When.com Web Search

  1. Ad

    related to: helicopter rear rotors reviews

Search results

  1. Results From The WOW.Com Content Network
  2. Helicopter rotor - Wikipedia

    en.wikipedia.org/wiki/Helicopter_rotor

    The number of rotors is also important, many helicopters have two rotors in a single line, and another configuration is 4 rotors. [22] An example of two-blade rotor is the Bell 212 , and four blade version of this helicopter is the Bell 412 . [ 23 ]

  3. Tail rotor - Wikipedia

    en.wikipedia.org/wiki/Tail_rotor

    The tail rotor is powered by the helicopter's main power plant, and rotates at a speed proportional to that of the main rotor. In both piston and turbine powered helicopters, the main rotor and the tail rotor are mechanically connected through a freewheeling clutch system , which allows the rotors to keep turning in the event of an engine ...

  4. Tandem-rotor aircraft - Wikipedia

    en.wikipedia.org/wiki/Tandem-rotor_aircraft

    However, the rear rotor works in the aerodynamic shadow of the front rotor, which reduces its efficiency. This loss can be minimized by increasing the distance between the two rotor hubs, and by elevating one hub over the other. [4] [5] Tandem-rotor helicopters tend to have a lower disk loading than single-rotor helicopters. [6]

  5. Bell UH-1 Iroquois - Wikipedia

    en.wikipedia.org/wiki/Bell_UH-1_Iroquois

    The UH-1H's dynamic components include the engine, transmission, rotor mast, main rotor blades, tail rotor driveshaft, and the 42-degree and 90-degree gearboxes of the tail rotor. The main rotor transmission consists of a 90 degree bevel gear assembly with a reduction ratio of 2.14:1, followed by a 2-stage planetary gearset with a ratio of 9.53 ...

  6. Bell 429 GlobalRanger - Wikipedia

    en.wikipedia.org/wiki/Bell_429_GlobalRanger

    Data from Bell 429 brochure, Bell Helicopter 429 product specifications, Flug Revue Bell 429 page, Aviation Week General characteristics Crew: 1 pilot Capacity: 7 passengers (six in passenger compartment; one beside pilot) / 2,755 lb (1,250 kg) payload Length: 41 ft 8 in (12.70 m) Height: 13 ft 3 in (4.04 m) Cabin volume: 204 cu ft (5.78 m 3) Empty weight: 4,245 lb (1,925 kg) Max takeoff ...

  7. NOTAR - Wikipedia

    en.wikipedia.org/wiki/NOTAR

    NOTAR ("no tail rotor") is a helicopter system which avoids the use of a tail rotor. It was developed by McDonnell Douglas Helicopter Systems (through their acquisition of Hughes Helicopters ). The system uses a fan inside the tail boom to build a high volume of low-pressure air, which exits through two slots and creates a boundary layer flow ...

  8. Fenestron - Wikipedia

    en.wikipedia.org/wiki/Fenestron

    Ducted fan tail rotors have also been used in the Russian Kamov Ka-60 medium-lift helicopter, [17] and also on the Japanese military's Kawasaki OH-1 Ninja reconnaissance rotorcraft. French light helicopter manufacturer Hélicoptères Guimbal has also used a Fenestron for their Guimbal Cabri G2, a compact reciprocating engine-powered rotorcraft ...

  9. Blue Edge - Wikipedia

    en.wikipedia.org/wiki/Blue_Edge

    The Airbus Helicopters H160 with the new Blue Edge rotor design.. Blue Edge is an advanced design of rotor blade developed and produced by multinational helicopter manufacturer Airbus Helicopters in cooperation with the French aerospace laboratory ONERA and the German Aerospace Center, purposed to achieve a meaningful reduction in both noise emissions and vibration as well as enhancement in ...