Subject: NAS2-99090 July monthly report
Date: August 2, 2000
The following items were completed or worked on during
July.
- Designed, fabricated, and installed new rotor prerotator.
Includes a modified Suzuki rear end and 2 constant velocity u-joints,
a 5 groove belt drive/clutch with associated pulleys, idler and hydraulic
cylinder, new rotor drive shaft and associated support structures.
- Performed torque proof tests on rotor drive at
3000 ft-lbs.
- Installed engine in aircraft.
- Determined new location for and installed the accessories
that were originally mounted to the engine compartment floor which is
now occupied by radiators and coolers.
- Installed all plumbing - electrical, oil and water.
- Painted rudders, wing, booms and horizontal stabilator.
- Finished installing co-pilot control stick and
adjusted control cables.
- Improve prop design programs to make it easier
to design for a wide variety of engines and aircraft.
- Started work on a new prop spinner.
- Presented forum at Oshkosh on CarterCopter.
The following items need to be completed before flight
testing can resume, hopefully in August.
- Finish checking out electrical systems
- Finish a few mechanical details
- Calibrate all sensors needed to test rotor and
prop in aircraft
- Test rotor to maximum RPM allowable at 2000 ft-lbs.
on drive shaft. Hopefully, the rotor RPM will exceed 450. Check that
rotor and rotor head is stable and smooth at all RPMs between 75 and
450 at varying degrees of collective. Design maximum jump takeoff RPM
is set at 425.
- Assuming rotor tests are completed without additional
modification, calibrate all data inputs and check that data downloading
from aircraft to ground is in working order.
- Retest prop with new spinner.
- Perform taxi test.
Sampling of rotor lift data
| Rotor
RPM |
Rotor
Collective Angle |
Lift |
| 300 |
8º |
4420
lbs. |
| 375 |
6.5º |
5645
lbs. |
| 400 |
3.1º |
3065
lbs. |
| 400 |
6º |
6120
lbs. |
|