Propeller blade retention device

Number of patents in Portfolio can not be more than 2000

United States of America Patent

PATENT NO 8753088
APP PUB NO 20090220344A1
SERIAL NO

12039516

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Importance

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Abstract

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A propeller blade retention system and method of manufacture are disclosed. Because of the design, a truly integral hub is able to house a set of variable pitch blades. Each hub socket establishes a substantially cylindrical interface with its respective blade, making the blade slidably receivable for installation. Each blade is allowed axial rotation, and held inside the socket by a set of angular contact bearings. A snap ring locks the blade against coming back out of the socket. An O-ring is provided in the interface to create a fluid seal. The hub alone accomplishes all of the required load-bearing and weather-seal functions.

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Patent Owner(s)

Patent OwnerAddress
CESSNA AIRCRAFT RHODE ISLAND40 WESTMINSTER STREET PROVIDENCE RI 02903

International Classification(s)

Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Ball, Danny Oxford, US 4 47
Pfeiffer, Kevin Wichita, US 3 46

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