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A Fiber-Optic Probe Design for Combustion Chamber Flame Detection Applications-Design Criteria, Performance S... NASA

A Fiber-Optic Probe Design for Combustion Chamber Flame Detection Applications-Design Criteria, Performance S... NASA PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages :

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A Fiber-Optic Probe Design for Combustion Chamber Flame Detection Applications-Design Criteria, Performance S... NASA

A Fiber-Optic Probe Design for Combustion Chamber Flame Detection Applications-Design Criteria, Performance S... NASA PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages :

Book Description


A Fiber-Optic Probe Design for Combustion Chamber Flame Detection Applications-Design Criteria, Performance Specifications, and Fabrication Technique

A Fiber-Optic Probe Design for Combustion Chamber Flame Detection Applications-Design Criteria, Performance Specifications, and Fabrication Technique PDF Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781721280513
Category :
Languages : en
Pages : 28

Book Description
This paper documents the design and development of the fiber-optic probes utilized in the flame detection systems used in NASA Langley Research Center's 8-Foot High Temperature Tunnel (8-ft HTT). Two independent flame detection systems are utilized to monitor the presence and stability of the main-burner and pilot-level flames during facility operation. Due to the harsh environment within the combustor, the successful development of a rugged and efficient fiber-optic probe was a critical milestone in the development of these flame detection systems. The final optical probe design for the two flame detection systems resulted from research that was conducted in Langley's 7-in High Temperature Pilot Tunnel (7-in HTT). A detailed description of the manufacturing process behind the optical probes used in the 8-ft HTT is provided in Appendix A of this report. Borg, Stephen E. and Harper, Samuel E. Langley Research Center NASA/TM-2001-211233, L-18121, NAS 1.15:211233

A Fiber-Optic Probe Design for Combustion Chamber Flame Detection Applications-Design Criteria, Performance Specifications, and Fabrication Technique

A Fiber-Optic Probe Design for Combustion Chamber Flame Detection Applications-Design Criteria, Performance Specifications, and Fabrication Technique PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 16

Book Description


A FIBER-OPTIC PROBE DESIGN FOR COMBUSTION CHAMBER FLAME DETECTION APPLICATIONS-DESIGN CRITERIA, PERFORMANCES... NASA/TM-2001-211233... DEC.

A FIBER-OPTIC PROBE DESIGN FOR COMBUSTION CHAMBER FLAME DETECTION APPLICATIONS-DESIGN CRITERIA, PERFORMANCES... NASA/TM-2001-211233... DEC. PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages :

Book Description


NASA Langley Scientific and Technical Information Output-2001

NASA Langley Scientific and Technical Information Output-2001 PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 166

Book Description


Optically Based Flame Detection in the NASA Langley 8-Ft High- Temperature Wind Tunnel

Optically Based Flame Detection in the NASA Langley 8-Ft High- Temperature Wind Tunnel PDF Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781721785339
Category :
Languages : en
Pages : 24

Book Description
Two optically based flame-detection systems have been developed for use in NASA Langley's 8-Foot High-Temperature Tunnel (8-ft HTT). These systems are used to detect the presence and stability of the main-burner and pilot-level flames during facility operation. System design considerations will be discussed, and a detailed description of the system components and circuit diagrams will be provided in the Appendices of this report. A more detailed description of the manufacturing process used in the fabrication of the fiber-optic probes is covered in NASA TM-2001-211233. Borg, Stephen E. Langley Research Center NASA/TM-2005-213755, L-19104

Fiber Optic (Flight Quality) Sensors for Advanced Aircraft Propulsion

Fiber Optic (Flight Quality) Sensors for Advanced Aircraft Propulsion PDF Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781722395445
Category :
Languages : en
Pages : 94

Book Description
Development of flight prototype, fiber-optic sensing system components for measuring nine sensed parameters (three temperatures, two speeds, three positions, and one flame) on an F404-400 aircraft engine is described. Details of each sensor's design, functionality, and environmental testing, and the electro-optics architecture for sensor signal conditioning are presented. Eight different optical sensing techniques were utilized. Design, assembly, and environmental testing of an engine-mounted, electro-optics chassis unit (EOU), providing MIL-C-1553 data output, are related. Interconnection cables and connectors between the EOU and the sensors are identified. Results of sensor/cable/circuitry integrated testing, and installation and ground testing of the sensor system on an engine in October 1993 and April 1994 are given, including comparisons with the engine control system's electrical sensors. Lessons learned about the design, fabrication, testing, and integration of the sensor system components are included. Poppel, Gary L. Unspecified Center...

Design and Evaluation of a Fiber Optic Probe as a Means of Subsurface Planetary Exploration

Design and Evaluation of a Fiber Optic Probe as a Means of Subsurface Planetary Exploration PDF Author: Robert Paul Pilgrim
Publisher:
ISBN: 9781303289071
Category : Fiber optics
Languages : en
Pages : 284

Book Description
The Optical Probe for Regolith Analysis (OPRA) is an instrumentation concept designed to provide spectroscopic analysis of the near subsurface of unconsolidated regolith on bodies such as moons, asteroids and planets. Below a chemically altered surface may lay the geological history in the form of stratigraphy that is shielded from degradation due to harsh external environments. Most of what we know about our solar system comes from remote platforms, such as satellites that are deployed into orbit around the target body. In the case of Mars, we have had several successful landers and rovers however, with the exception of the Mars Science Laboratory that just drilled its first hole, the complexity of subsurface excavation has limited the extent of subsurface exploration to simple scoops deployed on the ends of robotic arms which, by their very nature, will erase any stratigraphy that it may be digging into. The OPRA instrumentation concept allows for an integrated, lightweight and simple apparatus for subsurface exploration via a small, spike like structure which contains integrated optical fibers coupled to small windows running down the length of the probe. Each window is connected to a spectrometer housed onboard the deploying spacecraft. Each window is separately interrogated via the spectrometer over the wavelength range 1-2.5 nm to produce a spectroscopic profile as a function of depth. This project takes the Technology Readiness Level (TRL) of the OPRA instrumentation concept to level 3, which is defined by NASA to be the demonstration either analytically or experimentally of the proof of concept for critical functions of the proposed instrument. Firstly, to demonstrate that optical fibers are feasible for this type of application, we report on the techniques used by NASA to space qualify optical fibers. We investigate the optical performance of several fiber optic bundle configurations, both experimentally and numerically, to help optimize bundle performance. Optical bundles were then spectrally validated via a series of spectral comparisons between standardized reflectance spectroscopy targets and spectra obtained with the bundles. We also report on the integration of fiber optical bundles into other research and experimental results from several other groups within our research teams to obtain spectra under a more "space like" environment. Finally, the probe housing structural performance was investigated via finite element analysis, using probe penetration forces derived from data analysis of experimentation conducted by the Apollo lunar missions, and investigations into a mechanical analogue for the Martian regolith.

NASA Technical Memorandum

NASA Technical Memorandum PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 492

Book Description


Fiber Optic Sensors and Systems

Fiber Optic Sensors and Systems PDF Author:
Publisher: Information Gatekeepers Inc
ISBN:
Category :
Languages : en
Pages : 11

Book Description