- Joined
- Oct 30, 2003
- Messages
- 18,445
- Location
- Santa Maria, California
- Aircraft
- Givens Predator
- Total Flight Time
- 2600+ in rotorcraft
I feel there is value in re-examining my takeoff procedures flying The Predator from time to time.
Whatever gyroplane you fly; please follow the procedures in the pilot’s operating handbook.
I had a particularly challenging client who asked a lot of good questions about the how and why of the instrument scan during the takeoff roll.
I want him on the centerline so I don’t want him focused on the instruments.
It is a busy time and I may not pay enough attention to my rotor tachometer focusing too much on how things look and feel.
I often takeoff with a strong cross wind and guess at how much I need to tilt my disk into the wind to have an elegant takeoff.
My prerotator is an automobile starter and can be engaged at any angle.
Without wind I might see a hundred rotor rpm on my thirty foot diameter blades.
I begin my prerotation behind the hold short line and start rolling immediately. I bring the cyclic half back at a hundred rotor rpm because the rotor blades are coning up and I began to have aerodynamic control of the rotor and I bring the cyclic full back at a hundred twenty rotor rpm at which point I release the prerotator. This is generally about the time I reach the center line of the 150 foot wind runway.
One way to lose control of the blades (commonly called flapping or sailing the blades) with a two blade semi rigid teetering rotor on takeoff is to have too much indicated air speed for the rotor rpm. The retreating blade stalls first because it is at a higher angle of attack and the advancing blade sails forcing the stalled retreating blade to collide with the vertical stabilizer, rudder or propeller blades.
This is a very common gyroplane takeoff mishap and generally results in considerable damage to the gyroplane.
I leave the cyclic full back until around a hundred eighty to two hundred rotor rpm and no more than fifteen of ground speed at which point I smoothly advance the throttle and soon the nose comes up and I began to move the cyclic forward keeping the nose tire near the ground.
She waddles into the air on her own around forty five knots indicated air speed and around 300 rotor rpm.
She lingers near the ground until I see fifty knots and around three hundred thirty rotor rpm where she begins to climb at something over five hundred feet per minute depending on the takeoff weight and density altitude.
I typically fly from an eight thousand foot runway so there is no need to be so precise with the rotor rpm to shorten the takeoff distance.
Using the rotor tachometer gives me a basis for teaching rotor management.
I recently paid more attention to how tilting the disk into the cross wind affects my rotor acceleration and found there is substantial difference in how fast the rotor accelerates.
Because of the reduced drag of the rotor The Predator also accelerates faster with the disk tilted into the wind for a cross wind takeoff.
My conclusion is to be more conscious of the difference a cross wind makes; start the takeoff roll with the disk flat and tilt it into the wind just before liftoff.
In other words I need to take more time with a crosswind takeoff to allow the rotor to accelerate and perhaps add a little less power to keep from too much indicated air speed for the rotor rpm.
I fly so often in winds it is easy to become overconfident and become careless with the numbers.
Even in a gyroplane that prerotates to over two hundred rotor rpm; rotor management is important and the relative wind is still responsible for accelerating the rotor to flight rpm. Tilting the rotor into the wind will still slow the rotor acceleration and increase the speed the aircraft will accelerate for a given power setting.
Whatever gyroplane you fly; please follow the procedures in the pilot’s operating handbook.
I had a particularly challenging client who asked a lot of good questions about the how and why of the instrument scan during the takeoff roll.
I want him on the centerline so I don’t want him focused on the instruments.
It is a busy time and I may not pay enough attention to my rotor tachometer focusing too much on how things look and feel.
I often takeoff with a strong cross wind and guess at how much I need to tilt my disk into the wind to have an elegant takeoff.
My prerotator is an automobile starter and can be engaged at any angle.
Without wind I might see a hundred rotor rpm on my thirty foot diameter blades.
I begin my prerotation behind the hold short line and start rolling immediately. I bring the cyclic half back at a hundred rotor rpm because the rotor blades are coning up and I began to have aerodynamic control of the rotor and I bring the cyclic full back at a hundred twenty rotor rpm at which point I release the prerotator. This is generally about the time I reach the center line of the 150 foot wind runway.
One way to lose control of the blades (commonly called flapping or sailing the blades) with a two blade semi rigid teetering rotor on takeoff is to have too much indicated air speed for the rotor rpm. The retreating blade stalls first because it is at a higher angle of attack and the advancing blade sails forcing the stalled retreating blade to collide with the vertical stabilizer, rudder or propeller blades.
This is a very common gyroplane takeoff mishap and generally results in considerable damage to the gyroplane.
I leave the cyclic full back until around a hundred eighty to two hundred rotor rpm and no more than fifteen of ground speed at which point I smoothly advance the throttle and soon the nose comes up and I began to move the cyclic forward keeping the nose tire near the ground.
She waddles into the air on her own around forty five knots indicated air speed and around 300 rotor rpm.
She lingers near the ground until I see fifty knots and around three hundred thirty rotor rpm where she begins to climb at something over five hundred feet per minute depending on the takeoff weight and density altitude.
I typically fly from an eight thousand foot runway so there is no need to be so precise with the rotor rpm to shorten the takeoff distance.
Using the rotor tachometer gives me a basis for teaching rotor management.
I recently paid more attention to how tilting the disk into the cross wind affects my rotor acceleration and found there is substantial difference in how fast the rotor accelerates.
Because of the reduced drag of the rotor The Predator also accelerates faster with the disk tilted into the wind for a cross wind takeoff.
My conclusion is to be more conscious of the difference a cross wind makes; start the takeoff roll with the disk flat and tilt it into the wind just before liftoff.
In other words I need to take more time with a crosswind takeoff to allow the rotor to accelerate and perhaps add a little less power to keep from too much indicated air speed for the rotor rpm.
I fly so often in winds it is easy to become overconfident and become careless with the numbers.
Even in a gyroplane that prerotates to over two hundred rotor rpm; rotor management is important and the relative wind is still responsible for accelerating the rotor to flight rpm. Tilting the rotor into the wind will still slow the rotor acceleration and increase the speed the aircraft will accelerate for a given power setting.