Patrick Robert Oyler
Engineers in Sandy, UT
License number
Utah 168672-2202
Issued Date
Nov 8, 1989
Expiration Date
Mar 31, 2013
Category
Engineer/Land Surveyor
Type
Professional Engineer
Address
Address
Sandy, UT
Personal information
See more information about Patrick Robert Oyler at radaris.comName
Address
Phone
1424 Edgecliff Dr, Sandy, UT 84092
1424 E Edgecliff Dr, Sandy, UT 84092
Draper, UT
1424 Edgecliff Dr, Sandy, UT 84092
1738 Edgecliff Dr, Sandy, UT 84092
Professional information
Payload Fairing With Jettisonable Mass Acoustic Suppression
US Patent:
6394394, May 28, 2002
Filed:
May 9, 2000
Appl. No.:
09/567816
Inventors:
Richard L. Raun - Lindon UT
Patrick R. Oyler - Sandy UT
Bruce D. Hopkins - Salt Lake City UT
Patrick R. Oyler - Sandy UT
Bruce D. Hopkins - Salt Lake City UT
Assignee:
Alliant Techsystems Inc. - Edina MN
International Classification:
B64G 110
US Classification:
244158R, 244 1 N, 244121
Abstract:
A fairing for protecting a payload from excessive acoustic energy is disclosed. The fairing can be used with a launch vehicle for launching payloads such as satellites or the like. The invention provides structure to surround a payload and absorbs acoustic energy so that the noise is suppressed to acceptable levels and the payload is not damaged. The fairing comprises a two dimensional honeycomb core having composite face sheets and load skins bonded to each side of the core. A water barrier is connected to the inner side of the fairing to prevent moisture from entering the payload area. The fairing wall further includes a liquid which is added to the two dimensional honeycomb layer. The liquid is jettisoned during the launch of the vehicle at a predetermined time when the additional acoustic suppression provided by the mass of liquid is no longer needed. The fairing may also include an energy absorbing blanket connected to the inner side of the fairing to further suppress the energy generated by a launch vehicle.
Dry Preparation Of Particulate Solid Energetic Material
US Patent:
5501132, Mar 26, 1996
Filed:
Aug 31, 1994
Appl. No.:
8/298929
Inventors:
Clark C. de Nevers - Salt Lake City UT
Jeffrey L. Nelson - Kearns UT
Steven T. Newsome - Magna UT
Patrick R. Oyler - Sandy UT
Robert A. Patterson - West Jordan UT
Jeffrey L. Nelson - Kearns UT
Steven T. Newsome - Magna UT
Patrick R. Oyler - Sandy UT
Robert A. Patterson - West Jordan UT
Assignee:
Global Environmental Solutions, Inc. - Hopkins MN
Hercules Incorporated - Wilmington DE
Hercules Incorporated - Wilmington DE
International Classification:
F42B 3300, B26D 700, C06B 2100
US Classification:
86 24
Abstract:
Energetic material can be rapidly cut or machined at high speed in the substantial absence of liquid coolant with a cutting tool having a rotating cutting surface by maintaining a portion of the cutting surface out of contact with the energetic material and continuously removing the resulting reduced energetic material from the area of the cutting tool.
Payload Fairing With Improved Acoustic Suppression
US Patent:
6224020, May 1, 2001
Filed:
Dec 24, 1998
Appl. No.:
9/220495
Inventors:
Bruce D. Hopkins - Salt Lake City UT
Patrick R. Oyler - Sandy UT
Richard L. Raun - Lindon UT
Frank Jessen - Sandy UT
Patrick R. Oyler - Sandy UT
Richard L. Raun - Lindon UT
Frank Jessen - Sandy UT
Assignee:
Alliant Techsystems, Inc. - Hopkins MN
International Classification:
B64G 110
US Classification:
244158R
Abstract:
A fairing for protecting a payload from excessive acoustic energy is disclosed. The fairing can be used with a launch vehicle for launching payloads such as satellites or the like. The invention provides structure to surround a payload and absorbs acoustic energy so that the noise is suppressed to acceptable levels and the payload is not damaged. The fairing comprises a two dimensional honeycomb core having composite face sheets and load skins bonded to each side of the core. A water barrier is connected to the inner side of the fairing to prevent moisture from entering the payload area. The fairing may include an energy absorbing blanket connected to the inner side of the fairing to further suppress the energy generated by a launch vehicle.