AVIA PROPELLER - Propeller design specification form

Formulář požadavků na výrobek

Pomocí tohoto formuláře vám pracovníci AVIA Propeller doporučí nejvhodnější vrtuli pro vaše letadlo.

(Prosíme o kompletní vyplnění formuláře)

Aircraft Model
Manufacturer:

Max. Take Off Weight:

lbs

Engine Model:

Takeoff Power:

RPM

Max. Continuous:

RPM

No. of Cylinders:

Gear Ratio, if applicable:

RPM Restrictions:

RPM

Desired Propeller:

Fix pitch

Ground Adjustable

Hydraulic Constant Speed

Principally designed for:

Climb

Cruise

Allround

Agricultural

Aerobatic

Configuration:

Tractor

Pusher

Rotation (view in flight direction):

Single Engine:

Righthand

Lefthand

Multi Engine:
	Left Prop:	Righthand	Lefthand
	Right Prop:	Righthand	Lefthand

Features:

Counterweight

Feathering

Reversing

Prop Deice Required:

Yes

System Voltage:	VDC
Max. Permissible Diameter:	inches
Number of Blades:
Hub / Engine Flange Type:
Max. Propeller weight:	lbs
Max. Polar Moment of Inertia:	lb inch2
Spinner Diameter:	inches
Spinner Distance to Flange:	inches

Spinner Tip (pointed ore round):

AIRCRAFT DESIGN CONDITIONS

Max. Speed at Sea Level	KTAS @	HP @	RPM @
	Desired Thrust	lbs
Max. Speed KTAS @	ft MSL @	HP @	RPM @
	Desired Thrust lbs
VNE: KIAS
Best Climb Rate ft/min @ KIAS

Aircraft data for 1xP Excitation Evaluation

Engine Position:

Wing

Nose

Angle between the Propeller Axis and Wing Chord deg

Max. Climb:	Angledeg @ KTAS @ HP @ RPM
Max. Descent:	Angledeg @ KTAS @ HP @ RPM
Max. Yaw:	Angledeg @ KTAS @ HP @ RPM

Additional Comments:

		Name Address:
	First Name:
	Last Name:
	Company:
	Street:
	City, State:
	ZIP-Code:
	Country:
	Phone No:
	Fax No:
	E-mail:


	AVIA PROPELLER Tel: (+420) 296 336 530; -32, Fax: (+420) 296 336 519 E-Mail: sales@aviapropeller.cz, techsupport@aviapropeller.cz