Fan case assembly of turbo fan engine

Patent metadata

Field	Value
Publication number	US-12560131-B2
Application number	US-202118283965-A
Country	US
Kind code	B2
Filing date	Mar 31, 2021
Priority date	Mar 31, 2021
Publication date	Feb 24, 2026
Grant date	Feb 24, 2026

Abstract

A fan case assembly of a turbo fan engine including a tubular fan case surrounding a fan of the turbo fan engine from an outside in a radial direction. The assembly also includes a tubular panel set covering an inner peripheral surface of the fan case and including panels lined up in an axial direction of the turbo fan engine and at least one elastic body compressed by two members selected from the fan case and the panels.

First claim

The invention claimed is:

1 . A fan case assembly of a turbo fan engine,
the fan case assembly comprising: a tubular fan case surrounding a fan of the turbo fan engine from an outside in a radial direction; a tubular panel set covering an inner peripheral surface of the tubular fan case such that a radial gap is formed overall between the tubular fan case and the tubular panel set, the tubular panel set including panels lined up in an axial direction of the turbo fan engine; and at least one elastic body compressed by two members selected from the tubular fan case and the panels, wherein: a linear expansion coefficient of the tubular fan case and a linear expansion coefficient of the tubular panel set are different from each other; the at least one elastic body includes a radial elastic body compressed by the tubular fan case and the tubular panel set in the radial direction; and the radial elastic body is a plate spring extending in the axial direction, the radial elastic body includes
an attaching portion attached to one of the tubular panel set and the tubular fan case,
an elastic portion that projects in the radial direction and compressed by the other of the tubular panel set and the tubular fan case in the radial direction, and
an end portion that is on the opposite side in the axial direction to the attaching portion and is slidable in the axial direction,
wherein one of the two members includes a stopper that limits elastic deformation of the radial elastic body; the stopper is located such that when the elastic portion is pressed radially, the end portion slides in the axial direction so as to approach the stopper and then the end portion contacts the stopper.

2 . The fan case assembly according to claim 1 , wherein:
the tubular panel set includes an attachment hole; and the attaching portion of the radial elastic body is attached to the tubular panel set with a fastener in the attachment hole of the tubular panel set.

3 . The fan case assembly according to claim 1 , wherein the at least one elastic body includes at least one axial elastic body compressed by the panels in the axial direction.

4 . The fan case assembly according to claim 3 , wherein:
the panels include
a first sound absorbing panel,
a second sound absorbing panel, and
a fan track liner panel located between the first sound absorbing panel and the second sound absorbing panel in the axial direction and opposed to the fan in the radial direction; and
the at least one axial elastic body includes a first axial elastic body compressed by the fan track liner panel and the first sound absorbing panel in the axial direction and
a second axial elastic body compressed by the fan track liner panel and the second sound absorbing panel in the axial direction.

5 . The fan case assembly according to claim 1 , wherein:
the tubular fan case includes
a fan case main body located outside the tubular panel set in the radial direction and
a front closing plate and a rear closing plate which are respectively located at a front end and a rear end of the tubular panel set in the axial direction and are fixed to the fan case main body; and
the at least one elastic body includes at least one axial elastic body compressed in the axial direction by two adjacent elements selected from the front closing plate, the panels, and the rear closing plate.

6 . The fan case assembly according to claim 5 , wherein:
the panels include
a first panel opposed to the front closing plate in the axial direction and
a second panel opposed to the rear closing plate in the axial direction; and
the at least one axial elastic body includes an axial elastic body compressed in the axial direction by the front closing plate and the first panel or compressed in the axial direction by the rear closing plate and the second panel.

Assignees

• Kawasaki Heavy Ind Ltd

Inventors

• Ando Takahiro
• Sasaki Hirokazu

Classifications

• F02C7/24

  Heat or noise insulation (air intakes having provisions for noise suppression F02C7/045; turbine exhaust heads, chambers, or the like F01D25/30; silencing nozzles of jet-propulsion plants F02K1/00) · CPC title

• F02K1/827

  Sound absorbing structures or liners · CPC title

• F01D25/28

  Supporting or mounting arrangements, e.g. for turbine casing · CPC title

• F05D2240/14

  Casings or housings protecting or supporting assemblies within · CPC title

• F01D21/045

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