SOLICITATION NOTICE
29 -- SENSOR,TEMPERATURE,
- Notice Date
- 9/14/2006
- Notice Type
- Solicitation Notice
- NAICS
- 336413
— Other Aircraft Parts and Auxiliary Equipment Manufacturing
- Contracting Office
- DEPARTMENT OF THE AIR FORCE; 3001 STAFF DR STE 2AG1 109B; TINKER AFB; OK; 73145
- ZIP Code
- 73145-3015
- Solicitation Number
- FA8104-06-R-0598
- Response Due
- 10/30/2006
- Point of Contact
- Thomas E Kanaly, Phone 405-734-8096, Fax 405-739-4237, Email thomas.kanaly@tinker.af.mil
- E-Mail Address
-
Thomas Kanaly
(thomas.kanaly@tinker.af.mil)
- Small Business Set-Aside
- N/A
- Description
- PR Number(s): 2915013432931PR, FA810406R0598 Item: 0001 NSN: 2915013432931PRPR SENSOR,TEMPERATURE, P/N: 1534M60P04, Description: Temperature is sensed by a helium-filled sensing coil acting upon sensing bellows attached to a metering valve. A second bellows is reference bellows. Pressurized helium gas in sensing coil reacts to temperature changes. When temperature increases, gas pressure increases. When temperature decreases, gas pressure decreases. Control servo pressure (PC) is supplied through a fixed orifice in main engine control. Pressure between fixed orifice and metering valve is P6 Pressure. Pressure (P6) is regulated to that required to overcome force of helium acting on sensing bellows, plus force of preload springs, plus force of bypass pressure (PD) acting on reference bellows. This interaction of forces regulats P6 at a constant value above PD at a constant value above PD at a given temperature. An increases in temperature expands helium gas in sensing coil and sensing bellows. As sensing bellows expands, opening at metering valve is decreased. A smaller amount of P6 is than blec to PD, thus increasing P6 pressure. A temperature decrease in helium-filled sensing coil causes gas to contract. As gas contracts, metering valve opens farther, bleeding more P6 pressure to PD, and P6 pressure decreases. The reference bellows allows for variations in PD and is used to maintain absolute pressure reference. FUNCTION: The sensor is a temperature sensor and transducer unit for main engine control. It responds to changes in fan discharge temperature and regulates pressure as a function of discharge temperature. DIMENSIONS: 'Sensor body/length 3.000inches, width 4.390 inches, height 2.400 inches. Temperature coil dimensions: length 7.188 inches, width 2.750 inches, height 2.750 inches, weight (dry) 2.82 lbs, signal pressures 24.1-182.4 PSI above main fuel pump boost pressure and proportional to temperature, filter screen size 70 microns (nominal), pressure line connection0.562-18 UNF-3A thread, temperature range -65F to 480F. MATERIAL: consists of aluminum exterior surfaces anodized per MIL-L-8625 class I Type II. Total Line Item Qty:10-20,21-32 Destn: FB2039,Tinker AFB,OK.,73145-9013. Delivery: 29DEC2006, 10.00 Destn: FB2039,Tinker AFB,OK.,73145-9013. Delivery: 29DEC2006, 21.00 Electronic procedure will be used for this solicitation. To: WOODWARD GOVERNOR COMPANY, LOVES PARK, IL.,61111-5800. Specifications, plans, or drawings relating to the procurement described are incomplete or not available and cannot be furnished by the Government. See Note(s) 26. NOTE: THIS NOTICE MAY HAVE POSTED ON FEDBIZOPPS ON THE DATE INDICATED IN THE NOTICE ITSELF (14-SEP-2006). IT ACTUALLY APPEARED OR REAPPEARED ON THE FEDBIZOPPS SYSTEM ON 01-FEB-2007, BUT REAPPEARED IN THE FTP FEED FOR THIS POSTING DATE. PLEASE CONTACT fbo.support@gsa.gov REGARDING THIS ISSUE.
- Web Link
-
Link to FedBizOpps document.
(http://www.fbo.gov/spg/USAF/AFMC/OCALCCC/FA8104-06-R-0598/listing.html)
- Record
- SN01224374-F 20070203/070201225906 (fbodaily.com)
- Source
-
FedBizOpps Link to This Notice
(may not be valid after Archive Date)
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