초록 ▼

An inerting system and method characterized by a primary air separation module configured to communicate with an upstream source of pressurized air at elevated temperature for production of a primary downstream flow of nitrogen-enriched air to be delivered to a space to be inerted; a secondary air s

An inerting system and method characterized by a primary air separation module configured to communicate with an upstream source of pressurized air at elevated temperature for production of a primary downstream flow of nitrogen-enriched air to be delivered to a space to be inerted; a secondary air separation module configured to communicate with the upstream source of pressurized air at elevated temperature for production of a supplemental downstream flow of nitrogen-enriched air to be delivered to a space to be inerted when high nitrogen-enriched airflow is desired during a high flow period; and a flow controller configured to provide a warming flow through the secondary air separation module to heat the secondary air separation module to above ambient temperature during a warming period other than the high flow period.

대표청구항 ▼

What is claimed is: 1. An inerting system, comprising: a primary air separation module configured to communicate with an upstream source of pressurized air at elevated temperature for production of a primary downstream flow of nitrogen-enriched air to be delivered to a space to be inerted; a second

What is claimed is: 1. An inerting system, comprising: a primary air separation module configured to communicate with an upstream source of pressurized air at elevated temperature for production of a primary downstream flow of nitrogen-enriched air to be delivered to a space to be inerted; a secondary air separation module configured to communicate with the upstream source of pressurized air at elevated temperature for production of a supplemental downstream flow of nitrogen-enriched air to be delivered to a space to be inerted when high nitrogen-enriched air flow is desired during a high flow period; a flow controller configured to provide a warming flow through the secondary air separation module to heat the secondary air separation module to above ambient temperature during a warming period other than the high flow period; a main secondary outlet flow line connected to the outlet of the secondary air separation module for delivery of the outlet flow of the secondary air separation module to the space to be inerted, and wherein the flow controller comprises a main secondary outlet flow control valve for controlling flow through the a main secondary outlet flow line; and a warming flow bypass line connected to the main secondary outlet flow line at a first location upstream of the main secondary outlet flow control valve for diverting outlet flow of the secondary air separation module away from the space to be inerted, wherein the warming flow bypass line diverts outlet flow of the secondary air separation module away from the inerting system during warm up. 2. An inerting system as set forth in claim 1, in combination with an aircraft including a fuel tank to which the primary and supplemental downstream flows of nitrogen-enriched air are supplied, and wherein the warming flow bypass line diverts outlet flow of the secondary air separation module overboard during the warm up. 3. An inerting system as set forth in claim 1, wherein the outlet flow of the secondary air separation module can flow through the warming flow bypass line when the main secondary outlet control valve is open to allow for a warming flow through the secondary air separation module. 4. An inerting system as set forth in claim 1, wherein the flow controller includes a warming flow control valve for controlling flow through the bypass line during periods other than the high flow period. 5. An inerting system as set forth in claim 4, comprising a main secondary inlet flow line connected to the inlet of the secondary air separation module for delivery of the pressurized air at elevated temperature to the secondary air separation module, and wherein the flow controller comprises a main secondary inlet control valve for controlling flow through the main secondary inlet flow line. 6. An inerting system, comprising: a primary air separation module configured to communicate with an upstream source of pressurized air at elevated temperature for production of a primary downstream flow of nitrogen-enriched air to be delivered to a space to be inerted; a secondary air separation module configured to communicate with the upstream source of pressurized air at elevated temperature for production of a supplemental downstream flow of nitrogen-enriched air to be delivered to a space to be inerted when high nitrogen-enriched air flow is desired during a high flow period; a flow controller configured to provide a warming flow through the secondary air separation module to heat the secondary air separation module to above ambient temperature during a warming period other than the high flow period; a main secondary outlet flow line connected to the outlet of the secondary air separation module for delivery of the outlet flow of the secondary air separation module to the space to be inerted, and wherein the flow controller comprises a main secondary outlet flow control valve for controlling flow through the a main secondary outlet flow line; a warming flow bypass line connected to the main secondary outlet flow line at a first location upstream of the main secondary outlet flow control valve for diverting outlet flow of the secondary air separation module away from the space to be inerted; and a main secondary inlet flow line connected to the inlet of the secondary air separation module for delivery of the pressurized air at elevated temperature to the secondary air separation module, and wherein the flow controller comprises a main secondary inlet control valve for controlling flow through the main secondary inlet flow line; wherein the flow controller includes a warming flow control valve for controlling flow through the bypass line during periods other than the high flow period; and wherein the flow controller includes control circuitry for commanding the warming flow control valve and the main secondary inlet control valve to an open condition and the main secondary outlet flow control valve to a closed condition during the warming periods, thereby to allow flow of the pressurized air at elevated temperature to the secondary air separation module and diversion of the outlet flow of the secondary air separation module away from the space to be inerted. 7. An inerting system as set forth in claim 1, wherein the main secondary outlet flow line includes a main outlet flow restriction downstream of said first location, and the warming flow bypass line includes a bypass flow restriction that restricts flow to a greater extent than the main outlet flow restriction, such that a major portion of the flow will flow through main secondary outlet control valve when open than through the warming flow bypass line. 8. An inerting system as set forth in claim 6, in combination with an aircraft including a fuel tank to which the primary and supplemental downstream flows of nitrogen-enriched air are supplied. 9. A combination as set forth in claim 8, wherein the high flow period corresponds with descent of the aircraft. 10. A combination as set forth in claim 9, wherein the flow controller operates to provide a warming flow through the secondary air separation module to heat the secondary air separation module during ascent of the aircraft.