SAE ARP 6166-2011 Minisimulator Method《微型模拟器法》.pdf
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1、_ SAE Technical Standards Board Rules provide that: “This report is published by SAE to advance the state of technical and engineering sciences. The use of this report is entirely voluntary, and its applicability and suitability for any particular use, including any patent infringement arising there
2、from, is the sole responsibility of the user.” SAE reviews each technical report at least every five years at which time it may be revised, reaffirmed, stabilized, or cancelled. SAE invites your written comments and suggestions. Copyright 2016 SAE International All rights reserved. No part of this p
3、ublication may be reproduced, stored in a retrieval system or transmitted, in any form or by any means, electronic, mechanical, photocopying, recording, or otherwise, without the prior written permission of SAE. TO PLACE A DOCUMENT ORDER: Tel: 877-606-7323 (inside USA and Canada) Tel: +1 724-776-497
4、0 (outside USA) Fax: 724-776-0790 Email: CustomerServicesae.org SAE WEB ADDRESS: http:/www.sae.org SAE values your input. To provide feedback on this Technical Report, please visit http:/www.sae.org/technical/standards/ARP6166 AEROSPACE RECOMMENDED PRACTICE ARP6166 Issued 2011-07 Reaffirmed 2016-09
5、Minisimulator Method RATIONALE ARP6166 has been reaffirmed to comply with the SAE five-year review policy. 1. SCOPE This test method is designed to simulate the synergistic combinations of oil flow, temperature cycling, hot spots, and tribology that would typically be found in a gas turbine engine.
6、The method is intended to quantitatively characterize changes in four basic oil properties that are brought about by exposure to the afore mentioned simulated turbine engine environment: the tendency of aviation lubricants to form coke deposits, viscosity changes, total acid number changes (TAN), an
7、d oil consumption. 2. APPLICABLE DOCUMENTS The following publications form a part of this document to the extent specified herein. The latest issue of SAE publications shall apply. The applicable issue of other publications shall be the issue in effect on the date of the purchase order. In the event
8、 of conflict between the text of this document and references cited herein, the text of this document takes precedence. Nothing in this document, however, supersedes applicable laws and regulations unless a specific exemption has been obtained. 2.1 SAE Publications Available from SAE International,
9、400 Commonwealth Drive, Warrendale, PA 15096-0001, Tel: 877-606-7323 (inside USA and Canada) or 724-776-4970 (outside USA), www.sae.org. ARP5088 Test Method for the Determination of Total Acidity in Polyol Ester and Diester Gas Turbine Lubricants by Automatic Potentiometric Titration 2.2 ASTM Intern
10、ational Publications Available from ASTM International, 100 Barr Harbor Drive, P.O. Box C700, West Conshohocken, PA 19428-2959, Tel: 610-832-9585, www.astm.org. ASTM D445-11 Standard Test Method for Kinematic Viscosity of Transparent and Opaque Liquids (and Calculation of Dynamic Viscosity) 2.3 U. S
11、. Government Publications Available from the Document Automation and Production Service (DAPS), Building 4D, 700 Robbins Avenue, Philadelphia, PA 19111-5094, Tel: 215-697-9495, https:/assist.daps.dla.mil/quicksearch/. FED-STD-791D Method 3410.1 High Temperature Deposit and Oil Degradation Characteri
12、stics of Aviation Turbine Oils SAE INTERNATIONAL ARP6166 Page 2 of 35 3. METHOD SUMMARY 3.1 Test Operation The minisimulator test method utilizes the minisimulator apparatus. The essential components of the minisimulator apparatus consist of a bearing housing, an oil circulation system with pump, va
13、rious heating elements and a motor to drive two test bearings residing in the bearing housing. The test apparatus is brought up to temperature, the oil flow is established, and the bearings are spun at the required speed. Conditions are maintained for 10 hours (1 cycle). The test is then shut down i
14、n reverse order and the apparatus is allowed to cool completely. This procedure is repeated 10 times. 3.2 Quantitative Characterization After each cycle of the test, oil is sampled. The viscosity and total acid number (TAN) are evaluated. After all ten cycles are completed, the apparatus is disassem
15、bled. The coke deposits on a variety of components are visually inspected and given a score. These scores are compiled into an overall score that is assigned to the test. Coupons of sample metals are placed in the oil sump to evaluate possible corrosive behavior. 4. MINISIMULATOR APPARATUS 4.1 Assem
16、bled Test Head The essential part of the minisimulator apparatus is the Assembled Test Head. Figure 1 shows an assembly drawing of the Assembled Test Head. Engineering drawings of all custom made components in the Assembled Test Head are shown in Appendix A. 4.1.1 The test bearings are two 30-mm bor
17、e angular contact ball bearings (Rolls-Royce Corp. part #6889093). 4.1.2 The thirteen (Figure 1 does not account for the four jets or the two additional ports in the middle of the head at 6:00 and 9:00) thermocouples are type J (Omega part #ICSS-18G-6). They are mounted to positions on the Test Hous
18、ing and the Rear End Cap via 1/8-inch male connectors that have been bored through (Swagelok part #SS-200-1-2BT). A spring washer is used to provide axial loading to the Test Bearings (comparable to Nested Spirawave, part number 12492-01 supplied by Smalley Steel Ring Company, Wheeling IL). The Forw
19、ard Test Bearing is secured by size W-04 lock washer and a size N-04 lock nut. The Rear Test Bearing is secured by the Bearing Retainer which attaches to the Drive Shaft by four cap screws (#3-48x3/8) 4.1.3 The oil jets are assembled into upper and lower pairs. All of the jets are connected to male
20、branch tee fittings (Swagelok SS-200-3TTM) that are screwed into female connectors (Swagelok SS-400-7-2). The upper jets are assembled by connecting the shorter jet tubes to a union cross fitting (Swagelok SS-400-4) using two short -inch sections of tubing. Similarly, the lower jets are assembled by
21、 connecting the longer jet tubes to a union tee fitting (Swagelok SS-400-3) again using two short -inch sections of tubing. The jets are connected to the test head via male connectors (Swagelok SS-200-1-2BT). 4.1.4 The air/oil drain line is attached to the Forward End Cap of the assembly by a male c
22、onnector (Swagelok part #SS-600-1-6). 4.1.5 The air/inert gas inlet is attached to the Forward End Cap of the assembly by male elbow (Swagelok part #SS-200-2-2). 4.1.6 The Forward and Rear End Caps are attached to the Test Housing via V-Band Clamps (Clampco part #994AR-0500). 4.1.7 The rod heater pl
23、aced on Rear End Cap of the assembly (hot spot heater) is rated at 240V/200W and should be the equivalent of Watlow part #J1E52KW24. The band heaters attached to the Test Housing are rated 240V/1000W and should be the equivalent of Watlow part #ME5A1JP8. 4.1.8 The O-ring on the Drive Shaft is size 1
24、15 and constructed from Viton A elastomer. SAE INTERNATIONAL ARP6166 Page 3 of 35 4.1.9 A pair of 1/8-inch stainless steel tube air cooling coils are not shown in Figure 1. Each coil makes six revolutions around the Test Housing. The coils were made by winding the 1/8-inch SS tubing around a circumf
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