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Quick actuating closure and handling systemA quick activating closure and handling system, which utilizes conical sections for locking, was developed to allow quick access to the combustor internal components of the 8 ft High Temperature Tunnel. These critical components include the existing methane spraybar, a transpiration cooled nozzle and the new liquid oxygen (LOX) injection system housed within the combustor. A substantial cost savings will be realized once the mechanism is installed since it will substantially reduce the access time and increase the time available for conducting wind tunnel tests. A need exists for more frequent inspections when the wind tunnel operates at the more severe conditions generated by using LOX in the combustor. A loads analysis and a structural (finite element) analysis were conducted to verify that the new closure system is compatible with the existing pressure shell. In addition, strain gages were placed on the pressure vessel to verify how the pressure shell reacts to transient pressure loads. A scale model of the new closure system was built to verify the operation of the conical sections in the locking mechanisms.
Document ID
19880012092
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Allred, Johnny W.
(NASA Langley Research Center Hampton, VA, United States)
White, Dorsey E., III
(NASA Langley Research Center Hampton, VA, United States)
Updike, Benjamin T.
(NASA Langley Research Center Hampton, VA, United States)
Gregory, Peyton B.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 5, 2013
Publication Date
May 1, 1988
Publication Information
Publication: The 22nd Aerospace Mechanisms Symposium,
Subject Category
Mechanical Engineering
Accession Number
88N21476
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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