IP Library › Granted Patent US 10,174,633
Granted Patent B2
US 10,174,633 · App. 14/928,322 · Granted Jan 8, 2019

Containment hook for composite fan case

Inventors: Christopher Hall (Indianapolis, IN); Benedict N. Hodgson (Indianapolis, IN)
Assignee: Rolls-Royce Corporation
F01D21/045B64D33/02F01D5/282F01D25/24F01D25/28F02C7/04F02C7/045F05D2240/14Y02T50/672
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Quick Facts
Patent No.
US 10,174,633
App. No.
14/928,322
Granted
Jan 8, 2019
Kind
B2
Abstract

According to one aspect, a fan blade containment apparatus for turbofan engines includes a containment hook and a fan case barrel. The containment hook and the fan case barrel are formed from composite materials, and the containment hook is attached to the fan case barrel such that the containment hook contains forward motion of a fan blade during a fan blade off event. The apparatus further includes the containment hook being arranged to shorten the axial length of the fan case barrel.

Claims (32)

1. A fan blade containment apparatus for turbofan engines, comprising:

a fan case barrel;

a fan track liner extending in an axial direction away from the fan blade; and

a containment hook attached to the fan case barrel by a first bond at an aft location and a second bond at a forward location, where the containment hook abuts the fan track liner, and the containment hook and the fan case barrel are formed from composite materials,

wherein the containment hook contains forward motion of a fan blade during a fan blade off event after the fan blade is trapped between the fan track liner and the fan case barrel; and

a forward acoustic panel abutting the containment hook and extending forward from the containment hook in the axial direction.

2. The fan blade containment apparatus of claim 1 , wherein the containment hook is bonded to the fan case barrel to form an overall hook shape; and

wherein the containment hook and the fan case barrel are configured to contain within the fan blade containment apparatus both forward axial motion and radial motion of the fan blade during the fan blade off event.

3. The fan blade containment apparatus of claim 2 , wherein the containment hook and the fan case barrel are manufactured separately such that the containment hook is inserted into the fan case barrel.

4. The fan blade containment apparatus of claim 2 , wherein the fan case barrel is manufactured first; and

wherein the containment hook is subsequently manufactured within the fan case barrel.

5. The fan blade containment apparatus of claim 1 , wherein the first bond at the aft location is placed such that the containment hook and the fan case barrel form an overall hook shape; and

wherein the second bond in the forward location spreads the load transfer across the fan case barrel.

6. The fan blade containment apparatus of claim 1 , wherein the composite material forming the containment hook and the fan case barrel is at least one of continuous carbon fiber, an epoxy matrix, and glass.

7. The fan blade containment apparatus of claim 1 , wherein the containment hook has at least one of a c-channel shape, a tee shape; shelf shape, a candy cane shape, a square shape, and a rectangular shape.

8. The fan blade containment apparatus of claim 7 , wherein the containment hook at least has the c-channel shape; and

wherein the containment hook is bonded to the fan case barrel at an aft location and a forward location such that the c-channel shape traps the fan blade at the aft bond location and the forward bond location assists in load transfer to the fan case barrel during the fan blade off event.

9. The fan blade containment apparatus of claim 1 , further comprising:

a forward acoustic panel face sheet, wherein the containment hook abuts the forward acoustic panel; and

wherein the containment hook is attached to the forward acoustic panel face sheet by a third bond.

10. A system for fan blade containment for turbofan engines, comprising:

a containment hook, a fan case barrel surrounding a plurality of fan blades, and a fan track liner extending in an axial direction away from the fan blades, the containment hook and the fan case barrel formed from composite materials, wherein the containment hook is attached to the fan case barrel by a first bond at an aft location and a second bond at a forward location, where the containment hook abuts the fan case barrel such that the containment hook contains forward axial motion and radial motion of a fan blade during a fan blade off event.

11. The system for fan blade containment of claim 10 , wherein the containment hook traps the fan blade between the fan track liner and the fan case barrel during the fan blade off event.

12. The system for fan blade containment of claim 11 , wherein the containment hook and the fan case barrel are manufactured separately such that the containment hook is inserted into the fan case barrel.

13. The system for fan blade containment of claim 12 , wherein the fan case barrel is manufactured first; and

wherein the containment hook is subsequently manufactured within the fan case barrel.

14. The system for fan blade containment of claim 10 , wherein the containment hook has at least one of a c-channel shape, a tee shape; shelf shape, a candy cane shape, a square shape, and a rectangular shape.

15. The system for fan blade containment of claim 10 , wherein the composite material forming the containment hook and the fan case barrel is at least one of continuous carbon fiber, an epoxy matrix, and glass.

16. The system for fan blade containment of claim 10 , further comprising:

a forward acoustic panel; and

a forward acoustic panel face sheet, wherein the containment hook abuts the forward acoustic panel and the containment hook abuts the fan track liner; and

wherein the containment hook is attached to the forward acoustic panel face sheet by a third bond.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Oct 30, 2015
From: HALL, CHRISTOPHER; HODGSON, BENEDICT N.
To: ROLLS-ROYCE CORPORATION
Reel/Frame 036926/0107 →
Continuity (1)
Related Publication 20170122126A1 · May 4, 2017
Cited By (2)
US 12,209,506 US 12,337,985