the spinner, where the facility to direct the supply of warm forced air
- is integral with the facility to create the supply of warm forced air and
- further comprises a tubular construction where one end of the tubular construction fits into the hole in the front of the spinner;
- and
- c) directing the supply of warm forced air through the hole in the front of the spinner.
Dependencies are inferred from the claim text.