Amsafe, Inc.

Amsafe, Inc. (phoenix Group)

Other

Todd Humbert

David T Merrill

Michael James Walton

Trenton Dirk Moeller

Ronald A Shields

Willard F Hagan

Peter Anthony Settles

Daniel Nick Foubert

William Joseph Gehret

Matthew James Browning

Richard Patterson

Louis Gregory Vargas

Elizabeth Humbert

Ken Spencer

A lift and tilt support apparatus includes opposed scissor lift assemblies. Each scissor lift assembly includes a base, an upper frame, and scissored first and second legs, each having opposed top and bottom ends. The bottom end of the first leg is pivoted to the base, and the top end of the first leg is mounted to the upper frame for reciprocal movement. The top end of the second leg is pivoted to the upper frame, and the bottom end of the second leg is mounted to the base for reciprocal movement. The top end of the first leg reciprocates in a direction skewed from the top end of the second leg. The bottom end of the second leg reciprocates in a direction skewed from the bottom end of the first leg.

Lift and tilt support apparatus

Various embodiments of vehicle occupant safety systems having extendable restraints for use with, for example, airbags are described herein. In one embodiment, for example, the disclosed technology includes a 2-point occupant restraint that secures an occupant in an aircraft seat. In this embodiment, the aircraft seat is positioned in a seating area that includes a forward monument housing a stowed airbag. In the event of a crash or other significant dynamic event that causes, for example, a rapid deceleration of the aircraft above a preset magnitude, the airbag deploys between the occupant and the monument as the dynamic forces cause the occupant to pitch forward. The forward momentum of the occupant's body creates a significant tension load in the 2-point restraint, which causes the restraint to extend by a preset amount, thereby allowing the occupant to move forward in the seat more than the occupant would have moved had the occupant been wearing a conventional, non-extending 2-point restraint. Although the occupant is allowed to move forward, the occupant remains secured to the extended restraint by means of non-extending webbing that is secured around the waist of the occupant. Allowing the occupant to move forward in this manner enables the occupant's upper torso to impact the airbag at a reduced or otherwise more favorable angle. This can reduce both the speed and the angle at which the occupant's head impacts the airbag, thereby reducing the likelihood of injury.

Occupant restraint systems having extending restraints, and associated systems and methods

Vehicle occupant restraint systems that include a compact, web-mounted airbag that can be deployed during a crash event are described herein. In some embodiments, the web (e.g., a shoulder belt) passes through the stowed airbag during normal use and, when the airbag inflates and deploys, the airbag extends along the length of the web (for example, along the entire length, or at least most of the length, of the web) to protect the occupant. In some embodiments, the restraint systems include shoulder belts having first and second overlapping web portions, and when the airbag inflates and deploys, the airbag extends along the length of the first web portion between the first web portion and the second web portion.

Extending pass-through airbag occupant restraint systems, and associated systems and methods

Active airbag vent systems and associated systems and methods are described herein. An airbag system having an active vent configured in accordance with an embodiment of the present technology can include, for example, a first inflator operably coupled to a first hose for inflating an airbag in response to a rapid deceleration event. The airbag system can further include a second inflator operably coupled to a second hose configured to release a vent or seam on the airbag to rapidly deflate the airbag after initial deployment of the airbag.

Active airbag vent system

Various embodiments of restraint system pretensioning devices for use in land, air, and sea vehicles are described herein. In one embodiment, a seat unit for use in a military land vehicle or helicopter includes a stroking device that enables the seat to move downwardly in response to sudden movement. The seat unit also includes a seat belt or harness that extends around the occupant in the seat. Sudden movement of the seat in response to an explosion or hard landing causes a pretensioning assembly to automatically pretension the seat harness.

Restraint system pretensioners

Apparatuses, devices and systems for attaching seatbelts to anchoring structures in aircraft and other vehicles, are described herein. In some embodiments, such apparatuses include a modular connector having a base configured to be attached to an anchoring structure, a body configured to be attached to a seatbelt, and an annular lock configured to releasably couple the body to the base. In these embodiments, the body carries the lock adjacent to an aperture configured removably receive the base. When the body is pressed over the base, the base passes into the aperture and contacts the annular lock, expanding the lock outwardly around the base. The base continues moving though the aperture in the body until the lock retracts into a groove in base, thereby releasaby locking the body to the base.

Seatbelt anchor systems for aircraft and other vehicles, and associated methods of manufacture and use

Buckle assemblies with dual release features and associated systems and methods are disclosed herein. In one embodiment, a buckle assembly is configured to detachably engage latch plates. The buckle assembly can include a top cover and a bottom housing collectively defining an operation space; a load plate having a plurality of apertures, an actuator configured to connect with the top cover, a plurality of pawls configured to operably enter the corresponding apertures so as to secure a plurality of latch plates, a release ring positioned adjacent to the pawls and connected with a release cord. The latch plates can be released by rotating the top cover or pulling the release cord.

Dual release buckle assemblies and associated systems and methods

Buckle assemblies with lift latches and associated systems and methods are disclosed herein. In one embodiment, a buckle assembly is configured to detachably engage at least one latch plate. The buckle assembly includes a cover, a load plate connected to the cover and formed with a plurality of openings, a shaft passing through the cover, a lift latch being operably rotated around the shaft in the operation space, and pawls selectively locking corresponding latch plates inserted in the openings in response to the rotation of the lift latch.

Buckle assemblies with lift latches and associated methods and systems

Various embodiments of seat harness pretensioning devices for use in land, air, and sea vehicles are described herein. In one embodiment, a seat unit for use in a military land vehicle or helicopter includes a stroking device that enables the seat to move downwardly in response to sudden movement. The seat unit also includes a seat belt or harness that extends around the occupant in the seat. Sudden movement of the seat in response to an explosion or hard landing causes a tensioning system to automatically pretension the seat harness.

Seat harness pretensioner

Tensioning apparatuses for occupant restraint systems and associated systems and methods. In one embodiment, an occupant restraint system for a vehicle can include a flexible web configured to extend across at least a portion of an occupant seated in the vehicle and an electrically actuated web retractor operably coupled to a proximal end portion of the web. The web retractor is configured to automatically wind and unwind the web. The system also includes an acceleration sensor operably coupled to the electrically actuated web retractor. The acceleration sensor is configured to send an electrical signal to the web retractor in response to a vehicle acceleration above a preset magnitude. In response to the signal, the web retractor is configured to (a) retract the web, and/or (b) at least temporarily prevent the web from moving inwardly or outwardly.

Tensioning apparatuses for occupant restraint systems and associated systems and methods

Buckle assemblies with swivel and dual release features and associated systems and methods are disclosed herein. In one embodiment, a buckle assembly is configured to detachably engage a web connector coupled to a first web. The buckle assembly includes a support structure coupled to a first release actuator, a second release actuator, and a swivel subassembly. The buckle assembly is configured to allow a user to detach the web connector from the buckle assembly via the first and/or second release actuators. Moreover, the swivel subassembly is configured to be coupled to a second web and to prevent the second web from twisting with reference to the buckle assembly.

Buckle assemblies with swivel and dual release features and associated methods of use and manufacture

Various embodiments of seat harness pretensioning devices for use in land, air, and sea vehicles are described herein. In one embodiment, a seat unit for use in a military land vehicle or helicopter includes a stroking device that enables the seat to move downwardly in response to an explosion or hard landing, respectively. The seat unit also includes a seat belt or harness that extends around the occupant in the seat. Downward movement of the seat in response to an explosion or hard landing causes a tensioning system to automatically pretension the seat harness.

The invention provides a cargo hook apparatus for securing cargo external to an aircraft for transportation, the apparatus comprising, pendent sling means, an attachment for securing the pendent sling means to the aircraft, and a cargo hook assembly, where the cargo hook assembly comprises a high-strength, lightweight alloy, and where the cargo hook assembly weighs less than about 55 pounds.

Growing community of inventors

Chandler, AZ, United States of America

Todd Humbert