Hamilton Standard Propellers Flashcards

1
Q

3 Major Assemblies of Hamilton Standard Prop

A

Hub assembly
Dome assembly
Distributor Valve

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2
Q

What kind of aircraft uses Hamilton Standard Props?

A

Medium and Large radial engine transport category aircraft

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3
Q

consists of two halves that support the spider the propeller blades and the dome assembly.

A

The hub or barrel assembly

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4
Q

what permits each blade to rotate freely within the hub, as well as to hold the blades in place?

A

a combination of bearings and spacers installed between blade butt and the hub

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5
Q

splined to the engine crankshaft and supported in the barrel by the support blocks.

A

The spider

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6
Q

Why is Hydromatic propellers different from other constant speed propellers?

A

the butt of each blade consists of a sector gear that meshes with the pitch changing gear in the dome assembly.

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7
Q

acts as an extension to the engine’s crankshaft and is installed in the center of the dome assembly.

A

distributor valve

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8
Q

purpose of the distributor valve

A

to direct both governor oil and engine oil into and out of the dome assembly.

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9
Q

houses the primary components of the pitch-change mechanism including a piston a rotating cam and a fixed cam

A

dome assembly

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10
Q

The Hydromatic propeller uses ______ to feather the blades.

A

High-pressure oil

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11
Q

why is an oil reservoir and separate electric oil pump are installed in the propeller system?

A

To ensure an adequate supply of oil and a means to pressurize it

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12
Q

What stops the oil pressure delivery when the blades reaches their fully feathered position?

A

electric pressure cutout switch

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13
Q

What disables the governor constant-speed functions when the propeller is feathered or unfeathered?

A

High-pressure transfer Valve

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