http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-4638791-A

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classificationCPCInventive http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64D10-00
classificationIPCInventive http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B64D10-00
filingDate 1985-07-22^^<http://www.w3.org/2001/XMLSchema#date>
grantDate 1987-01-27^^<http://www.w3.org/2001/XMLSchema#date>
inventor http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_d4fb0461d85a8eb38a5c1b0e3f451b9c
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_a305d760fa64c268b51bafce6d1da099
publicationDate 1987-01-27^^<http://www.w3.org/2001/XMLSchema#date>
publicationNumber US-4638791-A
titleOfInvention Apparatus and methods for providing rapid protection from accelerative forces experienced by aircraft crew members
abstract Apparatus and methods for increasing the tolerance level of an aircraft aircrew member to G forces by providing a rapid response to the onset of the normal accelerative forces to inflate an anti-G suit worn by the aircrew member. An electronic controller controls a servo valve which in turn controls a main valve for regulating the flow of gas into the inflatable G suit. The G suit is worn by the aircraft crew member to prevent pooling of blood in the lower portion of the body during aircraft maneuvers when G forces are experienced. The electronic controller receives a first input indicative of the amount of force applied to the control stick of the aircraft by the crew member, and a second input indicative of measured accelerative forces which are normal to the longitudinal axis of the aircraft. The electronic controller, preferably a microprocessor based controller, is responsive to the first input, and includes a programmable memory for storing data defining a schedule of the anticipated accelerative force levels which the aircraft will experience as a function of the applied control stick force. The microprocessor is programmed to decrease the anticipated accelerative force levels at a predetermined rate which is approximately equivalent to the rate of increase of measured accelerative forces. The anticipated force level is added to the actual accelerative force level to produce a command output for controlling the servo valve and/or for controlling a pressure regulator to initiate positive pressure breathing in a breathing device worn by the aircrew member.
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priorityDate 1985-07-22^^<http://www.w3.org/2001/XMLSchema#date>
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