Torso restraint with in flight and ejection activation modes
AssigneeThe Boeing Company
InventorGerald F. Herndon
Life of this patent
Estimating the term…
Loading patent…
AssigneeThe Boeing Company
InventorGerald F. Herndon
Estimating the term…
In the operation of modern tactical aircraft, crew members are subjected to periodic high acceleration loads that cause fatigue and a decrease in operating capacity. Restraining the torso of a crew member and pulling the crew member back against the ejection seat (2) of the aircraft would help prevent such fatigue. Known restraint and haul back apparatus for use during ejection are not adapted for repeated in flight use. The invention provides a single mechanism that retracts torso restraint straps (6) any number of times during in flight maneuvering and also retracts straps (6) for ejection. A loop (7) of each strap (6) extends around an inflatable member (28). When in flight acceleration loads exceed a preset limit, engine bleed air inflates member (28) to expand loops (7). This retracts straps (6) and positions the crew member. Member (28) is allowed to deflate when the acceleration subsides. When the ejection procedure is initiated, a gas generator (44) inflates member (28).
In a flight vehicle, apparatus for retracting a personnel torso restraint strap on a personnel carrier, said apparatus comprising:
In a flight vehicle, apparatus for retracting a personnel torso restraint strap on a personnel carrier, said apparatus comprising:
In a flight vehicle, a system for restraining and positioning the torso of a person situated in a personnel carrier, said system comprising:
A method of retracting a personnel torso restraint strap on a personnel carrier in a flight vehicle to restrain a person situated in the carrier, said method comprising:
A method of restraining and positioning the torso of a person situated in a personnel carrier in a flight vehicle, said method comprising:
In a flight vehicle, apparatus for retracting a personnel restraint strap on a personnel carrier, said apparatus comprising:
A method of retracting a personnel restraint strap on a personnel carrier in a flight vehicle to restrain a person situated in the carrier, said method comprising:
Dependencies are inferred from the claim text.