Abstract:
A kit for building a mount assembly for securing a tubular member to a support structure of a gas turbine engine is described. The kit may comprise a base unit including a bottom surface configured to bond to the support structure and an upper portion with a concave surface. The kit may further comprise a first top unit including a first concave surface with a first diameter and a second top unit including a second concave surface with a second diameter that is smaller than the first diameter. The upper portion of the base unit may be configured to removeably connect to either of a selected one of the first top unit or the second top unit to provide the mount assembly.
Abstract:
An adapter for a gas turbine engine has a first portion with a control module mount interface. A second portion with a sensor mount interface defines a sensor mount position relative to a control module. A connecting body connects the first and second portions such that the second portion provides a re-orientated sensor mount position relative to the control module. A lubrication system for a gas turbine engine is also disclosed.
Abstract:
An adapter for a gas turbine engine has a first portion with a control module mount interface. A second portion with a sensor mount interface defines a sensor mount position relative to a control module. A connecting body connects the first and second portions such that the second portion provides a re-orientated sensor mount position relative to the control module. A lubrication system for a gas turbine engine is also disclosed.
Abstract:
A mount assembly is described. The mount assembly may comprise a base unit having a surface, an extension unit stacked on and connected to the surface, and a clamp unit stacked on and connected to the extension unit.
Abstract:
A mount assembly is described. The mount assembly may comprise a base unit having a surface, an extension unit stacked on and connected to the surface, and a clamp unit stacked on and connected to the extension unit.