Patents by Inventor Aleksey Kirillovich Shokurov

Aleksey Kirillovich Shokurov has filed for patents to protect the following inventions. This listing includes patent applications that are pending as well as patents that have already been granted by the United States Patent and Trademark Office (USPTO).

  • Aircraft with an integral aerodynamic configuration
    Patent number: 9180974
    Abstract: The invention relates to multimode aircraft operated at supersonic and subsonic flight speeds in a wide range of flight altitudes. The invention is particularly applicable in multimode super-maneuverable aircraft capable of cruising at supersonic speed and having low radar signature. The technical effect to be achieved by the invention is to provide an aircraft which has low radar signature, is super-maneuverable at high angles of attack, has high aerodynamic efficiency at supersonic speeds while keeping high aerodynamic efficiency at subsonic modes, and can accommodate bulky cargo in its internal compartments. The integral aerodynamic configuration aircraft comprises fuselage (1) with strake (2), wing with panels (3) smoothly blended into fuselage (1), all-moving horizontal tail (AMHT) (4), and all-moving vertical tail (AMVT) (5). Mid-fuselage is flattened and formed longitudinally by a set of aerodynamic profiles.
    Type: Grant
    Filed: April 7, 2011
    Date of Patent: November 10, 2015
    Assignee: OTKRYTOE AKCIONERNOE OBSCHESTVO “AVIACIONNAYA HOLDINGOVAYA KOMPANIYA SUHOI”
    Inventors: Mihail Aslanovich Pogosyan, Aleksandr Nikolaevich Davidenko, Mihail Yurievich Strelets, Vladimir Aleksandrovich Runishev, Aleksey Zaharovich Tarasov, Aleksey Kirillovich Shokurov, Sergey Yurievich Bibikov, Leonid Evgenievich Krylov, Pavel Borisovich Moskalev
  • AIRCRAFT WITH AN INTEGRAL AERODYNAMIC CONFIGURATION
    Publication number: 20140145027
    Abstract: The invention relates to multimode aircraft operated at supersonic and subsonic flight speeds in a wide range of flight altitudes. The invention is particularly applicable in multimode super-maneuverable aircraft capable of cruising at supersonic speed and having low radar signature. The technical effect to be achieved by the invention is to provide an aircraft which has low radar signature, is super-maneuverable at high angles of attack, has high aerodynamic efficiency at supersonic speeds while keeping high aerodynamic efficiency at subsonic modes, and can accommodate bulky cargo in its internal compartments. The integral aerodynamic configuration aircraft comprises fuselage (1) with strake (2), wing with panels (3) smoothly blended into fuselage (1), all-moving horizontal tail (AMHT) (4), and all-moving vertical tail (AMVT) (5). Mid-fuselage is flattened and formed longitudinally by a set of aerodynamic profiles.
    Type: Application
    Filed: April 7, 2011
    Publication date: May 29, 2014
    Inventors: Mihail Aslanovich Pogosyan, Aleksandr Nikolaevich Davidenko, Mihail Yurievich Strelets, Vladimir Aleksandrovich Runishev, Aleksey Zaharovich Tarasov, Aleksey Kirillovich Shokurov, Sergey Yurievich Bibikov, Leonid Evgenievich Krylov, Pavel Borisovich Moskalev