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©2010 Rolls-Royce Corporation The information in this document is the property of Rolls-Royce Corporation and may not be copied or communicated to a third.

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Presentation on theme: "©2010 Rolls-Royce Corporation The information in this document is the property of Rolls-Royce Corporation and may not be copied or communicated to a third."— Presentation transcript:

1 ©2010 Rolls-Royce Corporation The information in this document is the property of Rolls-Royce Corporation and may not be copied or communicated to a third party, or used for any purpose other than that for which it is supplied without the express written consent of Rolls-Royce Corporation. This information is given in good faith based upon the latest information available to Rolls-Royce Corporation, no warranty or representation is given concerning such information, which must not be taken as establishing any contractual or other commitment binding upon Rolls-Royce Corporation or any of its subsidiary or associated companies. EXPORT CONTROLLED NLR ECCN 9E991 Knowledge Fusion – Axial Requirements Roy Fulayter

2 Rolls-Royce data – strictly private EXPORT CONTROLLED NLR ECCN 9E991 2 These should be removed. These should be done before KF.

3 Rolls-Royce data – strictly private EXPORT CONTROLLED NLR ECCN 9E991 3 REMOVE rotation option, as it should be done before KF.

4 Rolls-Royce data – strictly private EXPORT CONTROLLED NLR ECCN 9E991 4 REMOVE flipping option, as it should be done before KF.

5 Rolls-Royce data – strictly private EXPORT CONTROLLED NLR ECCN 9E991 5 We need a selector box allowing.d.c format or xyz format. Currently only.d.c format (ver 1) works in UG6. We should be able to use our standard files like.d.c format! File should be externally converted before KF – Remove conversion

6 Rolls-Royce data – strictly private EXPORT CONTROLLED NLR ECCN 9E991 6 Defaults need to be reset to tangency

7 Rolls-Royce data – strictly private EXPORT CONTROLLED NLR ECCN 9E991 7 Additional Requirements Features should work in NX6 (be version independent) auto-population of an NX expression showing the axial location of the hot airfoil Comment the code where possible explaining each feature


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