Term which describes the main rotor blades of a helicopter.
A rotor for a rotary wing aircraft is provided, which includes a hub and a number of rotor blades (10).
The main rotor blade (52) is rotatable about a rotation axis that is tilted forwardly from a vertical axis of the aircraft.
The main rotor blade (52) is rotatable about a rotation axis that is tilted forwardly from a vertical axis of the aircraft.
The position of Manager of RW Flight Training and Standards was vacant at the time of the occurrence.
The Manager of RW Flight Safety position became vacant on 17 January 2013.
Until that time, rotary-wing aircraft designers were stymied by the problem of a rolling moment that was encountered when the aircraft began to move forward.
Until that time, rotary-wing aircraft designers were stymied by the problem of a rolling moment that was encountered when the aircraft began to move forward.
These companies do not have formal “doing business as” names; however, they are commonly referred to internally as “Ornge fixed-wing (FW)” and “Ornge rotor-wing (RW)”.
fixed wing and rotary wing aircraft
A rotary wing aircraft bearing for providing constrained relative motion between a first rotary wing aircraft member and a second rotary wing aircraft member.
The invention provides a rotary wing aircraft helicopter vehicle rod end and method of making a rod end.
The load is lifted by the necessary lifting force generated on the rotary wings.
Method of mounting an engine (50) in a rotary wing aircraft.
a Very Light Rotorcraft.
a Very Light Rotorcraft.
A rotary-wing aircraft having a rotary-wing aircraft rotor comprising a differential torque- splitting mechanism and a gimbal mechanism is disclosed.
A rotor-hub for a rotary-wing aircraft is disclosed.
An aircraft of any type supported by a rotor and having an auxiliary tail is provided with means that allows, at the moment of take-off, at least part of its tail to take an inclined position in relation to the position of flight.
From 1 (fixed propellers) to 2, 4 and 8 propellers (rotary propellers).
The invention is particularly applicable to autogyros.
A rotary-wing shaped fiber filter material includes a fiber bundle (1) composed of fibers and a rotary-wing core (2).
rotorcraft of 3175 kg MTOM or less
rotorcraft of 3175 kg MTOM or less
1.17.3.7.2 Manager, Rotor-wing Flight Training and Standards
(v) aerial construction operations using rotating wing aircraft,
A mechanical flight control system for a rotary-wing aircraft is disclosed.
A rotor kite or gyroglider is an unpowered rotary-wing aircraft.
A system and method to control hovering flight of a rotary aircraft.
Requêtes fréquentes français :1-200, -1k, -2k, -3k, -4k, -5k, -7k, -10k, -20k, -40k, -100k, -200k, -500k, -1000k,
Requêtes fréquentes anglais :1-200, -1k, -2k, -3k, -4k, -5k, -7k, -10k, -20k, -40k, -100k, -200k, -500k, -1000k,
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