Propeller Owner’s Manual
147
DESCRIPTION AND OPERATION
61-00-47
Page 2-21
Rev. 16 May/20
C. Feathering and Reversing Propellers HC-E5B-5A,
HC-E(4,5)N-5KL, and HC-E4P-5 Models
Refer to Figure 2-8, Figure 2-9, Figure 2-10, and
Figure 2-11. The propeller described in this section is
constant speed, feathering and reversing. It utilizes a single
oil supply from a governing device to hydraulically actuate a
change in blade angle. This propeller has five blades and is
used primarily on Garrett (Honeywell) turbine engines.
A two piece aluminum hub retains each propeller blade on a
thrust bearing. A cylinder is attached to the hub and contains
a feathering spring and piston. The hydraulically actuated
piston transmits linear motion through a pitch change rod
and fork to each blade to result in blade angle change.
While the propeller is operating the following forces are
constantly present, 1) spring force, 2) counterweight force,
3) centrifugal twisting moment of each blade and 4) blade
aerodynamic twisting forces. The spring and counterweight
forces attempt to rotate the blades to higher blade angle,
while the centrifugal twisting moment of each blade is
generally toward lower blade angle. Blade aerodynamic
twisting force is usually very small in relation to the other
forces and can attempt to increase or decrease blade angle.
The summation of the propeller forces is toward higher pitch
(low RPM) and is opposed by a variable force toward lower
pitch (high RPM). The variable force is oil under pressure
from a governor with an internal pump, which is mounted
on and driven by the engine. The oil from the governor
is supplied to the propeller and hydraulic piston through
a hollow engine shaft. Increasing the volume of oil within
the piston and cylinder will decrease the blade angle and
increase propeller RPM. Decreasing the volume of oil will
increase blade angle and decrease propeller RPM. By
changing blade angle the governor can vary the load on the
engine and maintain constant engine RPM (within limits),
independent of where the power lever is set. The governor
uses engine speed sensing mechanisms that allow it to
supply or drain oil as necessary to maintain constant engine
speed (RPM).
Содержание HC-E4 3 Series
Страница 6: ...Page 4 Rev 17 Sep 20 MESSAGE 61 00 47 Propeller Owner s Manual 147 This page is intentionally blank...
Страница 26: ...Propeller Owner s Manual 147 TABLE OF CONTENTS Page 2 Rev 16 May 20 61 00 47 This page is intentionally blank...
Страница 107: ...Propeller Owner s Manual 147 INSTALLATION AND REMOVAL 61 00 47 Page 3 17 Rev 16 May 20 This page is intentionally blank...
Страница 127: ...Propeller Owner s Manual 147 INSTALLATION AND REMOVAL 61 00 47 Page 3 37 Rev 17 Sep 20 This page is intentionally blank...
Страница 160: ...Propeller Owner s Manual 147 INSTALLATION AND REMOVAL 61 00 47 Page 3 70 Rev 17 Sep 20 This page is intentionally blank...
Страница 162: ...Propeller Owner s Manual 147 TESTING AND TROUBLESHOOTING 61 00 47 Page 4 2 Rev 6 May 20 This page is intentionally blank...
Страница 187: ...Propeller Owner s Manual 147 INSPECTION AND CHECK 61 00 47 Page 5 17 Rev 17 Sep 20 This page is intentionally blank...
Страница 210: ...Propeller Owner s Manual 147 INSPECTION AND CHECK 61 00 47 Page 5 40 Rev 17 Sep 20 This page is intentionally blank...
Страница 223: ...Propeller Owner s Manual 147 MAINTENANCE PRACTICES 61 00 47 Page 6 13 Rev 16 May 20 This page is intentionally blank...
Страница 242: ...Propeller Owner s Manual 147 MAINTENANCE PRACTICES 61 00 47 Page 6 32 Rev 16 May 20 This page is intentionally blank...
Страница 250: ...RECORDS 61 00 47 Page 8 2 Rev 17 Sep 20 Propeller Owner s Manual 147 This page is intentionally blank...
Страница 270: ...RECORDS 61 00 47 Page 8 22 Rev 16 May 20 Propeller Owner s Manual 147 This page is intentionally blank...
Страница 280: ...RECORDS 61 00 47 Page 8 32 Rev 16 May 20 Propeller Owner s Manual 147 This page is intentionally blank...