发明名称 |
CERAMIC CENTERBODY FOR AN AIRCRAFT GAS TURBINE ENGINE AND METHOD OF MAKING |
摘要 |
A ceramic centerbody (120) for an aircraft gas turbine engine. The ceramic centerbody (120) comprises an interlaced fiber structure having fibers oriented in a substantially transverse directions and a ceramic matrix surrounding the ceramic fiber structure. The ceramic fiber and matrix are formed into a conical shape having a fore end (128) and an aft end (126). The centerbody includes a means for mechanical attachment (130) circumferentially oriented around the fore end of the centerbody. The fore end further includes additional plies oriented in a third preselected direction, thereby providing additional strength to for mechanical attachment. |
申请公布号 |
WO2014058502(A3) |
申请公布日期 |
2014.07.17 |
申请号 |
WO2013US51201 |
申请日期 |
2013.07.19 |
申请人 |
GENERAL ELECTRIC COMPANY |
发明人 |
RENGGLI, BERNARD, JAMES;MILLER, JEFFREY, FRANKLIN |
分类号 |
B32B18/00;C04B35/18;C04B35/80;F02K1/04 |
主分类号 |
B32B18/00 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|