NASA SBIR 2007 Solicitation

FORM B - PROPOSAL SUMMARY


PROPOSAL NUMBER: 07-1 A1.06-8474
SUBTOPIC TITLE: Sensing and Diagnostic Capability
PROPOSAL TITLE: Autonomous Composite Fan Containment Integrity Monitoring (AUTOCONFIRM) system

SMALL BUSINESS CONCERN (Firm Name, Mail Address, City/State/Zip, Phone)
Acellent Technologies, Inc.
835 Stewart Drive
Sunnyvale, CA 94085 - 4514
(408) 745-1188

PRINCIPAL INVESTIGATOR/PROJECT MANAGER (Name, E-mail, Mail Address, City/State/Zip, Phone)
Amrita Kumar
akumar@acellent.com
835 Stewart Drive
Sunnyvale, CA 94085 - 4514
(408) 745-1188

Expected Technology Readiness Level (TRL) upon completion of contract: 5 to 6

TECHNICAL ABSTRACT (Limit 2000 characters, approximately 200 words)
New engine fan blade containment structures are being manufactured with advanced composite structures such that they can withstand blade-out events. The use of advance composites requires the understanding of the possible effects of aging degradation on the performance of "hard wall" or "soft wall" composite fan containment structures to ensure durability in their use in jet engine applications. Acellent Technologies, Inc. proposes to develop an innovative, low-cost and reliable system for assessment of the integrity of composite fan containment structures that will automatically monitor in real-time the location and extent of damage in the containment structure. The system will utilize a network of miniature sensors integrated with the structure to scan the entire structural area for any impact events, resulting structural damage and monitor degradation due to usage. Phase I will focus on developing a prototype of the system and demonstrating functionality to detect damage both on the inner and exterior surface of the fan containment structure.

POTENTIAL NASA COMMERCIAL APPLICATIONS (Limit 1500 characters, approximately 150 words)
The proposed system directly the need for inspection of fan containment composite structures and it is expected that once developed, the proposed system will provide the following advantages over current inspection techniques:
· Low-cost built-in reliable damage detection system for monitoring of containment structure integrity
· Improved personnel safety
· Improvement of fan containment structure reliability
· Ease of installation
· Reduction of labor time
· Real-time convenience and automation of inspection during service

POTENTIAL NON-NASA COMMERCIAL APPLICATIONS (Limit 1500 characters, approximately 150 words)
Since nearly all in-service composite structures require some form of inspection and maintenance procedures to monitor their integrity and health condition to prolong life span or to prevent catastrophic failures, the potential applications of the proposed system are very broad. In the future, this system can potentially be used to monitor all types of composite structures on aircraft and spacecraft.

NASA's technology taxonomy has been developed by the SBIR-STTR program to disseminate awareness of proposed and awarded R/R&D in the agency. It is a listing of over 100 technologies, sorted into broad categories, of interest to NASA.

TECHNOLOGY TAXONOMY MAPPING
Aircraft Engines
Airframe
Airport Infrastructure and Safety
Ceramics
Composites
Multifunctional/Smart Materials
Perception/Sensing
Propellant Storage
Sensor Webs/Distributed Sensors
Spaceport Infrastructure and Safety
Structural Modeling and Tools
Tankage
Thermal Insulating Materials


Form Generated on 09-18-07 17:50