Landing gear provided with energy absorber means, an aircraft provided with said landing gear, and a method of landing

1. Aircraft landing gear provided with at least one contact means for making contact with a contact surface (S), wherein the landing gear includes energy absorber means provided with an inflatable airbag secured to said contact means and suitable for interposing itself between said contact surface (S) and said contact means, said energy absorber means being provided with control means and with at least one inflation means for inflating said airbag under the control of said control means, said energy absorber means including adjuster means for adjusting the pressure that exists inside (INT) said airbag, said adjuster means comprising at least one orifice open to the inside (INT) of the airbag, said contact means being dimensioned to withstand the forces that result from landing at a predetermined vertical speed, said open orifice being dimensioned to enable said contact means to make contact with the contact surface (S) at said predetermined vertical speed.

2. Landing gear according to claim 1 , wherein said contact means is at least one of a wheel, a skid, or a ski.

3. Landing gear according to claim 1 , wherein said airbag is folded inside a container secured to said contact means, said airbag exploding the container when it is inflated by said inflation means under the control of said control means in order to interpose itself between said contact means and the contact surface (S).

4. Landing gear according to claim 1 , wherein said energy absorber means are provided with detector means for detecting an imminent impact and delivering at least one measurement signal to said control means relating to an imminent impact with the contact surface.

5. Landing gear according to claim 4 , wherein said impact detector means comprise a height detector for detecting height relative to the contact surface (S).

6. Landing gear according to claim 4 , wherein said impact detector means comprise a vertical speed detector for detecting the vertical speed of said contact means.

7. An aircraft, including landing gear according to claim 1 .

8. Landing gear according to claim 1 , wherein the contact means comprises a wheel having a tire arranged on an axle and the landing gear further comprises an explodable container fastened to the axle outside the wheel, the airbag being folded inside the container.

9. The aircraft landing gear of claim 1 , wherein the adjuster means comprises a valve and a valve controller configured to vary a flow area of the valve in response to a measured pressure inside the airbag.

10. A method of landing for touching an aircraft down on a contact surface, said aircraft having landing gear provided with at least one contact means, said aircraft including energy absorber means provided with an inflatable airbag secured to said contact means and suitable for interposing itself between said contact surface (S) and said contact means, said energy absorber means being provided with control means and at least one inflation means for inflating said airbag under the control of said control means, said energy absorber means including adjuster means for adjusting the pressure that exists in the inside (INT) of said airbag, during which method said airbag is inflated equally well:

either when the height between said contact means and said contact surface is less than a predetermined threshold height while a vertical speed of said contact means is greater than a predetermined vertical speed; or

else when said contact surface comprises a flexible material into which the contact means might penetrate;

and after said airbag has been inflated, the adjuster means are used to adjust the pressure that exists in the inside (INT) of said airbag in order to enable said contact means to make contact with the contact surface (S) at said predetermined vertical speed.

11. An energy absorber for an aircraft landing gear, the landing gear being connected to an aircraft fuselage and having a contact point for contacting a landing area, the landing gear being configured to withstand a landing at a vertical speed threshold, the energy absorber comprising:

an inflatable airbag secured to the landing gear and configured to interpose between the contact point and the landing area upon activation;

a controller;

an inflation device associated with the airbag and configured to inflate the airbag in response to a command from the controller; and

a pressure adjuster associated with the airbag and configured to adjust the pressure inside the airbag to reduce an aircraft velocity to the vertical speed threshold.

12. The energy absorber of claim 11 , wherein the pressure adjuster comprises an orifice open to the airbag, the orifice being sized to relieve pressure inside the airbag at a controlled rate to reduce the aircraft velocity to the vertical speed threshold.

13. The energy absorber of claim 11 , wherein the pressure adjuster comprises a valve and a valve controller configured to open the valve when a predetermined pressure is reached inside the airbag.

14. The energy absorber of claim 11 , wherein the controller is configured to command the inflation device to inflate the airbag in response to a detected water landing.

15. The energy absorber of claim 11 , wherein the landing gear comprises an axle supporting a vehicle wheel and the airbag is secured to the axle outside the wheel.

16. The energy absorber of claim 11 , wherein the landing gear comprises a skid and the airbag is folded within a container secured to the skid.

17. The energy absorber of claim 16 , wherein the skid has a first lateral portion and a second lateral portion and the airbag is configured to interpose between the first lateral portion and the landing area upon activation with the second lateral portion being uncovered.

18. The energy absorber of claim 11 , wherein the pressure adjuster comprises a valve and a valve controller configured to vary a flow area of the valve in response to a measured pressure inside the airbag.