Patents Assigned to Karem Aircraft, Inc.
  • Publication number: 20090226325
    Abstract: A spar of a rotor blade having moderate depth transitions to a relatively much deeper shank over a relatively short distance. This rapid transition enables a low-weight blade root that is structurally efficient, offers a high moment capability, and enables high Mach number axial flow. A transition could advantageously reduce section depth by at least 15%, 20%, 30%, or even 40% over at most 5%, 6%, 10%, or 12% of a total length of the rotor blade. Such a transition could advantageously be accomplished using a cuff, which has interfaces with each of the spar and the shank. The rotor blade shank has a generally circular cross-section which allows for a rotary attachment to a hub, where the attachment may advantageously comprise a mechanical or elastomeric bearing. Preferred embodiments have a spar with a generally rectangular cross-section.
    Type: Application
    Filed: March 4, 2009
    Publication date: September 10, 2009
    Applicant: KAREM AIRCRAFT, INC.
    Inventors: Neil Gupta, Abe Karem
  • Publication number: 20090224096
    Abstract: Systems and methods are provided in which an electrical control system independently effects acceleration of both driven and driving elements of a clutch to engage each other. In preferred embodiments the clutch is not a friction clutch, but a dog clutch, and forms part of a drive drain of a rotorcraft. A second clutch can be used, along with a mechanical interlock to prevent simultaneous engagement of the clutches. Speeds of the driven and driving elements can be sensed, and altered using at least one of a rotor, a brake, a generator, an electric motor, and a combustion motor.
    Type: Application
    Filed: March 6, 2009
    Publication date: September 10, 2009
    Applicant: KAREM AIRCRAFT, INC.
    Inventors: William Martin Waide, Abe Karem
  • Publication number: 20090227415
    Abstract: A gearbox comprising a gearset is able to transmit high output torques at high numerical reduction ratios at a power-to-weight ratio higher than previously attainable with existing designs. A distributor gear is disposed relative to a spur gear in order to produce automatic torque balancing. The distributor gear can be advantageously configured as an input floatring gear, for which support in all directions is provided by gear tooth mesh forces rather than bearings. Automatic torque balancing is achieved by configuring the distributor gear with first and second rows of helical teeth on the external circumference, and with a set of double helical teeth disposed on the internal circumference of the distributor gear. This allows for the placement of up to 50 or more planet gears in a countershaft arrangement with one end having helical teeth and the other end having spur teeth.
    Type: Application
    Filed: March 6, 2009
    Publication date: September 10, 2009
    Applicant: KAREM AIRCRAFT, INC.
    Inventor: Terry Buelna
  • Patent number: 7500935
    Abstract: Contemplated gearboxes combine a high numerical reduction ratio with the capability of transmitting power at a superior power-to-weight ratio using a compound star planetary gearbox configuration that is radially expanded using hollow driveshafts to link the planet gears. In most preferred compound planetary gear arrangements, planets of different diameter are torsionally connected to each other, or mesh with each other. Input and output gears counter-rotate while the planets rotate in bearings anchored to a static casing.
    Type: Grant
    Filed: June 23, 2006
    Date of Patent: March 10, 2009
    Assignee: Karem Aircraft, Inc.
    Inventor: William Martin Waide