|국가/구분||United States(US) Patent 등록|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 1 인용 특허 : 9|
A rotor assembly for a gas turbine engine includes a plurality of blades including a root portion and an airfoil portion. The rotor includes a plurality of slots that receive the root portion of a corresponding blade. The rotor includes an annular groove for a first and second retaining ring. The retaining rings are received within a common annular groove for holding each of the plurality of blades within the slots of the rotor.
1. A rotor assembly comprising: a plurality of blades including a root portion and an airfoil portion;a rotor including a plurality of slots for receiving the root portion of the plurality of blades, wherein the rotor includes a rotor alignment slot and an annular groove;a first retaining ring received within the annular groove;a second retaining ring received within the annular groove against the first retaining ring, wherein each of the first retaining ring and the second retaining ring includes a split enabling each of the first retaining ring and the...