UNIVERSITY COLLEGE OF ENGINEERING
RTU, KOTA
PRESENTATION ON
DIFFERENT TYPES OF TRIM TABS
Submitted to-
Mr. Anshul Bansal
Submitted by-
Sujeet kumar (14/616)
CONTENT
Tabs Location On Aircraft
Secondary Flight Control
Elevator Trim Tab System
Rudder and Aileron Trim Tab System
TAB LOCATION COLOUR CODE
AILLERON
ELEVATOR
RUDDER
TABS LOCATION ON AIRCRAFT
Secondary Flight Control
Elevator Trim Tab System
Elevator trim balances the control force necessary to
maintain the aerodynamic down force on the tail. When
aircraft is flying, a lot of trim could be required to maintain
the desired angle of attack. This mainly applies to slow flight,
where maintaining a nose-up attitude requires a lot of trim.
An important design parameter for aircraft is the stability of
the aircraft when trimmed for level flight. Any disturbances
such as gusts or turbulence will be damped over a short
period of time and the aircraft will return to its level flight
trimmed airspeed.
Trim Tab Up Elevator Down Trim Tab Down Elevator Up
An Elevator Trim Tab System
Secondary Flight Control
Types of Trim Tab System
Secondary Flight Control
Rudder and Aileron Trim Tab System
Trim doesn't only apply to the elevator, as there is also trim
for the rudder and ailerons. The use of this is to counter the
effects of slip stream, or to counter the effects of the centre
of gravity being to one side. This can be caused by a larger
weight on one side of the aircraft compared to the other,
such as when one fuel tank has a lot more fuel in it than the
other, or when there are heavier people on one side of the
aircraft than the other.
A Rudder Trim Tab System
Hands on experience with various type of tabs

Hands on experience with various type of tabs

  • 1.
    UNIVERSITY COLLEGE OFENGINEERING RTU, KOTA PRESENTATION ON DIFFERENT TYPES OF TRIM TABS Submitted to- Mr. Anshul Bansal Submitted by- Sujeet kumar (14/616)
  • 2.
    CONTENT Tabs Location OnAircraft Secondary Flight Control Elevator Trim Tab System Rudder and Aileron Trim Tab System
  • 3.
    TAB LOCATION COLOURCODE AILLERON ELEVATOR RUDDER TABS LOCATION ON AIRCRAFT
  • 4.
    Secondary Flight Control ElevatorTrim Tab System Elevator trim balances the control force necessary to maintain the aerodynamic down force on the tail. When aircraft is flying, a lot of trim could be required to maintain the desired angle of attack. This mainly applies to slow flight, where maintaining a nose-up attitude requires a lot of trim. An important design parameter for aircraft is the stability of the aircraft when trimmed for level flight. Any disturbances such as gusts or turbulence will be damped over a short period of time and the aircraft will return to its level flight trimmed airspeed.
  • 5.
    Trim Tab UpElevator Down Trim Tab Down Elevator Up An Elevator Trim Tab System
  • 6.
  • 7.
    Secondary Flight Control Rudderand Aileron Trim Tab System Trim doesn't only apply to the elevator, as there is also trim for the rudder and ailerons. The use of this is to counter the effects of slip stream, or to counter the effects of the centre of gravity being to one side. This can be caused by a larger weight on one side of the aircraft compared to the other, such as when one fuel tank has a lot more fuel in it than the other, or when there are heavier people on one side of the aircraft than the other.
  • 8.
    A Rudder TrimTab System