Turbofan engine

Patent metadata

Field	Value
Publication number	US-10995633-B2
Application number	US-201916590560-A
Country	US
Kind code	B2
Filing date	Oct 2, 2019
Priority date	Sep 26, 2018
Publication date	May 4, 2021
Grant date	May 4, 2021

Abstract

A turbofan engine includes: a cylindrical fan case; a fan rotatably disposed in the fan case and including a central member and multiple fan blades arranged on an outer circumference of the central member such that the fan blades are spaced apart from one another in a circumferential direction; an annular member disposed to surround the fan; and an elastic support device that supports the annular member to the fan case radially elastically such that a predetermined clearance is radially defined between the annular member and tips of the fan blades.

First claim

The invention claimed is:

1. A turbofan engine, comprising:
a cylindrical fan case;
a fan rotatably disposed in the fan case and including a central member and multiple fan blades arranged on an outer circumference of the central member such that the fan blades are spaced apart from one another in a circumferential direction;
an annular member disposed to surround the fan; and
an elastic support device that supports the annular member to the fan case radially elastically such that a predetermined clearance is radially defined between the annular member and tips of the fan blades,
wherein the elastic support device further includes:
multiple spring members provided at multiple positions around a central axis of the fan case;
an annular recess formed on an inner circumferential surface of the fan case;
multiple pins provided at multiple positions around the central axis of the fan case and each having a base end fixed to a bottom of the annular recess and extending radially inward from the base end; and
multiple sliders each engaging a corresponding one of the pins so as to be movable in an axial direction of the pin,
wherein the spring members are constituted of compression springs provided for the respective pins such that each compression spring is disposed between a corresponding one of the sliders and the bottom of the annular recess and urges the slider into contact with an outer.

2. The turbofan engine according to claim 1 , further comprising a caulking part formed of a filler affixed to the fan case to fill a gap between the annular recess and the annular member.

3. A turbofan engine, comprising:
a cylindrical fan case;
a fan rotatably disposed in the fan case and including a central member and multiple fan blades arranged on an outer circumference of the central member such that the fan blades are spaced apart from one another in a circumferential direction;
an annular member disposed to surround the fan; and
an elastic support device that supports the annular member to the fan case radially elastically such that a predetermined clearance is radially defined between the annular member and tips of the fan blades,
wherein the elastic support device further includes:
multiple spring members provided at multiple positions around a central axis of the fan case;

an annular recess formed on an inner circumferential surface of the fan case;
multiple pins provided at multiple positions around the central axis of the fan case and each having a base end fixed to a bottom of the annular recess, extending radially inward from the base end, and having a free end provided with an enlarged diameter to form a flange; and
multiple sliders each engaging a corresponding one of the pins so as to be movable in an axial direction of the pin, with radially inward movement of the slider being restricted by the flange of the pin,
wherein the spring members are constituted of compression springs provided for the respective pins such that each compression spring is disposed between a corresponding one of the sliders and the bottom of the annular recess and urges the slider into contact with an outer.

Assignees

• Honda Motor Co Ltd

Inventors

• Kusakabe Yukio

Classifications

• F01D11/08 Primary

  for sealing space between rotor blade tips and stator (specially-shaped blade tips therefor F01D5/20) · CPC title

• F05D2240/14

  Casings or housings protecting or supporting assemblies within · CPC title

• F01D21/04

  responsive to undesired position of rotor relative to stator {or to breaking-off of a part of the rotor}, e.g. indicating such position · CPC title

• F01D11/22

  by mechanically actuating the stator or rotor components, e.g. moving shroud sections relative to the rotor · CPC title

• F05D2220/36

  specially adapted for the fan of turbofan engines · CPC title