IP Library › Granted Patent US 7,086,219
Granted Patent B2
US 7,086,219 · App. 11/036,075 · Granted Aug 8, 2006

Cowl structure for a gas turbine engine

Assignee: Rolls-Royce plc
View Patent ↗
Loading inventors, assignments & file history…
Monitor This Case
Get email alerts when status or documents change.
Order Certified Copies
Most orders are placed with the USPTO same day — all within 24 business hours.
Order via The Patent Place →
Pre-filled with this patent's details
Quick Facts
Patent No.
US 7,086,219
App. No.
11/036,075
Granted
Aug 8, 2006
Kind
B2
Abstract

A cowl structure ( 18 ) for a gas turbine engine ( 10 ) comprises an outer skin ( 26 ) defining a first path for a load applied to the engine ( 10 ). The cowl structure ( 18 ) includes an inner skin ( 24 ) defining a second path for the load. The inner and outer skins ( 24, 26 ) are constructed such that a major proportion of the load is transmitted along the first path.

Claims (2)

1. A cowl structure for a gas turbine engine, the cowl structure comprising inner and outer skins constructed such that at least a major proportion of a load applied to the cowl structure is transmitted along the outer skin, wherein the cowl structure has a principal axis and the inner skin includes first, second and third sections arranged adjacent and in axial alignment with each other parallel to the principal axis of the cowl structure, the first section being resiliently mounted intermediate the second and third sections by joint means, the joint means permitting relative movement between the sections and insulating the second section from the adjacent cowl structure, the joint means includes resilient urging means to allow said relative movement between the sections and urge the adjacent sections away from each other wherein the resilient urging means comprises spring means wherein the cowl structure further comprises internal surfaces across which air can pass in use, wherein the spring means extends substantially radially outwardly from the inner skin, to maintain alignment of the internal surfaces.

2. A cowl structure for a gas turbine engine, the cowl structure comprising inner and outer skins constructed such that at least a major proportion of a load applied to the cowl structure is transmitted along the outer skin, wherein the cowl structure has a principal axis and the inner skin includes first, second and third sections arranged adjacent and in axial alignment with each other parallel to the principal axis of the cowl structure, the first section being resiliently mounted intermediate the second and third sections by joint means, the joint means permitting relative movement between the sections and insulating the second section from the adjacent cowl structure, the joint means including resilient urging means to allow said relative movement between the sections and to urge the adjacent sections away from each other wherein the resilient urging means comprises spring means and wherein the spring means comprises a plurality of spring members spaced around the cowl structure at substantially regular intervals.

Priority Claims (1)
GB 0203447.8 · Feb 13, 2002 · national
Continuity (2)
Division 1036151100 · Feb 11, 2003
Related Publication 20050263643A1 · Dec 1, 2005