Aircraft fire extinguishing device and mounting method
A fire extinguisher device for aircraft has a hanger structure and a reservoir of extinguishing agent, the aforementioned reservoir being hung beneath the aforementioned hanger structure by metal fittings held by fasteners to the aforementioned hanger structure. The aforementioned extinguisher wherein the reservoir has means of suspension and the hanger structure has carriers complementary to the means of suspension, the aforementioned means of suspension and the aforementioned carriers being such that when the fasteners are withdrawn, the reservoir is in a position called the “intermediate position,” in which the metal fittings are free and the reservoir is suspended by interaction of the means of suspension and the carriers. The disclosed embodiments also relate to a method for fastening such an extinguishing device.
1. A fire extinguisher device for aircraft comprising:
a hanger structure and
a reservoir of extinguishing agent,
the reservoir being hung beneath said hanger structure by metal fittings extending from said reservoir selectively secured by fasteners to said hanger structure,
the reservoir comprising a suspension element extending therefrom,
the hanger structure comprising a carrier element configured to receive and support the suspension element,
said suspension element and said carrier element being configured such that:
when the fasteners are tightened they clamp together the metal fittings and the hanger structure so that the reservoir is held in an operational position in which the metal fittings are integral with and mechanically support the reservoir from the hanger structure, and the suspension element and the carrier element are mechanically disengaged from contact with each other, and
when the fasteners are withdrawn from the metal fittings, the reservoir moves to an intermediate position in which the metal fittings are free from the hanger structure and the reservoir is suspended and supported by mechanical interaction of the suspension element and the carrier element.
2. The device according to claim 1 , wherein the suspension element is located in an upper part of the reservoir, essentially in a position vertical from a center of gravity of said reservoir.
3. The device according to claim 1 , wherein the suspension element and the carrier element are made so that the intermediate position is adjacent to the operational position.
4. The device according to claim 1 , wherein the suspension element has a free end in the form of a hook.
5. The device according to claim 4 , wherein the carrier element comprises a ring.
6. The device according to claim 1 , wherein the suspension element has only one free end.
7. The device according to claim 1 , wherein the suspension element has a free end with a T-shaped cross section.
8. The device according to claim 1 , wherein the carrier element comprises a longitudinal slide bar.
9. An aircraft that has at least one engine pylon in which at least one extinguishing device is fastened, the extinguishing device comprising:
a hanger structure and
a reservoir of extinguishing agent,
the reservoir being hung beneath said hanger structure by metal fittings extending from said reservoir selectively secured by fasteners to said hanger structure,
the reservoir comprising a suspension element extending therefrom,
the hanger structure comprising a carrier element configured to receive and support the suspension element,
said suspension element and said carrier element being configured such that:
when the fasteners are tightened they clamp together the metal fittings and the hanger structure so that the reservoir is held in an operational position in which the metal fittings are integral with and mechanically support the reservoir from the hanger structure, and the suspension element and the carrier element are mechanically disengaged from contact with each other, and
when the fasteners are withdrawn from the metal fittings, the reservoir moves to an intermediate position in which the metal fittings are free from the hanger structure and the reservoir is suspended and supported by mechanical interaction of the suspension element and the carrier element.
10. A method for fastening a reservoir of extinguishing agent for an extinguishing device comprising:
a hanger structure and
a reservoir of extinguishing agent,
the reservoir being hung beneath said hanger structure by metal fittings extending from said reservoir selectively secured by fasteners to said hanger structure,
the reservoir comprising a suspension element extending therefrom,
the hanger structure comprising a carrier element configured to receive and support the suspension element,
said suspension element and said carrier element being configured such that:
when the fasteners are tightened they clamp together the metal fittings and the hanger structure so that the reservoir is held in an operational position in which the metal fittings are integral with and mechanically support the reservoir from the hanger structure, and the suspension element and the carrier element are mechanically disengaged from contact with each other, and
when the fasteners are withdrawn from the metal fittings, the reservoir moves to an intermediate position in which the metal fittings are free from the hanger structure and the reservoir is suspended and supported by mechanical interaction of the suspension element and the carrier element,
the method comprising the steps:
suspending the reservoir on the hanger structure during which the suspension element of the reservoir is engaged in the carrier element of the hanger structure and interacts with said carrier element so that the reservoir is in the intermediate suspended position in which the metal fittings are free, and
fastening the reservoir beneath the hanger structure in which the fittings of said reservoir are fastened to said hanger structure by tightening the fasteners.