Composite structure with load distribution devices, and method for making same

Patent metadata

Field	Value
Publication number	US-10030535-B2
Application number	US-201514802149-A
Country	US
Kind code	B2
Filing date	Jul 17, 2015
Priority date	Jul 17, 2015
Publication date	Jul 24, 2018
Grant date	Jul 24, 2018

Abstract

An improved composite structure and method for making same has been provided. The provided improved composite structure has locally strengthened areas within a reinforcement region. The locally strengthened areas within the reinforcement region have load distribution devices to redistribute load in order to (i) locally strengthen an area around damage induced by an initial momentary and direct transmitted load, and (ii) limit growth and propagation of damage induced by an initial momentary and direct transmitted load during a subsequent unbalance load. The improved composite structure reduces the impact of the fan blade out phenomenon in a weight efficient manner.

First claim

What is claimed is:

1. A method of manufacturing a fan case for a turbine engine, comprising:
fabricating a cylindrical casing comprising composite fibers such that a first fiber of the composite fibers has a first fiber axis oriented tangentially around the cylindrical casing, the cylindrical casing having a forward end, an aft end, and an axis;
determining an area on the cylindrical casing to be a reinforcement region, wherein the reinforcement region begins and ends aft of a fan containment housing;
disposing, within the reinforcement region, a plurality of load distribution devices (LDDs) that comprise composite fibers, the LDDs arranged axially within the reinforcement region such that, (i) for each LDD, a fiber of the composite fibers of the LDD has a fiber axis that is oriented to be within a range of plus or minus 30 degrees from perpendicular to the first fiber axis of the cylindrical casing, (ii) the plurality of LDDs does not cover more than 50% of the reinforcement region, (iii) each LDD of the plurality of LDDs is separated from each of its respective neighbor LDDs by a space, and (iv) the spaces between the LDDs are substantially equal.

2. The method of claim 1 , further comprising: coupling the plurality of LDDs to the cylindrical casing.

3. The method of claim 2 , wherein coupling the plurality of LDDs to the cylindrical casing comprises interleaving the plurality of LDDs within the composite fibers of the cylindrical casing.

4. The method of claim 2 , wherein coupling the plurality of LDDs to the cylindrical casing comprises applying an adhesive.

5. The method of claim 3 , wherein each of the plurality of LDDs comprises a predetermined width and a predetermined length, and wherein the predetermined length is about nine times the predetermined width.

6. The method of claim 2 , wherein the composite fibers of the LDD and the composite fibers of the cylindrical casing are the same.

7. The method of claim 1 , wherein, for each of the LDDs, the composite fibers of the LDD are braided.

8. A fan case assembly, comprising:
a cylindrical casing comprising composite fibers such that a first fiber of the composite fibers has a first fiber axis oriented tangentially around a circumference of the cylindrical casing, the cylindrical casing having a forward end, an aft end, an axis, a fan containment housing, and a region aft of the fan containment housing defined as a reinforcement region, wherein the reinforcement region begins and ends aft of the fan containment housing; and
a plurality of load distribution devices (LDDs) comprising composite fibers coupled to the reinforcement region, the LDDs disposed along the reinforcement region such that (i) for each LDD of the plurality of LDDs, a fiber of the composite fibers of the LDD has a fiber axis that is oriented to be within a range of plus or minus 30 degrees from perpendicular to the first fiber axis of the cylindrical casing, and (ii) the plurality of LDDs do not cover more than 50% of the reinforcement region, (iii) each LDD of the plurality of LDDs is separated from each of its respective neighbor LDDs by a space, and (iv) each of the spaces are substantially equal.

9. The fan case assembly of claim 8 , wherein the plurality of LDDs are coupled to the reinforcement region of the cylindrical casing by being interleaved into the composite fibers of the cylindrical casing.

10. The fan case assembly of claim 8 , wherein the plurality of LDDs are coupled to the cylindrical casing by applying an adhesive.

11. The fan case assembly of claim 8 , wherein the composite fibers of the LDD and the composite fibers of the cylindrical casing are the same.

12. The fan case assembly of claim 8 , wherein, for each of the LDDs, the composite fibers of the LDD are braided.

13. A method of manufacturing a composite structure, comprising:
fabricating a cylindrical casing comprising composite fibers such that a first fiber of the composite fibers has a first fiber axis oriented tangentially around the cylindrical casing, the cylindrical casing having a forward end, an aft end, and an axis;
determining an area on the cylindrical casing to be a reinforcement region, wherein the reinforcement region begins and ends aft of a fan containment housing;
interleaving into the reinforcement region a plurality of load distribution devices (LDDs) that comprise composite fibers such that, (i) each of the plurality of LDDs are substantially parallel to each other, and each are oriented to be within a range of plus or minus 30 degrees from perpendicular to the first fiber axis of the cylindrical casing, (ii) the plurality of LDDs do not cover more than 50% of the reinforcement region, (iii) each LDD of the plurality of LDDs is separated from each of its respective neighbor LDDs by a space, and (iv) each of the spaces are substantially equal.

14. The method of claim 13 , wherein each of the plurality of LDDs comprises a predetermined width and a predetermined length, and wherein the predetermined length is about nine times the predetermined width.

15. The method of claim 13 , wherein, for each of the LDDs, the composite fibers of the LDD are braided.

Assignees

• Honeywell Int Inc

Inventors

• Watson Bill Russell
• Braley Michael
• Roberts Gary

Classifications

• F01D5/282

  Selecting composite materials, e.g. blades with reinforcing filaments · CPC title

• F05D2300/603

  Composites; e.g. fibre-reinforced · CPC title

• B29C53/587

  having a non-uniform wall-structure, e.g. with inserts, perforations, locally concentrated reinforcements · CPC title

• B29C70/887 Primary

  locally reinforced, e.g. by fillers (filler concentrated near the surface B29C70/64) · CPC title

• F01D25/24

  Casings (modified for heating or cooling F01D25/14); Casing parts, e.g. diaphragms, casing fastenings (casings for rotary machines or engines in general F16M {; special arrangements in stators dealing with breaking-off of part of rotor F01D21/045}) · CPC title