The tail boom includes a first side located on an opposite side of the tail boom from a second side of the tail boom.
The first side and the second side of the tail boom include asymmetrical surface profiles about a vertical plane of the tail boom.
Shafts in the tail boom, tail rotor, sufficiently reinforced tail boom design - another 400 kg.
Each tail boom supports a horizontal tail with an elevon (28) at its trailing edge.
The auxiliary tail rotor is collapsible within the tail boom of the helicopter when not in use.
A main rotor blade of the helicopter approaches the second side of the tail boom during rotation.
The method further includes securing a plurality of vortex generators to the first side of the tail boom.
Horizontal stabilisers were fitted each side of the tail boom.
The tail boom is equipped on the left side swept plumage.
Two sets of vanes deflect an air flow stream flowing along the tail boom respectively to opposed sides of the tail boom.
Thus the tailboom can pivotally couple with respect to the payload unit, which advantageously permits the tailboom to assume an orientation desirable for a particular mode of flight.
The underside of the fuselage and the right horizontal stabilizer were also substantially damaged.
The tail beam (205) is arranged on the imaging compartment (200) at a location away from the organic photo conductor drum (201).
The system of the present application includes a duct for receiving airflow from within a duct portion of a tailboom.
The system of the present application includes a duct for receiving airflow from within a duct portion of a tailboom.
The first and second horizontal airfoils extend outboard from the tailboom to provide aerodynamic pitch stability.
According to the invention, a collision avoidance apparatus is provided, which is designed to avoid a collision of a person with the tail jib (12).
A method, apparatus and computer program product for alerting the pilot of a helicopter of a possible tail strike hazard.
The tail boom has ellipse cross-section through which the stabilizer installed unmanaged type.
Since the parachute brake unit was removed, it was necessary to shorten the ending of the tail boom.
By design, the Mi-1 is a helicopter, made according to the classic single-rotor scheme with a tail rotor on the tail boom.
In turn, the fuselage includes four sections: a cockpit, a cargo and passenger compartment, a tail boom with vertical and horizontal flights.
Horizontal and vertical tail surfaces (138, 140) are located at the rear end of a boom assembly (120) rotatably connected to the fuselage (102).
Compared to the base model in the rotary wing extended tail boom and fuselage, increased the number of pucks and tail extended cab.
The tail boom had partially separated on the right side, near the attachment to the rear structure.
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,
Traduction Translation Traducción Übersetzung Tradução Traduzione Traducere Vertaling Tłumaczenie Mετάφραση Oversættelse Översättning Käännös Aistriúchán Traduzzjoni Prevajanje Vertimas Tõlge Preklad Fordítás Tulkojumi Превод Překlad Prijevod 翻訳 번역 翻译 Перевод