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Back to: "S"semirigid rotor
- Definição1
- A rotor which may change pitch and flap as a unit.
- Fonte1
- SCHAFER, Joe. Helicopter maintenance. Englewood: Jeppesen Sanderson, Inc., c2007. viii, 343 p.
- Definição2
- A rotor system in which the blades are fixed to the hub but are free to flap and feather.
- Fonte2
- FEDERAL AVIATION ADMINISTRATION. Rotorcraft flying handbook (FAA-H-8083-21). Washington, DC: FAA, 2000. Disponível em: http://www.faa.gov/library/manuals/aircraft/media/faa-h-8083 -21.pdf. Acesso em: 10 fev. 2012.
- Definição3
- A type of helicopter rotor that allows the pitch of the blades to be changed by rotating the blades about their feather axis (the axis that extends along the length of the blade). The blade cannot flap up and down individually, but the entire rotor can flap as a unit. It is free to teeter (rock back and forth) about the mast.
- Fonte3
- CRANE, Dale (ed.). Dictionary of aeronautical terms. 4th ed. Newcastle: ASA, 2006.
- Definição4
- A rotor system in which the blades are fixed to the hub, generally by a teetering or seesaw hinge, allowing the blades to flap and feather but not lead-lag or drag.
- Fonte4
- KUMAR, Bharat (ed.). An illustrated dictionary of aviation. New York: McGraw-Hill, c2005. 752 p.
- Subárea1
- Rotorcraft
- Related Term
- rigid rotor
- Português
- rotor semirrígido
- Imagem
Rotor of a Bell 212/HH-1N helicopter.
Fonte: http://en.wikipedia.org/wiki/File:Navy-hh1n-158256-070327-16cr-10.jpg
Rigid rotor systemb.
Fonte: KUMAR, Bharat (ed.). An illustrated dictionary of aviation. New York: McGraw-Hill, c2005. 752 p.
