AIR FORCE A-A-59863-2010 LINEAR AND ROTARY ELECTRO-MECHANICAL ACTUATOR TEST STAND (LREATS)《线性和旋转式电动机械动作器试验台(LREATS)》.pdf
《AIR FORCE A-A-59863-2010 LINEAR AND ROTARY ELECTRO-MECHANICAL ACTUATOR TEST STAND (LREATS)《线性和旋转式电动机械动作器试验台(LREATS)》.pdf》由会员分享,可在线阅读,更多相关《AIR FORCE A-A-59863-2010 LINEAR AND ROTARY ELECTRO-MECHANICAL ACTUATOR TEST STAND (LREATS)《线性和旋转式电动机械动作器试验台(LREATS)》.pdf(6页珍藏版)》请在麦多课文档分享上搜索。
1、 FSC 4920 Beneficial comments, recommendations, additions, deletions, clarifications, etc. and any other data that may improve this document should be sent to FSC: 4920 - 642 CBSG/GBEA, 460 Richard Ray Blvd, Suite 200, Robins AFB, GA 31098-1813. Since contact information can change, you may want to
2、verify the currency of this address information using the ASSIST Online database at https:/assist.daps.dla.mil/online/. A-A-59863 1 April 2010 COMMERCIAL ITEM DESCRIPTION LINEAR AND ROTARY ELECTRO-MECHANICAL ACTUATOR TEST STAND (LREATS) The General Services Administration has authorized the use of t
3、his commercial item description (CID), for all federal agencies. 1. Scope. This commercial item description covers a permanent back shop test stand designed to check the function of linear and rotary electro-mechanical actuators. The test stand should be capable of interfacing with 42 different actu
4、ators from seven different aircraft (C-5, C-141, F-15, F-16, KC-135, T-38, and T-39). The LREATS should be capable of accommodating the size, stroke length, physical mounting interface, and electrical connectors of each actuator. The LREATS should also be able to supply the correct power input type
5、and the precise amount of resistance to motion required for each individual actuator. 2. SALIENT CHARACTERISTICS. 2.1 Design. The LREATS design shall consist of a linear test stand (LTS), an instrument test stand (ITS), and a rotary test stand (RTS). 2.1.1 Linear test stand (LTS). The LTS shall be d
6、esigned with a hydraulic load cylinder and an adjustable mounting platform with mounting positions that will accommodate the load and stroke of the unit(s) under test (UUT). The LTS shall contain two sections; 0-5000 pounds of force (lbf) for high rated actuators and 0-1000 lbf for low rated actuato
7、rs. The LTS shall contain a hydraulic system capable of supplying hydraulic pressure to the load cylinder. 2.1.1.1 LTS physical characteristics (nominal). Length 128 inches Width 88 inches Height 63 inches Weight 3500 lbs INCH-POUND Provided by IHSNot for ResaleNo reproduction or networking permitte
8、d without license from IHS-,-,-A-A-59863 2 2.1.1.2 LTS power requirements. The LTS hydraulic system shall be powered by 3 phase, 220 VAC, 60 Hz power. The LTS control panel shall be powered by 1 phase, 120 VAC, 60 Hz power. 2.1.1.3 LTS performance characteristics (nominal). Speed of travel 5.5 inche
9、s per second Speed indicator 10 inches per second (maximum) Load Range 2 to 5000pounds (lbs). Stroke 24 inches (maximum) Max Actuator Length 53 inches Low force load cell 2 to 1000 lbs +/- 0.05% High force load cell 10 to 5000 lbs +/- 0.05% 2.1.1.4 Hydraulic system particulars (nominal). Hydraulic f
10、luid MIL-PRF-5606 Capacity 30 gallons Supply flow and pressure 5 gallons per minute (gpm) 825 pounds per square inch gauge (psig) (1000 psig max) 13.5 gpm 175 psig Operating temperature 100 165 degrees F Electric motor rating 5 HP 1800 revolutions per minute (rpm) Electric motor power 220/440 VAC, 6
11、0 Hz, 3 phase 2.1.2 Rotary test stand (RTS). The RTS shall be designed with an independent control panel which will be mounted onto a swing arm and shall provide the means to control and monitor the operation of each load system as well as torque and speed of the UUT. The RTS shall be designed with
12、a rotary test load fixture that includes two adjustable mounting facilities to test rotary devices. One of the two lighting facilities shall be capable of applying and measuring a 5 inch-pound torque (in-lbf) load and 0 - 25.000 rpm input. The second mounting facility shall be Provided by IHSNot for
13、 ResaleNo reproduction or networking permitted without license from IHS-,-,-A-A-59863 3 capable of applying and measuring a 200 in-lbf load and 0 - 2,000 rpm input. The RTS shall be designed to test one rotary device at any given time. The UUTs utilized with the rotary test load fixture must interfa
14、ce with the instrument test stand (ITS). 2.1.2.1 RTS physical characteristics (nominal). Length 38 inches Width 46 inches Height 72 inches Weight 600 lbs. 2.1.2.2 RTS performance characteristics. Speed Range 0 to 25,000 rpm Load Range 0-200 inch lbs (in-lbf) High Load Cell 0 to 200 in-lbf and 0-2000
15、 rpm Low Load Cell 0 to 5 in-lbf and 0 to 25,000 rpm High Load Transducer 200 in-lbf and 7,000 rpm Torque Break (low load) 0 to 5 in-lbf and 25000 rpm input capability Torque Break (high load) 0 to 200 in-lbf and 0 to 200 rpm 2.1.3 Instrument test stand (ITS). The ITS shall provide complete instrume
16、ntation for reading the results of the RTS and LTS. The ITS shall interface with the RTS and the LRS. The ITS shall provide means of energizing or de-energizing the system panels. The ITS shall provide complete instrumentation for controlling and monitoring the LTS and the RTS. The ITS shall have a
17、28 volts direct current (DC) section and connection in order to provide power to UUT when required. The DC section shall have display that will indicate when the DC circuit is activated, as well as display voltage and current reading. The ITS shall have an alternating current (AC) section and connec
18、tion provide 208VAC, 400 Hertz (Hz) power to the UUT. The ITS shall have the ability to adjust the AC voltage to the desired levels by the operator. The AC section shall have a display that will indicate AC voltage, current and power to the user. The AC sections shall allow for forward, reverse, and
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