NTL Record

Title Evaluation of a fiberglass instrument glare shield for protection against head injury.
Record ID 39183
Personal Name
Creator
Langston, E.D.; Swearingen, John J.
Corporate Creator Civil Aeromedical Institute
Corporate
Contributor
United States. Office of Aviation Medicine
Publisher Civil Aerospace Medical Institute
Publication Date 19720200
Language English
Abstract An all fiberglass prototype glare shield has been evaluated in terms of head injury protection. In 30-ft./sec. head impacts, a protrusion is designed to fold down over the heavy instruments, offering significant improvement in head injury protection when compared to current aircraft instrument panel design. Design changes to eliminate a fracture point and incorporation of fiberglass glare shields of similar design in future general aviation aircraft could lead to a significant reduction of head injuries during crash decelerations.
Rosap ID dot:20986
Rosap URL https://rosap.ntl.bts.gov/view/dot/20986
TRT Terms Air pilots; Crash injury research; Crash victim simulation; Head; Crash tests; Dummies; Sled tests; Deceleration; Instrument panels; Equipment design; Glare; Fiberglass; Laceration; Skull fractures; Fatalities; Velocity; Crashworthiness
General Subjects Air pilots; Crash injuries--Research; Crash test dummies; Acceleration (Mechanics); Aeronautical instruments; Airplanes--Windshields; Glare; Glass fibers--Impact testing; Skull--Fractures; Head--Wounds and injuries; Airplanes--Crashworthiness
Classification NTL - AVIATION - Aviation Safety/Airworthiness;
NTL - SAFETY AND SECURITY - Accidents;
NTL - SAFETY AND SECURITY - Aviation Safety/Airworthiness;
NTL - SAFETY AND SECURITY - Vehicle Design
Geographical
Coverage
United States
Report Number FAA-AM-72-7; DOT/FAA/AM-72/7
Resource type Tech Report
URL https://ntlrepository.blob.core.windows.net/lib/39000/39100/39183/AM72-07.pdf
Format PDF
Database NTL Digital Repository