turn indicator Flashcards
turn indicator
1 gimbal, gyro and degree of freedom
only able to rotate about longitudinal axis
restrained by springs either side- provide restoring force
as aircraft turns longitudinal axis moves (yaws) along horizontal axis
precession acts 90° to yaw and acts at top or bottom of gyro causing it to tilt
turn indicator display
needle shows rate 1,2,3 turns and balance ball rate 1- 3°/sec,360°=2min rate 2- 6°/sec, 360° = 1min rate 3- 9°/sec, 360° = 40sec
turn indicator operation
needle connected to gimbal
gimbal deflection related to turn rate
turn indicator errors
indicator relies on: TAS, gyro rotor RPM, absence of accelerations in pitch
only accurate for one TAS but fairly accurate for wide range of speeds
not at correct RPM precession incorrect:
RPM high- over read
RPM low- under read
affected by pitching:
pitch up- over read
pitch down- under read
is there an unusable or toppled position for a turn indicator?
no
provided it is powered
turn coordinator
axis for gimbal tilted at 30°- makes it more sensitive to roll
small amounts of roll quickly detected
turn coordinator easier to use than turn indicator
shows wings level or rate 1 turn- display has no pitch info wrote on
turn coordinator errors
same as indicator
only strictly accurate at one TAS and one rotor RPM and zero pitch rate
TI & TC behaviour during a spin
TI not sensitive to roll- always correctly indicate yaw and thus direction of spin
TC is sensitive to roll- in unstable or inverted spin may indicate incorrectly
balance indicator
rear flow tube- allow free movement of fluid when ball moves
shows if turn in balance or not
fluid provides dampening
curved tube acts as pendulum
correcting imbalance
step on ball
ball opposite to turn - skid
ball same as turn - slip
effect of imbalance on turn radius
skid- radius decrease
slip- radius increase
AOB for rate 1 =
(TAS/10) + 7