[특허]Balance weight

Rolls-Royce Corporation

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특허 상세정보

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Balance weight

특허상세정보
국가/구분	United States(US) Patent 등록
국제특허분류(IPC7판)	B63H-007/00
미국특허분류(USC)	416/144;
출원번호	US-0421674 (2009-04-10)
등록번호	US-8322991 (2012-12-04)
발명자 / 주소	MacFarlane, Russel Engebretsen, Eric William
출원인 / 주소	Rolls-Royce Corporation
대리인 / 주소	Krieg DeVault LLP
인용정보	피인용 횟수 : 6 인용 특허 : 19

초록

A balance weight adapted to be assembled to a nose cone assembly of a turbine engine for improving a balance of the nose cone assembly is disclosed herein. The balance weight is one-piece and formed from a plurality of different materials including at least first and second materials. The first and second materials are arranged substantially heterogeneously relative to one another such that said first and second materials are separate from one another and fixed together.

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1. A balance weight adapted to be assembled to a nose cone assembly of a turbine engine for improving a balance of the nose cone assembly, said balance weight being one-piece and formed from a plurality of different materials including at least first and second materials arranged substantially heterogeneously relative to one another such that said first and second materials are separate from one another and fixed together. 2. The balance weight of claim 1 further comprising: a first body portion formed from said first material; and a second body portion formed from said second material, wherein said first and second body portions are joined to one another with adhesive. 3. The balance weight of claim 1 wherein further comprising: a first body portion formed from said first material and having a first volume; and a second body portion formed from said second material and having a second volume, wherein said first and second volumes are different from one another. 4. The balance weight of claim 1 wherein a density of said first material is at least twice a density of said second material. 5. The balance weight of claim 1 further comprising: a first body portion formed from said first material; and a second body portion formed from said second material, wherein said first and second body portions respectively include first and second apertures aligned along a common axis adapted to receive a fastener. 6. The balance weight of claim 1 wherein one of said first and second apertures includes a counter-sunk portion. 7. The balance weight of claim 1 further comprising a plurality of said balance weights, wherein a ratio of said first material relative to said second material varies between at least two of said plurality of balance weights to provide said at least two of said plurality of balance weights with different masses. 8. The balance weight of claim 1 further comprising a plurality of said balance weights, wherein each of said plurality of balance weights comprise: a first body portion formed from said first material; anda second body portion formed from said second material; andwherein a plurality of said first body portions are differently sized from one another. 9. The balance weight of claim 8 wherein a plurality of said second body portions are differently sized from one another. 10. A kit comprising: at least a plurality of balance weights each adapted to be assembled to a nose cone assembly of a turbine engine for improving a balance of the nose cone assembly, each of said plurality of balance weights being one-piece and formed from a plurality of different materials including at least first and second materials arranged substantially heterogeneously relative to one another such that said first and second materials are separate from one another and fixed together. 11. The kit of claim 10 wherein all of said plurality of balance weights are formed from the same combination of materials. 12. The kit of claim 10 wherein all of said plurality of balance weights are the same volumetric size and at least two of said plurality of balance weights include different ratios of said first and second materials. 13. The kit of claim 10 wherein each of said plurality of balance weights further comprise: a first body portion formed from said first material; anda second body portion formed from said second material, wherein a plurality of said first body portions are differently sized from one another. 14. The kit of claim 10 further comprising: a plurality of blanks each adapted to be assembled to the nose cone assembly of the turbine engine and substantially similarly shaped as said plurality of balance weights. 15. The kit of claim 10 wherein a density of said first material is at least twice a density of said second material. 16. The kit of claim 10 wherein a ratio of said first material relative to said second material varies between at least two of said plurality of balance weights to provide said at least two of said plurality of balance weights with different masses. 17. The kit of claim 10 wherein each of said plurality of balance weights further comprise: a first body portion formed from said first material; anda second body portion formed from said second material, wherein said first and second body portions respectively include first and second apertures aligned along a common axis adapted to receive a fastener and wherein one of said first and second apertures includes a counter-sunk portion. 18. The kit of claim 17 wherein a depth of said counter-sunk portion is the same for all of said plurality of balance weights. 19. The kit of claim 17 wherein said counter-sunk portion is formed the one of said first and second materials being easier to form. 20. A turbine engine comprising: a fan adapted for rotation about a centerline axis;a nose cone assembly coupled for rotation with said fan and having an outer surface defining at least part of a radially inner boundary of a fluid flow path into said fan; andat least one balance weight assembled to said nose cone assembly for improving a balance of said nose cone assembly, said balance weight being one-piece and formed from a plurality of different materials including at least first and second materials arranged substantially heterogeneously relative to one another such that said first and second materials are separate from one another and fixed together. 21. The turbine engine of claim 20 wherein said at least one balance weight is further defined as: a plurality of balance weights each including a first body portion formed from said first material and a second body portion formed from said second material, wherein a plurality of said second body portions are differently sized from one another. 22. The turbine engine of claim 20 wherein said first material is further defined as more brittle than the second material and is positioned radially inward of said second material. 23. The turbine engine of claim 20 wherein said first material is aluminum and said second material is tungsten. 24. The turbine engine of claim 20 wherein said at least one balance weight includes a first surface defining at least part of the radially inner boundary of the fluid flow path. 25. The turbine engine of claim 24 further comprising: a fastener adapted to couple said at least one balance weight to said nose cone assembly and including a second surface defining at least part of the radially inner boundary of the fluid flow path, wherein said outer surface and said first surface and said second surface are flush with one another.

이 특허에 인용된 특허 (19)

이 특허를 인용한 특허 피인용횟수: 6

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Balance weight

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Balance weight

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이 특허에 인용된 특허 (19)

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