Fan containment cases for fan casings in gas turbine engines, fan blade containment systems, and methods for producing the same

Patent metadata

Field	Value
Publication number	US-9714583-B2
Application number	US-201414465098-A
Country	US
Kind code	B2
Filing date	Aug 21, 2014
Priority date	Aug 21, 2014
Publication date	Jul 25, 2017
Grant date	Jul 25, 2017

Abstract

Fan blade containment systems and methods for producing the same are provided. The fan blade containment system comprise a first ballistic material configured to be wrapped in overlapping layers around a fan casing to form a containment covering of a fan containment case for the fan casing. A plurality of patches comprised of a second ballistic material are configured to be loosely disposed between adjacent overlapping layers of the first ballistic material with each patch partially overlapping a circumferentially adjacent patch.

First claim

What is claimed is:

1. A fan blade containment system comprising:
a first ballistic material wrapped in continuous overlapping layers around a fan casing to form a containment covering of a fan containment case for the fan casing; and
a plurality of patches comprised of a second ballistic material, the plurality of patches loosely disposed between adjacent overlapping layers of the first ballistic material, with a majority of the plurality of patches positioned within a single revolution of the containment covering and each patch partially overlapping a circumferentially adjacent patch.

2. The fan blade containment system of claim 1 , wherein the first ballistic material includes fibers of a first fiber orientation and the second ballistic material includes fibers of a second fiber orientation that is different from the first fiber orientation.

3. The fan blade containment system of claim 2 , wherein the fibers of the first ballistic material are oriented in a different direction than the fibers of the second ballistic material to provide strength in different directions.

4. The fan blade containment system of claim 2 , wherein the first fiber orientation and the second fiber orientation differ by 90 degrees.

5. The fan blade containment system of claim 2 , wherein the first ballistic material includes fibers having a non-axial first fiber orientation and the second ballistic material includes fibers having an axial second fiber orientation.

6. The fan blade containment system of claim 1 , wherein the containment covering comprises the outermost covering of the fan containment case.

7. The fan blade containment system of claim 1 , wherein at least one patch of the plurality of patches is configured, when in a deployed condition, to move and occlude an opening at an impact location in the containment covering caused by impact of a released blade thereat.

8. The fan blade containment system of claim 1 , wherein each patch of the plurality of patches has a size that substantially matches an axial length of the containment covering.

9. The fan blade containment system of claim 1 , wherein each patch has opposed end portions, one of the end portions partially overlapping one of the end portions of the circumferentially adjacent patch between the pair of adjacent overlapping layers.

10. A fan containment case for a fan casing in a gas turbine engine, the fan containment case comprising:
a containment covering comprising continuous overlapping layers of a first ballistic material wrapped around the fan casing; and
a plurality of patches comprised of a second ballistic material, the plurality of patches positioned between a pair of adjacent overlapping layers with a majority of the plurality of patches positioned within a single revolution of the containment covering, each patch has opposed end portions, and one of the end portions partially overlaps one of the end portions of a circumferentially adjacent patch between the pair of adjacent overlapping lavers.

11. The fan containment case of claim 10 , wherein the first ballistic material includes fibers of a first fiber orientation and the second ballistic material includes fibers of a second fiber orientation that is different from the first fiber orientation.

12. The fan containment case of claim 11 , wherein the fibers of the first ballistic material are oriented in a different direction than the fibers of the second ballistic material to provide strength in different directions.

13. The fan containment case of claim 11 , wherein the first fiber orientation and the second fiber orientation differ by 90 degrees.

14. The fan containment case of claim 11 , wherein the first ballistic material includes fibers having a non-axial first fiber orientation and the second ballistic includes fibers having an axial second fiber orientation.

15. The fan containment case of claim 10 , wherein at least one patch of the plurality of patches is detached from the containment covering and is configured, when in a deployed condition, to move and occlude an opening at an impact location in the containment covering caused by impact of a released blade thereat.

16. The fan containment case of claim 10 , wherein each patch of the plurality of patches has a size that matches an axial length of the containment covering.

17. A method for producing a fan blade containment system, the method comprising:
wrapping a first ballistic material in continuous overlapping layers around a fan casing forming a containment covering; and
positioning a plurality of patches comprising a second ballistic material between a pair of adjacent overlapping layers of the containment covering with a majority of the plurality of patches positioned within a single revolution of the containment covering such that each patch partially overlaps a circumferentially adjacent patch and is detached from the containment covering.

18. The method of claim 17 , wherein the step of positioning a plurality of patches comprises positioning the plurality of patches such that at least one patch of the plurality of patches is configured, when in a deployed condition, to move and occlude an opening at an impact location in the containment covering caused by impact of a released blade thereat.

19. The method of claim 17 , wherein each patch has opposed end portions and the step of positioning a plurality of patches comprises positioning each patch such that one of the end portions of each patch partially overlaps one of the end portions of the circumferentially adjacent patch between the pair of adjacent overlapping layers.

Assignees

• Honeywell Int Inc

Inventors

• Watson Bill Russell

Classifications

• F05D2300/6034

  Orientation of fibres, weaving, ply angle · CPC title

• Y02T50/672

  Cross-Sectional Technologies · mapped topic

• F01D21/045 Primary

  special arrangements in stators or in rotors dealing with breaking-off of part of rotor · CPC title

• B23P15/04

  turbine or like blades from several pieces · CPC title

• Y02T50/60

  Efficient propulsion technologies, e.g. for aircraft · CPC title