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    1.
    发明专利
    未知

    公开(公告)号：DE06750638T1

    公开(公告)日：2009-02-26

    申请号：DE06750638

    申请日：2006-04-19

    Applicant: BELL HELICOPTER TEXTRON INC

    Inventor： STAMPS FRANK ,  RAUBER RICHARD

    IPC: B64C27/02 ,  B64C27/52

    Abstract: A torque coupling (13) for a rotor head (11) of a rotary-wing aircraft has upper and lower plates (29, 31) configured for rotation with a rotor mast (19). Drive links (33) pivotally connected to the upper and lower plates (29, 31) pivot about a pivot axis generally parallel to and radially offset from an axis of rotation of the plates. Each link (33) is engaged with adjacent drive links (33) to form a continuous ring of links, such that motion of one link (33) about its pivot axis causes motion in an opposite direction of each adjacent link (33) about its pivot axis. Drive elements (25) connect the drive links (33) to an assembly configured to receive rotor blades. The drive elements (25) may be components of a universal joint, a multiple trailing-link configuration, a pad-bearing configuration, or another type of articulating assembly.

    TORQUE COUPLING FOR ROTARY-WING AIRCRAFT
    2.
    发明专利
    TORQUE COUPLING FOR ROTARY-WING AIRCRAFT 未知

    公开(公告)号：CA2592947A1

    公开(公告)日：2007-06-07

    申请号：CA2592947

    申请日：2006-04-19

    Applicant: BELL HELICOPTER TEXTRON INC

    Inventor： STAMPS FRANK ,  RAUBER RICHARD

    IPC: B64C27/02 ,  B64C27/52

    Abstract: A torque coupling (13) for a rotor head (11) of a rotary-wing aircraft has upper and lower plates (29, 31) configured for rotation with a rotor mast (19). Drive links (33) pivotally connected to the upper and lower plates (29 , 31) pivot about a pivot axis generally parallel to and radially offset from an axis of rotation of the plates. Each link (33) is engaged with adjacent driv e links (33) to form a continuous ring of links, such that motion of one link (33) about its pivot axis causes motion in an opposite direction of each adjacent link (33) about its pivot axis. Drive elements (25) connect the dri ve links (33) to an assembly configured to receive rotor blades. The drive elements (25) may be components of a universal joint, a multiple trailing-li nk configuration, a pad-bearing configuration, or another type of articulating assembly.

    3.
    发明专利
    未知

    公开(公告)号：DE06849841T1

    公开(公告)日：2009-10-08

    申请号：DE06849841

    申请日：2006-10-12

    Applicant: BELL HELICOPTER TEXTRON INC

    Inventor： SMITH MICHAEL ,  STAMPS FRANK

    IPC: B64C27/04

    Abstract: A preferred embodiment of a pylon has six pylon mounting links for mounting the pylon to an airframe. Each link is considered near-rigid and has a spherical-bearing rod-end on both ends such that the link can only transmit axial loads. At least one of the links has a mass carried within the link and selectively moveable by an actuating means along the axis of the link in an oscillatory manner for attenuating vibrations traveling axially through the link. The actuating means may be an electromechanical, hydraulic, pneumatic, or piezoelectric system. By mounting each link in a selected orientation relative to the other links, the actuating means may be operated in a manner that attenuates axial vibration that would otherwise be transmitted through the link and into the airframe.

    TORQUE COUPLING FOR ROTARY-WING AIRCRAFT
    4.
    发明专利
    TORQUE COUPLING FOR ROTARY-WING AIRCRAFT 未知

    公开(公告)号：CA2592947C

    公开(公告)日：2011-10-11

    申请号：CA2592947

    申请日：2006-04-19

    Applicant: BELL HELICOPTER TEXTRON INC

    Inventor： STAMPS FRANK ,  RAUBER RICHARD

    IPC: B64C27/02 ,  B64C27/52

    Abstract: A torque coupling (13) for a rotor head (11) of a rotary-wing aircraft has upper and lower plates (29, 31) configured for rotation with a rotor mast (19). Drive links (33) pivotally connected to the upper and lower plates (29, 31) pivot about a pivot axis generally parallel to and radially offset from an axis of rotation of the plates. Each link (33) is engaged with adjacent drive links (33) to form a continuous ring of links, such that motion of one link (33) about its pivot axis causes motion in an opposite direction of each adjacent link (33) about its pivot axis. Drive elements (25) connect the drive links (33) to an assembly configured to receive rotor blades. The drive elements (25) may be components of a universal joint, a multiple trailing-link configuration, a pad-bearing configuration, or another type of articulating assembly.

    8.
    发明专利
    未知

    公开(公告)号：AT483957T

    公开(公告)日：2010-10-15

    申请号：AT01986156

    申请日：2001-12-12

    Applicant: BELL HELICOPTER TEXTRON INC

    Inventor： STAMPS FRANK ,  MARTIN RONNIE ,  BRASWELL JR

    IPC: G01L7/06 ,  F16F7/10 ,  F16F7/112 ,  F16F9/32 ,  G01L7/08 ,  G01L19/10 ,  G01L19/12 ,  H01H35/34

    Abstract: A pressure indicator (106) according to the present invention monitors the pressure of the fluid in a vessel (102). One embodiment of the present invention comprises a closed pressurized gas volume (210) behind a dimpled metal diaphragm (208). In normal operation, the force of the fluid pressure acting on the external surface of the diaphragm (208) to hold the diaphragm (208) in a concave geometry. In the event of a sufficient loss of fluid pressure, the force of the gas pressure acting on the internal surface of the diaphragm (208) will overcome the force of the fluid pressure acting on the external surface of the diaphragm (208), thereby moving the diaphragm (208) into a convex geometry. A viewing window (110) disposed in the side of the vessel (102) can be used to view the pressure indicator (106) and determine the shape of the indicator diaphragm (208).

    10.
    发明专利
    未知

    公开(公告)号：DE06733805T1

    公开(公告)日：2008-03-13

    申请号：DE06733805

    申请日：2006-01-24

    Applicant: BELL HELICOPTER TEXTRON INC

    Inventor： STAMPS FRANK ,  TISDALE PATRICK ,  SHERRILL PAUL ,  RAUBER RICHARD ,  CAMPBELL THOMAS ,  BRASWELL JAMES LEE JUN ,  MEASOM RON ,  HIROS TRICIA ,  POPELKA DAVID ,  SOUTHERLAND MICHAEL ,  STANNEY KEITH ,  WASIKOWSKI MARK ,  LEDBETTER TIM

    IPC: B63H1/06 ,  B63H5/125

    Abstract: An assembly for providing flexure to a blade of a rotary blade system includes an upper support plate having an upper curved surface, a lower support plate having a lower curved surface, and a yoke positioned therebetween. At least one of the upper and lower yoke surfaces has a layer of cushioning material positioned thereon and secured thereto. An alternate embodiment includes an assembly for providing flexure to a blade of a rotary blade system, including, an upper support plate having an upper curved surface, a lower support plate having a lower curved surface, and a yoke positioned therebetween and directly contacting the support plates wherein one of the curved surfaces is a non-circular arc that does not form part of the circumference of a circle. Another alternate embodiment includes a similar assembly having a twist-shank type of yoke for providing rotation of attached blades about their respective pitch axes.

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