The proposed research effort shall explore a hybrid material approach to disk design by performing assessments of improvements, design trade studies, and design analyses. The effort shall include…

Ended Awarded Last action

Contract number
NNC14TA04T
Awardee
Awarding agency
Obligated
$680,744

Award facts

Contract value 100% obligated
$680,744.00 Current and potential, with all options
Completion date 100% complete
Current and potential, with all options
Set-aside
No set-aside
Competition
Full and Open Competition · 2 offers Multiple Award, Fair Opportunity
Pricing
Firm Fixed Price
Place of performance
Phoenix, AZ 85072, USA
Legislative mandates

Award details come from SAM.gov/FPDS.

Transactions

Action Obligated Date
Close Out 2 $0
Supplemental Agreement for work within scope 1 $0
Original award $680,744

Description

The proposed research effort shall explore a hybrid material approach to disk design by performing assessments of improvements, design trade studies, and design analyses. The effort shall include two phases, phase i design of a hybrid disk concept and phase II initial validation of hybrid disk design concept. The contractor shall perform conceptual design of a least one hybrid material disk made up of a powder metal superalloy and a single crystal superalloy. The contractor shall select a PM superalloy for the bore/web and a SX superalloy for the rim. The contractor shall then analyze the design(s) to determine the development path necessary to attain a technology readiness level of 5 for NASA consideration in future program planning. The contractor shall estimate improvements obtainable, including relative increases in compressor exit temperature, turbine inlet temperature, overall pressure ratio, and fuel efficiency for each proposed engine concept, using available and estimated material properties of a PM superalloy bore/web, combined with a SX superalloy rim. The long-term objectives for this research are to assess the operational benefits and limitations of hybrid material disks with the emphasis placed on: 1) quantifying improvements in compressor exit temperature, turbine inlet temperature, overall pressure ratio, and fuel efficiency possible for gas turbine engines having commercial applications relevant to NASA n+3 goals; 2) identifying the most beneficial hybrid materials, disk configuration, material processing and material slot/joining, material transition zone location and required properties and design considerations; 3) identifying the limiting properties and development path necessary to demonstrate a technology readiness level of 5.

Quick answers

Who was awarded contract NNC14TA04T?

NNC14TA04T was awarded to Honeywell International Inc. by Glenn Research Center (National Aeronautics and Space Administration) on June 25, 2014.

How much is contract NNC14TA04T worth?

The government has obligated $680,744 on NNC14TA04T.

Is contract NNC14TA04T an order under another contract?

Yes. NNC14TA04T is a delivery order under NNC10BA07B, an indefinite delivery contract, on Research and Technologies for Aerospace Propulsion Systems (RTAPS).

Was contract NNC14TA04T competed?

The extent of competition for NNC14TA04T was full and open competition. The government received 2 offers.

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