SBIR/STTR Research Award

Mapping Liquid Mass Fractions in Optically Dense Rocket Combustion Chambers

Award identifier 654789a06fbbb31524963a065a64a2b9babc6e12f8195908a2601456e22ff731Awarding agency Department of Defense · Air Force

Award amount

$150,000

Program and phase

SBIR · Phase I

Award year

2012

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Award details

Awarding agency
Department of Defense
Branch
Air Force
Recipient company
En'urga Inc.
Proposal award date
2012-06-20
Contract end date
Not reported
UEI
LFCSBTSRFJU2
Solicitation number
2012.1
Topic code
AF121-193

Research abstract

ABSTRACT: This Small Business Innovation Research Phase 1 project will evaluate the feasibility of utilizing X-Ray tomography to map liquid mass fractions in optically dense sprays. High fuel flow rate nozzles are ubiquitous in rocket propulsion, power generation, and transportation. In these high flow rate nozzles, the local mass fraction of fuel is directly proportional to the local heat release rate, and therefore it impacts both the combustion stability and engine efficiency. However, it is not currently possible to fully elucidate the structure of these dense sprays, particularly in a reacting environment, where conventional optical diagnostics is impossible. During Phase I, En"Urga Inc. will demonstrate the feasibility of utilizing X-Ray tomography for obtaining the structure of fuel sprays in a non-reacting environment. During Phase II, a prototype system will be developed and evaluated in hot fire condition. There are two issues of intellectual merit that will be addressed during the Phase I work. The first issue is the development of an X-Ray tomography system to measure path-integrated extinction from high mass flow rate sprays. The second is the development of an advanced algorithm that will provide local mass concentrations from the path integrated measurements. These two novel features enable an accurate characterization of liquid mass fractions in optically dense sprays. BENEFIT: There are two primary commercial applications for the proposed spray diagnostic. The first is in the characterizing the near injector structure of dense sprays prevalent in the automotive and aerospace industries. Characterization of near injector structure is extremely important for the development and evaluation of newer fuel injectors, which provide greater efficiency and lower pollution. Typical customers in this area include aircraft engine manufactures such as Rolls-Royce, GE, and Pratt and Whitney, as well as automotive manufacturers and their suppliers such as GM, Eaton, Ford, Bosch, Cummins, Chrysler, Detroit Diesel, Caterpillar, John Deere, etc. The second commercial application for the proposed diagnostics is in industrial burners. There are several high flow industrial burner nozzles using fuels ranging from coal slurry to furnace oil. These nozzles cannot be currently evaluated due to the fact that they produce sprays that are very dense. The proposed system will make the fuel flow pattern from such nozzles amenable to investigation for the first time.

Technology keywords

Not reported

Other awards by this recipient

Verified by the same UEI. These are other public SBIR/STTR award pages, not a merged company record.

Awards with the same topic code

Verified by an exact topic code match. This is not a text-similarity match.

Research funding history

40 SBIR/STTR records share this UEI (1996–2022). Reported award amounts total $6,688,664. Reported amounts are not federal obligations.

Phases: Phase I, Phase II

Agencies: National Science Foundation, National Aeronautics and Space Administration, Department of Commerce, Department of Defense, Department of Agriculture, Department of Energy

Agency intelligence

Department of Defense

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