Back to results
US 8,782,865 B2Granted
Combustor liner and flow sleeve tool
AssigneeGeneral Electric Company
InventorMustafa Gerengi
Life of this patent
Estimating the term…
Abstract
A tool includes an annular frame portion including a mount portion extending radially from the frame portion, a hook portion arranged on the mount portion, the hook portion sized and shaped to engage a member of a tubular component of a turbine combustor, and a force exertion portion arranged on the mount portion, the force exertion portion operative to engage a portion of the turbine combustor.
Claims12
A tool comprising:
- an annular frame portion including a mount portion extending radially from the frame portion;
- a hook portion arranged on the mount portion, the hook portion sized and shaped to engage a member of a tubular component of a turbine combustor;
- and
- a force exertion portion arranged on the mount portion, the force exertion portion operative to engage a portion of the turbine combustor, wherein the hook portion includes an aperture arranged in parallel to a rotational axis of the frame portion.
1 more element
Dependencies are inferred from the claim text.