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A -- On-Board Turbine Blade Health Sensor

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Reference-Number-RFI-5-17-04-PRKFederal

Contract Overview

Solicitation details, issuing organization, response deadlines, documents, and interested companies for this government contract opportunity.

AI Contract Overview

The Request for Information seeks a non-developmental engine diagnostic system designed to monitor blade tip frequency responses in the Pratt & Whitney F100 engine, utilized in USAF F-15 and F-16 fighter aircraft. The system must detect and provide warnings of changes caused by pre-critical low cycle fatigue and transient high cycle fatigue cracks by integrating real-time sensor data with advanced predictive algorithms. Key requirements include the system being self-contained, capable of operating independently from existing engine controls, and able to function reliably within the harsh engine environment characterized by extreme temperatures up to 1500°C, pressures up to 10 MPa, and vibrations up to 15g. Respondents must demonstrate prior system deployment on similar multi-aircraft fleets and have the technical skills necessary for system integration, fabrication, performance verification, data analysis, and reporting related to the F100 engine. The solicitation clarifies that no contract award is anticipated directly from this RFI; it is aimed at gathering market capabilities and information for future planning. Participation is voluntary, and respondents will not receive compensation. Interested parties are encouraged to submit detailed descriptions of their non-developmental diagnostic systems, limited to eight pages, by the specified due date. Points of contact are provided for communications and submission, ensuring that relevant technical expertise is accessible throughout the process. This initiative underscores the Department of Defense’s emphasis on advancing engine health monitoring technologies to enhance the operational readiness and safety of fighter aircraft powered by the F100 engine.

General Info

Seeking non-developmental diagnostic system for F100 engine fatigue detection, self-contained, high-temperature tolerant.

Agency

Department Of Defense → FA8650 USAF Afmc Afrl Pzl Afrl/pzl

NAICS

334513 - Instruments and Related Products Manufacturing for Measuring, Displaying, and Controlling Industrial Process Variables

Place of Performance

Set-Aside

NONE

Documents

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Timeline

PostedMay 17

special-notice

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Organization & Contact Information

AgencyDepartment Of Defense → FA8650 USAF Afmc Afrl Pzl Afrl/pzl

Contacts2 people available

OfficeWRIGHT PATTERSON AFB, OH, 45433-7541, USA

Organization / AgencyDepartment Of Defense → FA8650 USAF Afmc Afrl Pzl Afrl/pzl

Office AddressWRIGHT PATTERSON AFB, OH, 45433-7541, USA

Contacts

Brian W AllportContract Negotiator

contact@example.gov

+1 (555) 000-0000

Bruce J MillerContracting Officer

contact@example.gov

+1 (555) 000-0000

Full Description

This Request for Information (RFI) is for a non-developmental engine diagnostic system for monitoring blade tip frequency response in the Pratt & Whitney F100 engine. The United States Air Force operates F-15 and F-16 fighter aircraft powered by the F100 engine. These turbine engines have multi-stage rotating components that have unique vibratory responses that shift due to changes in the operating environment related to airflow, blade tip clearances, engine speed, or component damage, etc. The diagnostic system must serve to detect and warn of frequency response changes due to propagation of pre-critical LCF and/or transient HCF component cracks by fusing real-time state awareness sensor data with advanced predictive algorithms. This diagnostic system must be non-developmental. Potential respondents must have demonstrated the system capability on a fielded system for a multi-aircraft fleet. The system must be self-contained and not require integration with an existing engine control or monitoring system. It must maintain operability in the engine-operating environment including temperatures up to 1500C, pressures up to 10 Mpa, and vibration up to15g. Potential respondents should possess the technical ability to perform an advanced diagnostic system verification task. This task includes the F100 engine system integration, related fabrication and assembly, performance parameter verification, data analysis, and reporting. The Government does not presently intend to award a contract on the basis of this RFI, but wants to obtain market information or capabilities for planning purposes. Responses to this notice are not offers and cannot be accepted by the Government to form a binding contract. Submission of a response is voluntary, and participants will not be compensated. Routine communications concerning this special notice should be directed to Brian Allport, Contract Negotiator, at (937) 656-9832, or Bruce Miller, Contracting Officer, at (937) 255-2643. Potential sources should submit information describing their non-developmental engine diagnostic system to Brian Allport, AFRL/PRKB, by e-mail (brian.allport@wpafb.af.mil) by 14 June 2004. Submissions should not exceed 8 pages in length.