Crash attenuation system for aircraft
A crash attenuation system for an aircraft, the system having an airbag carried by the aircraft and inflatable generally adjacent an exterior of the aircraft. The airbag has at least one vent for releasing gas from the interior of the airbag. A first gas source is in fluid communication with the interior of the airbag for inflating the airbag with gas generated provided by the first gas source. A vent valve is provided for controlling a flow of gas through each vent, each vent valve being selectively configurable between an open state, in which gas can pass through the associated vent from the interior of the airbag, and a closed state, in which gas is retained within the interior of the airbag. A second gas source is provided for at least partially re-inflating the airbag after venting of gas through the at least one vent.
1. A crash attenuation system for an aircraft, the system comprising:
an airbag carried by the aircraft and inflatable to a position exterior of the aircraft, the airbag having at least one vent for releasing gas from the interior of the airbag for crash attenuation;
a first gas source in fluid communication with the interior of the airbag for inflating the airbag to the position exterior of the aircraft with gas provided by the first gas source;
a vent valve for controlling a flow of gas through each of the at least one vent, each vent valve being selectively configurable between an open state, in which gas can pass through the associated vent from the interior of the airbag, and a closed state, in which gas is retained within the interior of the airbag; and
a second gas source in fluid communication with the interior of the airbag for at least partially re-inflating the airbag with gas provided by the second gas source after venting of gas through the at least one vent.
2. The crash attenuation system according to claim 1 , wherein the first gas source is a gas generator.
3. The crash attenuation system according to claim 1 , wherein the second gas source comprises compressed gas.
4. The crash attenuation system according to claim 1 , further comprising:
a water-detection system for detecting the presence of water.
5. The crash attenuation system according to claim 1 , further comprising:
a water-detection system for detecting the presence of water;
wherein when the water-detection system detects water, each vent valve is switched to the closed state, and the second gas source is used to at least partially re-inflate the airbag.
6. A crash attenuation system for an aircraft, the system comprising:
an airbag carried by the aircraft and inflatable to a position exterior of the aircraft, the airbag having at least one vent for releasing gas from the interior of the airbag for crash attenuation;
a first gas source in fluid communication with the interior of the airbag for inflating the airbag to the position exterior of the aircraft with gas provided by the first gas source;
a vent valve for controlling a flow of gas through each of the at least one vent, each vent valve being selectively configurable between an open state, in which gas can pass through the associated vent from the interior of the airbag, and a closed state, in which gas is retained within the interior of the airbag;
a second gas source in fluid communication with the interior of the airbag for at least partially re-inflating the airbag with gas provided by the second gas source after venting of gas through the at least one vent; and
a water-detection system for detecting the presence of water.
7. The crash attenuation system according to claim 6 , wherein the first gas source is a gas generator.
8. The crash attenuation system according to claim 6 , further comprising:
wherein the second gas source comprises compressed gas.
9. The crash attenuation system according to claim 6 , further comprising:
wherein when the water-detection system detects water, each vent valve is switched to the closed state, and the second gas source is used to at least partially re-inflate the airbag.