Rotating structure and a method of producing the rotating structure
원문보기
IPC분류정보
국가/구분
United States(US) Patent
등록
국제특허분류(IPC7판)
F01D-005/30
B23P-015/00
F04D-029/32
출원번호
US-0886904
(2015-10-19)
등록번호
US-10099323
(2018-10-16)
발명자
/ 주소
Fanton, Bradley T.
Fulayter, Roy David
출원인 / 주소
Rolls-Royce Corporation
대리인 / 주소
McCracken & Gillen LLC
인용정보
피인용 횟수 :
0인용 특허 :
17
초록▼
According to one aspect, a rotating structure comprises a hub having a mounting slot defined by a cavity surface and a body having an anchor structure disposed in the mounting slot. A wear member is disposed between the anchor structure and the cavity surface and the wear member has at least first a
According to one aspect, a rotating structure comprises a hub having a mounting slot defined by a cavity surface and a body having an anchor structure disposed in the mounting slot. A wear member is disposed between the anchor structure and the cavity surface and the wear member has at least first and second portions of first and second material characteristics, respectively.
대표청구항▼
1. A rotating structure, comprising: a hub having a mounting slot defined by a cavity surface;a body having an anchor structure disposed in the mounting slot; anda wear member disposed between the anchor structure and the cavity surface,wherein the wear member has at least first and second portions
1. A rotating structure, comprising: a hub having a mounting slot defined by a cavity surface;a body having an anchor structure disposed in the mounting slot; anda wear member disposed between the anchor structure and the cavity surface,wherein the wear member has at least first and second portions of first and second material characteristics, respectively, the first material extends between inner and outer surfaces of the first portion, the second material extends between inner and outer surfaces of the second portion, and the wear member is disposed in the slot such that the outer surfaces of the first and second portions abut the cavity surface and the inner surfaces of first and second portions abut a surface of the anchor structure; andwherein each of the first and second portions includes first and second metals respectively. 2. The rotating structure of claim 1, wherein the wear member includes a transition from the first portion to the second portion and wherein the transition defines a line extending in an axial direction with respect to a longitudinal axis of the mounting slot. 3. The rotating structure of claim 1, wherein the wear member includes a transition from the first portion to the second portion and wherein the transition defines a line extending in a direction tangent to the cavity surface. 4. The rotating structure of claim 1, wherein the first portion includes a first material and the second portion includes a second material softer than the first material. 5. The rotating structure of claim 1, wherein the first and second metals comprise brass and steel, respectively. 6. The rotating structure of claim 1, wherein the anchor structure has one of a curved and a linear shape. 7. The rotating structure of claim 1, wherein at least one of a gradual and a discontinuous transition is disposed between the first portion and the second portion. 8. The rotating structure of claim 1, wherein each of the first and second portions includes first and second types, respectively, of a single metal wherein the first and second types have different moduli of elasticity. 9. The rotating structure of claim 1, wherein each of the first and second portions includes first and second materials, respectively, wherein each of the first and second materials comprises at least one of brass, bronze, steel, and a composite metallic material with nanovate coating. 10. The rotating structure of claim 9, wherein the wear member has a third portion separate from the first and second portions having one of the first and second characteristics. 11. The rotating structure of claim 9, wherein the first material is harder than the second material. 12. The rotating structure of claim 1, wherein the wear member covers at least one of a first side and a second side of the anchor structure. 13. A rotating structure, comprising: a turbomachine hub having a plurality of mounting slots each defined by a cavity surface;a plurality of rotatable fan blades each having an anchor structure disposed in an associated one of the mounting slots; andat least one wear member disposed between each anchor structure and the cavity surface defined by the associated mounting slot,wherein each wear member includes at least a first and a second material, each having different moduli of elasticity and disposed in respective discrete first and second portions of the wear member, the first material extends between inner and outer surfaces of the first portion, the second material extends between inner and outer surfaces of the second portion, and the wear member is disposed in the slot such that the outer surfaces of the first and second portions abut the cavity surface and the inner surfaces of first and second portions abut a surface of the anchor structure; andwherein each of the first and second portions includes first and second metals respectively. 14. The rotating structure of claim 13, wherein each of the at least two materials comprises at least one of brass, bronze, steel, and a composite metallic material with nanovate coating. 15. The rotating structure of claim 14, wherein the anchor structure has one of a curved and a linear shape. 16. The rotating structure of claim 15, wherein at least one of a gradual and a discontinuous transition is disposed between the at least two materials. 17. A method of producing a rotating structure having a rotatable member and a rotatable hub wherein an anchor member of the rotatable member is adapted for retention by a surface defining a slot in the hub, the method comprising the steps of: Determining stresses experienced by first and second anchor structure portions as a result of the hub rotating the rotatable member;Providing a wear member including first and second wear member portions made of first and second metallic materials, respectively, having different wear characteristics that are dependent upon the stresses, the first material extending between inner and outer surfaces of the first wear member portion, and the second material extending between inner and outer surfaces of the second wear member portion; andAssembling the anchor structure and the wear member in the slot so that the wear member is disposed between the anchor structure and the surface defining the slot and so that the outer surfaces of the first and second wear member portions abut the surface defining the slot and the inner surfaces of the first and second wear member portions abut a surface of the anchor structure. 18. The method of claim 17, wherein the step of providing the wear member comprises the step of producing at least one of a discontinuous and a gradual transition between the first and second wear member portions. 19. The method of claim 18, wherein the step of providing the wear member comprises the step of producing first and second wear member portions including first and second materials, respectively, wherein each of the first and second materials comprises at least one of brass, bronze, steel, and a composite metallic material with nanovate nickel coating.
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이 특허에 인용된 특허 (17)
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Herzner Fredrick C. (Fairfield OH) Juenger Jerome A. (Cincinnati OH) Wayte Peter (Cincinnati OH), Turbine blade wear protection system with multilayer shim.
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