Helicopter with an auxiliary lubricating circuit
There is described a helicopter having a first member movable with respect to a second member; lubricated supporting means for supporting the first member with respect to the second member; and a primary lubricating circuit for lubricating the supporting means and in turn having primary storage means for accumulating a lubricating fluid, and primary fluid feed means for feeding the lubricating fluid to the supporting means; the helicopter also has an auxiliary lubricating circuit supplied continually by the primary storage means with a first lubricating fluid flow value, and itself continually supplying the supporting means with a second lubricating fluid flow value lower than the first value, so as to produce an auxiliary storage volume of lubricating fluid for use in the event of breakdown of the primary lubricating circuit.
1. A helicopter comprising:
a first and a second member;
lubricated supporting means for supporting said first member movably with respect to said second member; and
a primary lubricating circuit for lubricating said supporting means and in turn comprising primary storage means for accumulating a lubricating fluid, and primary fluid feed means for feeding said lubricating fluid to said supporting means;
said helicopter comprising an auxiliary lubricating circuit supplied continually by said primary storage means with a first lubricating fluid flow value, and itself continually supplying said supporting means with a second lubricating fluid flow value lower than said first value, so as to produce an auxiliary storage volume of lubricating fluid for use in the event of breakdown of said primary lubricating circuit;
said auxiliary storage volume being located outside the first member;
said helicopter being characterized in that said first member rotates about an axis with respect to said second member, and defines internally a chamber supplied by said primary and said auxiliary lubricating circuit and fluidly connected to said supporting means by an opening formed in the first member and radial with respect to said axis.
2. A helicopter as claimed in claim 1 , characterized in that said auxiliary lubricating circuit comprises auxiliary storage means supplied by said primary storage means and defining said auxiliary storage volume; and auxiliary fluid feed means supplied by said auxiliary storage means and in turn supplying said supporting means by means of an outlet, which is smaller than an outlet of said primary fluid feed means in a direction crosswise to the flow of said lubricating fluid.
3. A helicopter as claimed in claim 2 , characterized in that said auxiliary storage means are supplied by said primary storage means along a fluid line, and in that said outlet of said auxiliary fluid feed means is smaller than said fluid line in a direction crosswise to the flow of said lubricating fluid.
4. A helicopter as claimed in claim 3 , characterized by comprising a transmission comprising said first and said second member.
5. A helicopter as claimed in claim 3 , characterized in that said primary storage means supply said primary lubricating circuit and said auxiliary lubricating circuit via the same fluid line.
6. A helicopter as claimed in claim 2 , characterized in that said primary storage means supply said primary lubricating circuit and said auxiliary lubricating circuit via the same fluid line.
7. A helicopter as claimed in claim 2 , characterized by comprising a transmission comprising said first and said second member.
8. A helicopter as claimed in claim 1 , characterized in that said primary storage means supply said primary lubricating circuit and said auxiliary lubricating circuit via the same fluid line.
9. A helicopter as claimed in claim 8 , characterized by comprising a transmission comprising said first and said second member.
10. A helicopter as claimed in claim 1 , characterized by comprising a transmission comprising said first and said second member.