Examples of 'anti-torque' in a sentence
Meaning of "anti-torque"
Anti-torque is an adjective used in aviation and engineering to describe a device or mechanism that counteracts the torque produced by an engine or rotor
How to use "anti-torque" in a sentence
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anti-torque
Blade for a helicopter anti-torque device.
Such anti-torque systems using an auxiliary rotor are particularly reliable and efficient.
Rotorcraft are also fitted with an anti-torque device.
It further relates to anti-torque and yaw control apparatus for a helicopter.
Some paramotors use an adjustable anti-torque strap.
Such an anti-torque device is also used for guiding the rotorcraft in yaw.
There is then no need for the aircraft to have an anti-torque device.
An anti-torque device serves to maneuver the rotorcraft in turning about a yaw axis.
Which helicopter is remarkable in that said anti-torque system further includes,.
Ducted Anti-torque rotor with floating blades.
This leads to optimized power efficiency for the anti-torque function.
Thus, yaw control and the anti-torque function are provided in particular by the tail rotor.
None of those documents describes an aircraft having an anti-torque tail rotor.
A main anti-torque device is thus still necessary, in particular at low speeds.
This is to prevent torque damage to the cable if the anti-torque system fails.
See also
Said anti-torque rotor 10 is preferably ducted in a fairing constituted by the base of the fin 9.
The present invention also provides a helicopter having such an anti-torque system.
Flights with main or anti-torque rotor defects ;.
The present invention relates to a compound aircraft having an additional anti-torque device.
There exist various configurations for main anti-torque devices for rotary wing aircraft.
This power necessary for flight is shared between the main rotor and the anti-torque rotor.
Bolt and tool with anti-torque features.
Figure 7 schematically shows the situation of interference between the first rotor and the anti-torque rotor.
Varying forces developed by an anti-torque device of the aircraft ;.
The tail anti-torque rotor is driven from a power take-off on the torsion shaft.
The hybrid helicopter therefore does not need to have an anti-torque tail rotor.
Furthermore, the helicopter 1 possesses an anti-torque rotor 4 arranged at the tail of the helicopter airframe.
At least one steering airfoil that is controllable and that generates anti-torque transverse thrust.
In the anti-torque mode of operation, controlling said second pitch using first control means ; and.
At least one steering airfoil of controllable steering and suitable for generating anti-torque transverse lift ;.
An anti-torque auxiliary rotor that is controllable and that exerts anti-torque lateral thrust ; and.
Rotary wing aircraft generally has a single main rotor and a single anti-torque tail rotor.
Reference flight with the defect-free main or anti-torque rotor adjusted to said reference adjustment ;.
Figure 7 graphically shows a case of interference between the helicopter 's first rotor and the anti-torque rotor.
Varying forces developed by an anti-torque device of the rotorcraft ;.
The anti-torque system comprises,.
Operation and effect of cyclic, collective and anti-torque controls.
Thus, the auxiliary, anti-torque rotor absorbs a fraction of the power available from said driving source.
The anti-splay device can also be anti-torque device.
An anti-torque system comprising,.
In some systems, the anti-splay device can also be anti-torque device.
Circulation-controlled anti-torque or circulation-controlled directional control systems " ;.
In some embodiments, the anti-splay device can also be anti-torque device.
Anti-torque spacer 42 also restricts the entry of outside elements into housing 27.
In some examples, the anti-splay device can also be anti-torque device.
Cat 7 " Circulation-controlled anti-torque or circulation-controlled direction control systems ".
Secondly by introducing defects into said defect-free main or anti-torque rotor ; and.
Main rotor and / or anti-torque system malfunction ( FFS or discussion only ).
Both secondary rear rods are mounted on the lower bracket through anti-torque controls ; and / or.
The bracket corresponding to the anti-torque structure 13 in FIG . 1 is therefore not required.
