Statements (49)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
Aircraft control surface
|
| gptkbp:canBe |
Split
All-moving Anti-servo tab Electrically actuated Hydraulically actuated Manually actuated Servo tab Trimmable |
| gptkbp:controls |
gptkb:Pitch
|
| gptkbp:criticalFor |
gptkb:Landing
gptkb:Takeoff Maneuvering |
| gptkbp:effectOfDownMovement |
Nose up
|
| gptkbp:effectOfUpMovement |
Nose down
|
| gptkbp:failureMode |
Loss of pitch control
|
| gptkbp:foundIn |
T-tail
V-tail Canard configuration Conventional tail |
| https://www.w3.org/2000/01/rdf-schema#label |
Elevator (aeronautics)
|
| gptkbp:influenced |
gptkb:Lift
Aircraft stability Angle of attack |
| gptkbp:introducedIn |
Early 20th century
|
| gptkbp:location |
Horizontal stabilizer
|
| gptkbp:material |
wood
Aluminum Composite materials |
| gptkbp:movement |
gptkb:Up
gptkb:Down |
| gptkbp:operatedBy |
gptkb:Pilot
Control column |
| gptkbp:partOf |
gptkb:Empennage
|
| gptkbp:regulates |
gptkb:Descent
Climb Level flight |
| gptkbp:relatedTo |
gptkb:Aileron
gptkb:Rudder Stabilator |
| gptkbp:requires |
Hinges
Aircraft pitch control Control linkage Trim tab |
| gptkbp:subjectOf |
Aerodynamics research
Flight control system studies |
| gptkbp:usedOn |
gptkb:aircraft
|
| gptkbp:bfsParent |
gptkb:Rudder
|
| gptkbp:bfsLayer |
7
|