Invention Grant
US08191254B2 Method and apparatus for improving fan case containment and heat resistance in a gas turbine jet engine
失效
一种用于改善燃气轮机喷气发动机中的风扇壳体容纳和耐热性的方法和装置
- Patent Title: Method and apparatus for improving fan case containment and heat resistance in a gas turbine jet engine
- Patent Title (中): 一种用于改善燃气轮机喷气发动机中的风扇壳体容纳和耐热性的方法和装置
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Application No.: US10947923Application Date: 2004-09-23
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Publication No.: US08191254B2Publication Date: 2012-06-05
- Inventor: Louis James Cardarella, Jr.
- Applicant: Louis James Cardarella, Jr.
- Applicant Address: US CA Paramount
- Assignee: Carlton Forge Works
- Current Assignee: Carlton Forge Works
- Current Assignee Address: US CA Paramount
- Agency: Konrad Raynes & Victor LLP
- Main IPC: F01D21/00
- IPC: F01D21/00 ; F02K3/04

Abstract:
A method and apparatus for improving fan case containment in a gas turbine jet engine employs a containment ring and a heat resistance ring which are shrink interference fit on the inside diameter of the fan case, the containment ring where the large fan blades turn, and the heat resistance ring where heated air from backfiring heats up the fan case. The containment ring is made of a super alloy to provide added strength to the fan case should a fan blade break, containing the fan blade within the fan case. The heat resistance ring is made of titanium or other suitable material. Additionally, one or more stiffener rings are shrink interference fit on the outside diameter of the fan case. The containment ring and stiffener rings can reduce the flight weight of the fan case and lower the material costs, while increasing the containment strength of the fan case.
Public/Granted literature
- US20060059889A1 Method and apparatus for improving fan case containment and heat resistance in a gas turbine jet engine Public/Granted day:2006-03-23
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