Containment hook for composite fan case

Patent metadata

Field	Value
Publication number	US-10174633-B2
Application number	US-201514928322-A
Country	US
Kind code	B2
Filing date	Oct 30, 2015
Priority date	Oct 30, 2015
Publication date	Jan 8, 2019
Grant date	Jan 8, 2019

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.

First claim

We claim:

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.

Assignees

• Rolls Royce Corp

Inventors

• Hall Christopher
• Hodgson Benedict N

Classifications

• F01D21/045 Primary

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

• F01D5/282

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

• F02C7/04

  Air intakes for gas-turbine plants or jet-propulsion plants · CPC title

• F05D2240/14

  Casings or housings protecting or supporting assemblies within · CPC title