Abstract: A combined anti-G and pressure suit intended for use in a high performance aircraft includes a helmet into which is fed respiratory air and a cooperating body suit comprised of a plurality of air-tight toroidal air segments which surround the wearer's body from the neck to the feet and which, independently, are pressurized so as to match the fluid pressure in each segment to body fluid pressures resulting from vertical accelerations of the aircraft.

Abstract: A flexible lower body negative pressure (LBNP) anti-G suit for protecting against the adverse effects of -G.sub.z acceleration is disclosed. Conventional anti-G suits protect against the adverse effects of +G.sub.z acceleration. Accelerations in the negative z direction, -G.sub.z, can also cause adverse physiological effects and, additionally, severely unpleasant subjective sensations. LBNP has been used in the past to alleviate the somewhat similar physiological effects of weightlessness in space. It has also been used with merely limited success to treat various medical problems. The present invention provides an improved LBNP suit that successfully alleviates the adverse physiological and subjective effects of -G.sub.z accelerations. Applying LBNP to an aircrew member increases venous vascular volumes in the lower body and reduces the otherwise increased pressures in the upper cardiovascular system.

Abstract: A method and apparatus for maintaining useful conciousness and reducing the risk of injury for a subject exposed to high levels of acceleration while in a vehicle. A buoyancy force suit is provided for supporting the subject with a buoyancy force. The buoyancy force suit includes at least two layers of flexible material, each layer being relatively impermeable to a substantially incompressible fluid locatable in a space between the layers. The suit fits over substantially the entire subject, including the subject's neck. A fluid reservoir is provided for maintaining a constant fluid level within the buoyancy force suit during acceleration. The fluid reservoir is supported at substantially the subject's eye level for maintaining an optimal fluid pressure gradient for ensuring an efficient blood supply to the subject's brain. Means are provided for securely suspending the buoyancy suit within the vehicle.

Abstract: A system and method for alerting a crew member if his anti-G system is not at the proper pressure during a flight. Flight condition sensors and an anti-G suit pressure sensor input data to a computer controller. The controller selects a pressure for protecting the crew member against blackout based on the input and data stored. The controller generates a signal to change the pressure in the anti-G suit to the selected pressure. The controller monitors the pressure status of the anti-G suit and rate of pressure change over time after the signal is generated. If the anti-G suit does not reach the selected pressure within a selected time, an alarm is provided to the crew member. Early warning, caution or failure alarms are generated if the suit does begin to inflate immediately or if it fails to reach a threshold pressure after a threshold time.

Abstract: A control system for an anti-G suit for aircraft pilots anticipates G-forces before they are incurred. The system has an available load circuit which receives the actual airspeed signal and computes an available load factor. The system is connected to the command stick of the pilot. The signal from the command stick is multiplied by the available load factor to provide an anticipated G-force. A selector monitors the actual acceleration with the anticipated signal and passes the higher of the two to a valve. The valve controls air pressure leading to the anti-G suit.

Abstract: A universal life support system adapted for use in an aircraft or spacecraft. The system includes components attached to the aircraft or spacecraft, components attached to the seat, and the ensemble to be worn. While appropriate gases and signals are sent between the craft and the seat, the seat connector at the suit side is adapted to receive any of the variety of connectors used with the ensembles that may be worn. While all potentially required gases, electrical signals, and electrical power are provided at the seat side of the seat-ensemble connection, the ensemble connector is configured to receive possibly only a subset of them. In addition, the ensemble connector can actuate a switch built into the seat connector to produce a signal indicative of the suit being worn. This signal provides information to the life support control system in the aircraft to cause the life support control system to adapt appropriate temperature and gas supply schedules.

Abstract: A G-protective ejection seat assembly for an occupant of the cockpit of an aircraft. The assembly includes a cradle having a rigid, non-articulated upper portion and a rigid lower portion pivotally attached to the upper portion. The upper portion is pivotally attached to the aircraft for selected angular movement within the cockpit between an upright position and a reclined position. The cradle upper portion includes arm rests movable therewith for supporting hand flight controls. Foot flight controls are mounted to the cradle lower portion which is formed by a pair of leg rests. The assembly includes a separable, non-articulated ejection seat removably carried by and stationary with respect to the cradle upper portion during non-ejection use. The seal is moved with the cradle upper portion as the cradle upper portion pivots between the upright and reclined positions.