AMI Industries, Inc. Patent applications |
Patent application number | Title | Published |
20150337576 | DEFORMABLE STOW BOX DOOR HINGE - As described herein, a hinge system may comprise one or more a guide wire hinges. In general, the guide wire hinges may be unitary members having a generally constant diameter. A pair of guide wire hinges may be utilized to hingeably couple a stow box door to the stow box housing. The hinge system may be configured to be deformable in response to experiencing a warping. | 11-26-2015 |
20150336675 | SEAT PAN CLOSURE MECHANISM - A seat closure and retention system comprising a spring, a retention device, a seat, and a housing is disclosed herein. The system may include a tapered ramp surface configured such that as the anchoring device, such as a spring loaded device, approaches a notch and/or bowl shaped portion based on movement of the seat from a substantially horizontal portion to a substantially vertical position. Stated another way, in response to the pin and/or ball of anchoring device making contact with the tapered ramp surface a damper effect is achieved. | 11-26-2015 |
20150320216 | SYSTEMS AND METHODS FOR RECLINING SEATS - Systems and methods are disclosed herein for reclining seats. A seat may have a seat back, a seat bottom, and a spine within the seat back and seat bottom. The seat bottom may be coupled to a base. The seat bottom may translate relative to the base. The seat may include a guide ramp coupled to the base. A portion of the spine may be located within the guide ramp. In response to translation of the seat bottom, the guide ramp may apply a torque on the spine, causing the seat back to recline. | 11-12-2015 |
20150054323 | EJECTION SEAT PAN LIFTER - An aircraft is provided and includes a fixed frame including a ledge and a seat pan on which seating elements for seating an aircraft crewperson are disposable. The seat pan includes a hinge about which the seat pan is pivotable relative to the fixed frame and a flange disposable on the ledge to establish a first pivot position for the seat pan relative to the fixed frame and a seat pan lifter coupled to the fixed frame and selectively interposable between the flange and the ledge to establish a second pivot position for the seat pan relative to the fixed frame. | 02-26-2015 |
20140327283 | VERTICAL SEAT MOTION LOCK - A vertical seat motion lock apparatus is provided and includes a seat base, a locking system coupled to the seat base and disposable in a locking position, at which the locking system is configured to permit upward seat base movement and to prevent uncommanded downward seat base movement, and an unlocked position and a control system coupled to the locking system, the control system being biased to cause the locking system to assume the locking position and configured to be selectively actuated to cause the locking system to assume the unlocked position. | 11-06-2014 |
20120199695 | SELF-STOWING JUMPSEAT FOR AIRCRAFT - A self-stowing jumpseat consists of a seat frame that is deployed by pulling the seat frame out of a pocket formed in the edge of a bulkhead. Once the seat frame has been deployed and locked in position, the seat pan is folded down to enable a user to be seated. The seat pan is spring-loaded to fold up, so that when the user vacates the seat, the seat pan automatically folds up into the closed configuration. As it does so, an interlock lever attached to the seat pan trips the seat frame locks from their locked to their unlocked positions. The seat frame has a retraction mechanism that urges the seat into the pocket. Accordingly, as soon as the seat pan interlock lever releases the seat frame locks, the retraction mechanism causes the folded seat frame to move into the stowed position within the bulkhead. | 08-09-2012 |
20110114790 | PASSIVE EJECTION SEAT ARM FLAIL RESTRAINT APPARATUS AND METHOD - An ejection seat arm flail injury prevention apparatus comprises a pair of rigid support arms on each side of the ejection seat that deploy outwardly to support a semi-rigid backstop substantially behind the ejection seat occupant. When the ejection seat is propelled out of the aircraft and is subjected to the windblast, the occupant's arms are allowed to flail in a rearward direction in the windblast until the occupant's arms impact the semi-rigid backstop. The backstop is semi-rigid in that it deforms sufficiently to enable the rearward motion of the occupant's arms to be arrested without impact injury, yet is sufficiently rigid to prevent the occupant's arms from rebounding off the backstop or striking the rigid support arms. | 05-19-2011 |
20110084167 | AIRCRAFT EJECTION SEAT WITH MOVEABLE HEADREST - An ejection seat includes a headrest that, upon initiation of the ejection seat, moves forward to support the pilot's head in a tilted-forward position. By holding the crewmember's head in a tilted-forward position, windblast forces are controlled to prevent the helmet from pulling upward and backward on the crewmember's head. The headrest may include a pair of struts that extend forward around the sides of the crewmember's helmet to support the crewmember's head against flailing from the windblast. A flexible panel extending between the struts and the headrest panel may also be included to further support the crewmember's head against windblast flailing. | 04-14-2011 |
20110068229 | AIRCRAFT EJECTION SEAT WITH PASSIVE LIMB RETENTION - An aircraft ejection seat includes a passive limb retention system. The limb retention system comprises a primary lanyard that forms a loop around the crewmember's footwell and a secondary lanyard that is releasably attached to a medial portion of the loop in the primary lanyard. Upon initiation, as the ejection seat is propelled out of the aircraft, the primary and secondary lanyards simultaneously close the lanyard loop around the crewmember's leg from both ends until the lanyard loop contacts the crewmember's leg. Once the lanyard loop is closed around the crewmember's leg, the secondary lanyard releases, allowing the primary lanyard to continue to tighten around the crewmember's leg until the shear fastener shears and the ejection seat exits the aircraft. | 03-24-2011 |
20110062286 | AIRCRAFT EQUIPMENT SUPPORT - An equipment support for attaching equipment to an aircraft comprises a gripper foot having a T-shaped slot that engages a track mounted to the aircraft floor. The gripper foot is mounted to a trunnion mount that enables the gripper foot to rotate freely about a vertical axis so that the gripper foot can negotiate curves along a non-linear track. The trunnion mount is mounted to the equipment support frame by means of a horizontal pivot. The horizontal pivot is held against rotation below a predetermined load by a torque-resisting element. If the floor track is warped, for example during a crash, the twisting loads transmitted from the floor track to the gripper foot overcome the torque-resisting element, which allows the trunnion mount and gripper foot to rotate with the floor track thereby allowing the gripper foot to remain attached to the track without imparting excessive loads on the track, gripper foot, or equipment support frame. | 03-17-2011 |
20110049960 | AIRCRAFT SEAT WITH ADJUSTABLE ARMREST - An aircraft seat has an adjustable armrest in which the armrest platform is supported by a hinged attachment to an armrest support member. The hinged attachment between the armrest platform and the arm support member is located at the wrist-end of the arm support member near the aircraft control stick. The armrest platform and the armrest support are locked into position by means of telescoping struts that are controlled at the wrist-end of the arm platform member. The telescoping struts can be selectively locked to create triangular and/or quadrilateral trusses that lock the armrest firmly into position and may include springs or other elements to bias the armrest platform up and forward so that the armrest “floats” when the telescoping struts re released. | 03-03-2011 |
20100155535 | AIRCRAFT EJECTION SEAT WITH MOVEABLE HEADREST - An ejection seat includes a headrest that, upon initiation of the ejection seat, moves forward to support the pilot's head in a tilted-forward position. By holding the crewmember's head in a tilted-forward position, windblast forces are controlled to prevent the helmet from pulling upward and backward on the crewmember's head. The headrest may include a pair of struts that extend forward around the sides of the crewmember's helmet to support the crewmember's head against flailing from the windblast. A flexible panel extending between the struts and the headrest panel may also be included to further support the crewmember's head against windblast flailing. | 06-24-2010 |
20100148552 | CUSHION FOR AIRCRAFT EJECTION SEAT - A seat cushion for an aircraft seat includes a plurality of rear edge securing straps attached to the lower surface of the seat cushion. The rear edge securing straps each have a free end that includes a pull-the-dot fastener that engages a corresponding pull-the-dot fastener at the rear edge of the seat pan. The length of the rear edge securing straps is selected so that when the seat cushion is installed, the rear edge securing straps are pulled substantially flat so that the seat cushion is firmly held in place. The seat cushion is easily removable because the pull-the-dot fasteners are at the ends of the rear edge securing straps rather than affixed directly to the bottom of the seat cushion. Therefore, when the front edge of the seat cushion is released, the seat cushion can be lifted up enough to allow the cushion to be released without pulling at the bottom of the seat cushion. | 06-17-2010 |
20090045285 | AIRCRAFT EJECTION SEAT WITH MOVABLE HEADREST - An ejection seat includes a headrest that, upon initiation of the ejection seat, moves forward to support the pilot's head in a tilted-forward position. By holding the crewmember's head in a tilted-forward position, windblast forces are controlled to prevent the helmet from pulling upward and backward on the crewmember's head. The headrest may include a pair of struts that extend forward around the sides of the crewmember's helmet to support the crewmember's head against flailing from the windblast. A flexible panel extending between the struts and the headrest panel may also be included to further support the crewmember's head against windblast flailing. | 02-19-2009 |
20080238124 | SEAT TRACK LOCKING MECHANISM - An apparatus for adjusting the position of a seat comprises a rack and a clock nut that grips the rack. The rack comprises a threaded rod, while the clock nut comprises a short cylindrical body that is drilled and threaded along its diameter with internal threads corresponding to the thread diameter and pitch of the rack. Circumferential reliefs are then formed in the threaded bore to enable the clock nut to be “clocked” from a position in which the threads of the clock nut engage the threads of the rack to a second position in which the threads of the clock nut disengage the threads of the rack. A pair of linkages are provided to rotate the clock nut between the engaged and disengaged positions and to transmit loads from the clock nut. Because the clock nut engages multiple teeth of the rack simultaneously, the seat track locking mechanism of the present invention is capable of extremely fine position adjustment without sacrificing ruggedness and because of the design of the linkages, the seat track locking mechanism locks bi-directionally and with little or no backlash. | 10-02-2008 |
20080237398 | AIRCRAFT EQUIPMENT SUPPORT - A support for aircraft seats and other equipment has a lower support link that sweeps out a lateral arc. The lower support link supports a platform that may have a conventional linear track. The linear track provides fore/aft movement substantially orthogonal to a line tangent to the center of the lateral arc. A pilot link is attached to the platform to form a parallelogram linkage that maintains the equipment platform in a rotationally fixed attitude as the lower support link sweeps out its lateral arc. | 10-02-2008 |