Systems and methods for determining a boiling point distribution of a sample include controlling the rates of temperature increase for a column and an injection port. An analyzer includes a column having a column heating element and an injection port having an injection port heating element. The temperature of the column can be increased at a first rate, and a temperature of the injection port can be increased at a second rate. The first and second rates are selected such that the temperature of the injection port is within about five to fifteen degrees Celsius of the temperature of the column when the temperature of the injection port reaches a target temperature of minimal thermal decomposition.

Systems and methods for determining a boiling point distribution of a sample include controlling the rates of temperature increase for a column and an injection port. An analyzer includes a column having a column heating element and an injection port having an injection port heating element. The temperature of the column can be increased at a first rate, and a temperature of the injection port can be increased at a second rate. The first and second rates are selected such that the temperature of the injection port is within about five to fifteen degrees Celsius of the temperature of the column when the temperature of the injection port reaches a target temperature of minimal thermal decomposition.

Embodiments of the present disclosure relate to an Operational Flight Efficiency Evaluation (OFEE) system for an aircraft. The system comprises an Avionics Situation Awareness Device (ASAD). The ASAD includes one or more processors, a memory communicatively coupled to the one or more processors, and a flight data collection interface configured to, via the one or more processors, collect empirical flight data for a flight and store the empirical flight data in the memory. The OFEE also includes a Simulation And Comparison System (SACS) in communication with the ASAD. The ASAD includes a database communicatively coupled to a National Airspace System (NAS). The database is also configured to automatically acquire and store avionics systems available for flight efficiencies from the NAS. The ASAD also includes a simulator configured to identify at least one avionics upgrade based on the collected empirical flight data and the avionics systems available for flight efficiencies.

Embodiments of the present disclosure relate to an Operational Flight Efficiency Evaluation (OFEE) system for an aircraft. The system comprises an Avionics Situation Awareness Device (ASAD). The ASAD includes one or more processors, a memory communicatively coupled to the one or more processors, and a flight data collection interface configured to, via the one or more processors, collect empirical flight data for a flight and store the empirical flight data in the memory. The OFEE also includes a Simulation And Comparison System (SACS) in communication with the ASAD. The ASAD includes a database communicatively coupled to a National Airspace System (NAS). The database is also configured to automatically acquire and store avionics systems available for flight efficiencies from the NAS. The ASAD also includes a simulator configured to identify at least one avionics upgrade based on the collected empirical flight data and the avionics systems available for flight efficiencies.

Analytic sensors and methods utilize an attenuated total reflection (ATR) crystal to detect volatile compounds in an arrangement that reduces interference from compounds other than the one of interest. In particular, the components in the measurement stream are limited to those having volatilities close to that of the analyte of interest, which may be identified based on, for example, the temperature of the ATR crystal and the dwell timei.e., an interval of substantially constant temperature as the ATR crystal is heated.

Analytic sensors and methods utilize an attenuated total reflection (ATR) crystal to detect volatile compounds in an arrangement that reduces interference from compounds other than the one of interest. In particular, the components in the measurement stream are limited to those having volatilities close to that of the analyte of interest, which may be identified based on, for example, the temperature of the ATR crystal and the dwell timei.e., an interval of substantially constant temperature as the ATR crystal is heated.

Embodiments of the present disclosure relate to an Operational Flight Efficiency Evaluation (OFEE) system for an aircraft. The system comprises an Avionics Situation Awareness Device (ASAD). The ASAD includes one or more processors, a memory communicatively coupled to the one or more processors, and a flight data collection interface configured to, via the one or more processors, collect empirical flight data for a flight and store the empirical flight data in the memory. The OFEE also includes a Simulation And Comparison System (SACS) in communication with the ASAD. The ASAD includes a database communicatively coupled to a National Airspace System (NAS). The database is also configured to automatically acquire and store avionics systems available for flight efficiencies from the NAS. The ASAD also includes a simulator configured to identify at least one avionics upgrade based on the collected empirical flight data and the avionics systems available for flight efficiencies.

This present disclosure is directed to a method and apparatus for collecting small amounts, sub mg levels, of elemental sulfur (or other trace elements such as mercury) deposited from the ppm levels of elemental sulfur (or other trace elements such as mercury) contained in gases found in typical oil production environments or gas streams with anticipated sulfur deposition problems, as well as in industries other than oil and gas. An analytical chemistry technique for determining the amount of sulfur collected is used and from this result, the solubility of sulfur in a gas at a fixed temperature, pressure and gas composition can be calculated.

Disclosed herein are embodiments for real-time measurement of drying in a freeze-drying system. In at least one embodiment, the freeze-drying system includes a freeze-drying chamber; a condenser coupled to the freeze-drying chamber; one or more load sensors; and a processing device operatively coupled to the one or more load sensors and configured to measure mass change of components of the freeze-drying system during a freeze-drying process.

Disclosed herein are embodiments for real-time measurement of drying in a freeze-drying system. In at least one embodiment, the freeze-drying system includes a freeze-drying chamber; a condenser coupled to the freeze-drying chamber; one or more load sensors; and a processing device operatively coupled to the one or more load sensors and configured to measure mass change of components of the freeze-drying system during a freeze-drying process.