Blade Blade Tip Cavitation Cup Diameter Hub Leading Edge Non Thru-Hub Exhaust Over-Hub Exhaust Over/Thru-Hub Exhaust Pitch Radius Rake Rotation Trailing Edge Controllable Pitch Propeller Fixed Pitch Propeller Constant Pitch Propeller Variable Pitch Propeller Thru Hub Ehxuast Skew Slip Ventilation Cylindrical Section Pitch Reference Line Geometric Pitch Angle Track
Suction side. Forward side of the blade (surface facing the bow).
Pressure Side, Pitch Side. Aft side of the blade (surface facing the stern).
Equal to the number of blades on the propeller.
Fillet area. The region of transition from the blade surfaces and edges to the hub periphery. The area where the blade attaches to the hub.
Maximum reach of the blade from the center of the hub. Separates the leading and trailing edges.
Cavitation, (which is often confused with ventilation), is a phenoma of water vaporizing or “boiling” due to the extreme reduction of pressure on the back of the propeller blade. Many propellers partially cavitate during normal operation, but excessive cavitation can result in physical damage to the propeller’s blade surface due to the collapse of the microscopic bubbles on the blade. There may be numerous causes of cavitation such as incorrect matching of propeller style to application, incorrect pitch, physical damage to the blade edges, etc
Small radius of curvature located on the trailing edge of the blade. This curved lip on the propeller allows it to get a better bite in the water. This results in reduced vebtilation, slipping, and allows for a better hole shot in many cases.
Diameter is two times the distance from the center of the hub to the tip of the blade. It can also be looked at as the distance across the circle that the propeller would make when rotating. This is the first number listed when describing a propeller.
Solid cylinder located at the center of the propeller. Bored to accommodate the engine shaft. Hub shapes include cylindrical, conical, radius, & barreled.
The edge of the propeller blade adjacent to the forward end of the hub. When viewing the propeller from astern, this edge is furthest away. The leading edge leads into the flow when providing forward thrust.
Non thru-hub exhaust propellers are used for inboards using shaft driven propellers, sterndrives using through hull exhaust, and on some outboards that don’t route the exhaust through the lower topedo.
Over-hub exhaust propellers have the blades attached directly to the smaller tube that fits over the propeller shaft, eliminating the larger exhaust tube. These types of propellers are often used for attaining maximum top speeds. (On some boats, the hole shot can suffer due to extreme exhuast flooding that occurs around the propeller blades during acceleration.)
Over/Thru-hub exhaust propellers are a combination of thru-hub and over-hub exhaust propellers. This allows some exhaust to escape at lower RPMs, providing a controlled amount of exhaust flooding. These types of propellers will allow the propeller to be slightly easier to turn during initial acceleration, allowing for a better hole shot on some engine/boat combinations.
Pitch is defined as the theoretical forward movement of a propeller during one revolution — assuming there is no “slippage” between the propeller blade and the water.
Pitch is the second number listed in the propeller description.
The distance from the axis of rotation to the blade tip. The radius multiplied by two is equal to the diameter.
Rake is the degree that the blades slant forward or backwards in relation to the hub. Rake can affect the flow of water through the propeller, and as implications with respect to boat performance.
Aft Rake helps to trim the bow of the boat upward, which often results in less wetted surface area and therefore higher top end speed.
Forward, or negative rake, helps hold the bow of the boat down. This is more common in workboat type applications.
When viewed from the stern (facing forward): Right-hand propellers rotate clockwise to provide forward thrust. Left-hand propellers rotate counter-clockwise to provide forward thrust.
The edge of the propeller adjacent to the aft end of the hub. When viewing the propeller from astern, this edge is closest. The trailing edge retreats from the flow when providing forward thrust.
The propeller blades mount separately on the hub, each on an axis of rotation, allowing a change of pitch in the blades and thus the propeller.
The propeller blades are permanently mounted and do not allow a chance in the propeller pitch.
The propeller blades have the same value of pitch from root to tip and from leading edge to trailing edge.
The propeller blades have sections designed with varying values of local face pitch on the pitch side or blade face.
Thru-hub exhaust propellers consist of a round barrel to which the blades are attached. The exhaust passes through the barrel and out the back, without making contact with the propeller blades. This provides a good, clean water flow to the blades, usually resulting in good acceleration and hole shot.
The transverse sweeping of a blade such that viewing the blades from fore or aft shows an asymmetrical shape.
Aft skew is positive skew, where blades sweep in the direction opposite of rotation.
Forward skew is negative skew, where blades sweep in the same direction as rotation.
Slip is the difference between actual and theoretical travel of the propeller blades through water. A properly match propeller will actually move forward about 80 to 90 perfect of the theoretical pitch.
A situation where surface air or exhaust gases are drawn into the propeller blades. When this situation occurs, boat speed is lost and engine RPM climbs rapidly. This can result from excessively tight cornering, a motor that is mounted very high on the transom, or by over-trimming the engine.
A cross section of a blade cut by a circular cylinder whose centerline is the propeller axis of rotation.
Reference line used to establish the geometric pitch angle for the section. This line may pass through the leading and trailing edges of the section and may be equivalent to the chord line.
The angle between the pitch reference line and a line perpendicular to the propeller axis of rotation.
The absolute difference of the actual individual blade height distributions to the other blade height distributions. Always a positive value and represents the spread between the individual blade height distributions.