Auxillary rolling system for aircraft

• US 4,915,324 A
• Filed: 04/19/1988
• Issued: 04/10/1990
• Est. Priority Date: 04/24/1987
• Status: Expired due to Term

• Current Assignee: Airbus France
• Original Assignee: Aerospatiale Societe Nationale Industrielle
• Inventors: Pichon, Alain, Foreau, Bernard, Nazair-Blanc, Claude
• Primary Examiner(s): Barefoot, Galen
• Application Number:
  US07/183,230
• Time in Patent Office: 721 Days
• Field of Search: 244/100 R, 244/102 R, 244/102 SS, 244/104 R, 244/104 FP
• US Class Current: 244/102.00R
• CPC Class Codes: B64C 25/34 wheeled type, e.g. multi-wheeled bogies
• CPC Class Codes: B64C 25/66 Convertible alighting gear; Combinations of different kinds of ground or like engaging elements

Abstract

This invention relates to a rolling system for aircraft, comprising telescopic landing gears which abut on the ground via wheels and which present a variable length as a function of the load applied thereto by said aircraft. According to the invention, this system comprises at least one jack assembly capable of outwardly pressing at least one rolling member with a constant force and said rolling member is placed in contact with the ground only after impact of the telescopic landing gears and when the length of said telescopic landing gears corresponds to a predetermined load threshold applied thereto, said threshold being less than the load corresponding to take-off.

Claims

1. A rolling system for aircraft, comprising telescopic landing gears which abut on the ground via wheels and which present a variable length as a function of the load which is applied thereto by said aircraft;

wherein it comprises at least one jack assembly capable of outwardly pressing at least one rolling member having a constant force and said jack assembly is capable of communicating to said rolling member at least two relative positions of retraction with respect to the wheels of said telescopic landing gears, the first of these positions being such that such rolling member is maintained spaced apart from the ground wherever the compression of said telescopic landing gears under the load that is applied thereto by the aircraft, whilst the second of said positions is such that said rolling member is placed in contact with the ground when the length of said telescopic landing gears corresponds to a predetermined load threshold applied thereto, said threshold being less than the load corresponding to take-off;

wherein said jack assembly comprises a cylinder the cavity of which is provided with a projection separating said cavity into two communicating chambers, one of said chambers containing a piston provided with a rod opposite said projection and hermetically passing through the corresponding bottom of said cylinder, a first orifice for passage of fluid disposed in the vicinity of said projection and in simultaneous communication with the two communicating chambers, a second orifice in the vicinity of the bottom of said cylinder for passage of fluid disposed in said chamber containing said piston, and a line for supply of hydraulic fluid at constant pressure and a line for return of hydraulic fluid, capable of being alternately connected to said first and second orifices via a valve.

2. The system of claim 1,

wherein said jack assembly provided with its rolling member forms a leg articulated beneath the fuselage or beneath the wings of the aircraft and adapted to occupy either a retracted position inside said fuselage or said wings, or an extended, at least substantially vertical position.

3. The system of claim 2, wherein said leg may take a retracted position and an extended position.

4. The system of claim 3, wherein, when said leg is both in extended position and in retracted position, when the aircraft rests on the ground in stopped position, the rolling member is distant from the ground.

5. The system of claim 3, wherein, when said leg is both in extended position and in position of extension and when no load is applied on the landing gears, the lowermost point of the rolling member of said leg lies, above the lowermost point of the wheels of the landing gears, at a distance corresponding to the compression thereof when said predetermined load threshold is applied thereto.

6. The system of claim 1,

wherein said jack assembly comprises:

a jack of which the cavity of the cylinder is provided with a projection separating said cavity into two communicating chambers, one of said chambers containing a piston provided with a rod opposite said projection and hermetically passing through the corresponding bottom of said cylinder;

a first orifice for passage of fluid disposed in the vicinity of said projection and in simultaneous communication with the two communicating chambers;

a second orifice for passage of fluid disposed in said chamber containing said piston, in the vicinity of said corresponding bottom of said cylinder; and

a line for supply of hydraulic fluid at constant pressure and a line for return of hydraulic fluid, capable of being alternately connected to said first and second orifices via a valve.

7. The system of claim 6, wherein, in the other of said chambers of the cylinder, there is disposed a floating piston defining, between itself and the bottom of the cylinder opposite the bottom traversed by said piston rod, a tight enclosure which contains an elastically compressible gaseous fluid.

8. The system of claim 6, wherein a relief valve is disposed between said first orifice for passage of fluid and said fluid return line.