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Evaluation of a head injury criteria component test device : final report / Richard L. DeWeese, David M. Moorcroft.

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Format:
Book
Government document
Author/Creator:
DeWeese, Rick
Contributor:
Moorcroft, David M.
United States. Office of Aerospace Medicine
United States. National Technical Information Service
Civil Aerospace Medical Institute
Language:
English
Subjects (All):
Airplanes--Seats--Safety measures--Evaluation.
Airplanes.
Head--Wounds and injuries--Prevention.
Head.
Craniocerebral Trauma--prevention & control.
Accidents, Aviation--prevention & control.
Aerospace Medicine--methods.
Equipment Design.
Evaluation Studies as Topic.
United States.
Medical Subjects:
Craniocerebral Trauma--prevention & control.
Accidents, Aviation--prevention & control.
Aerospace Medicine--methods.
Equipment Design.
Evaluation Studies as Topic.
United States.
Physical Description:
1 online resource
Place of Publication:
Washington, DC : Office of Aerospace Medicine ; Springfield, Va. : Available through the National Technical Information Services, [2004]
Summary:
Aircraft seats that are certified to meet the requirements of 14 CFR Parts 23.562, 25.562, 27.562 and 29.562 must protect the occupant from serious head injury as defined by the Head injury criterion (HIC). Currently this is demonstrated during a dynamic sled test that includes a 50% male-size test dummy, the seat, and any surrounding aircraft structure that could be impacted by the occupant's head. To reduce cost and expedite design and certification, a means of demonstrating compliance using a component-level test was desired. A project to develop a component test method was initiated by the FAA Technical Center's Materials and Structures Branch, under contract to the National Institute for Aviation Research (NIAR) at Wichita State University (WSU). This effort resulted in the development of the HIC Component Test Device (HCTD) as described in FAA report DOT/FAA/AR-02-99. The HCTD consisted of a test dummy head attached to a pivoted arm that is propelled in an arc by an air actuator. The device was transferred to CAMI in Dec. 2002 for evaluation and further development.
Notes:
Title from PDF title page (viewed July 14, 2006).
"November 2004."
"DOT/FAA/AM-04/18."
Includes bibliographical references.
Other Format:
Online version: DeWeese, Rick. Evaluation of a head injury criteria component test device.
OCLC:
70713400

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