Portable aircraft arresting apparatus

• US 4,809,933 A
• Filed: 02/21/1984
• Issued: 03/07/1989
• Est. Priority Date: 02/21/1984
• Status: Expired due to Term

• Current Assignee: Wickes Manufacturing Co.
• Original Assignee: Wickes Manufacturing Co.
• Inventors: Lopez, Edmond S., Buzby, Paul R., Kelly, Terence C., Reid, Paul D.
• Primary Examiner(s): Barefoot, Galen
• Application Number:
  US06/581,807
• Time in Patent Office: 1,841 Days
• Field of Search: 244/110 R, 244/110 G, 244/110 C, 244/114 R, 244/110 F, 244/110 A, 254/380, 254/327, 254/224
• US Class Current: 244/110.00C
• CPC Class Codes: B64F 1/02 for arresting aircraft, e.g. nets or cables
• CPC Class Codes: B64F 1/027 using net or mesh
• CPC Class Codes: B64F 1/029 using a cable or tether

Abstract

Portable aircraft arresting apparatus is comprised of a towable wheeled trailer providing a platform adapted to be anchored along a runway or landing strip and which carries component parts to selectively provide a cable-type or net-type aircraft arresting system. In connection with a net-type system, the platform includes a stanchion assembly including a stanchion mast. The mast is stored in a horizontal position relative to the platform and is elevated to an inclined position to support a net together with a like platform positioned on the opposite side of the landing strip. To accommodate selectivity and rapid conversion between cable and net-type systems, the platform on opposite sides of the landing strip are reversely oriented, and the stanchion assembly on one of the platforms is detached and reversely mounted on the platform for the inclined stanchion masts on opposite sides of the landing strip to be parallel to one another and inclined in the direction of landing.

Claims

1. Portable aircraft arresting apparatus comprising, portable platform means having opposite ends, means including energy absorber means on said platform means for said apparatus to be operable in a cable-type aircraft arresting system, means including said energy absorber means and stanchion mast means on said platform means for said apparatus to be operable in a net-type aircraft arresting system, frame means mounted on said platform means and supporting said stanchion mast means for pivotal displacement about a horizontal axis transverse to said opposite end and between horizontal and inclined positions relative to said platform means, said frame means having selectable first and second mounting positions relative to said platform means, said mast means in said first position of said frame means and in said horizontal position of said mast means being in a storage position between said opposite ends of said platform means, said mast means in said first and second positions of said frame means and in said inclined position of said mast means being inclined in opposite directions relative to said platform means, and hydraulic piston and cylinder means between said mast means and said frame means for pivoting said mast means about said axis between said horizontal and inclined positions, said mast means having outer and inner ends, and said axis being between said outer and inner ends and adjacent said inner end.

2. Apparatus according to claim 1, and means bracing said stanchion mast means in said inclined position against displacement relative to said platform means.

3. Apparatus according to claim 1, wherein said stanchion mast means is extendable and retractable in the direction transverse to said axis.

4. Apparatus according to claim 1, and interengaging stop means on said inner end and said frame means to locate said mast means in said inclined position relative to said platform means.

5. Apparatus according to claim 4, wherein said stop means includes a stop wheel on said inner end of said mast means and a stop pad on said frame means.

6. Apparatus according to claim 4, wherein said mast means includes axially slidably interengaged mast members providing for said mast means to be adjustable in length, and means to interconnect said mast members in any one of a plurality of different relative axial positions to provide selectable lengths for said mast means.

7. Apparatus according to claim 4, and further including first and second brace members respectively between said mast means and said frame means and between said mast means and said platform means when said mast means is in said inclined position, each said brace member being detachably connected at least to said mast means.

8. Apparatus according to claim 7, wherein said mast means includes axially slidably interengaged mast members providing for said mast means to be adjustable in length, and means to interconnect said mast members in any one of a plurality of different relative axial positions to provide selectable lengths for said mast means.

9. Apparatus according to claim 8, and winch means on said mast means, said winch means including crank means, and means for selectively mounting said winch means on said mast means for said crank means to be accessible from opposite sides of said mast means.

10. Portable aircraft arresting apparatus comprising, transportable platform means having opposite ends, means including energy absorber means on said platform means for said apparatus to be operable in a cable-type aircraft arresting system, means including said energy absorber means and a stanchion assembly on said platform means for said apparatus to be operable in a net-type aircraft arresting system, said stanchion assembly including frame means having opposite ends and selectively mountable on said platform means for said opposite ends of said frame means to be reversely oriented, a stanchion mast extending in the direction between said opposite ends of said frame means and having inner and outer ends, means supporting said inner end of said stanchion mast on said frame means for pivotal displacement of said mast about an axis transverse to said direction between said opposite ends of said frame means, fluid operated piston and cylinder means having opposite ends connected one to said mast and the other to said frame means and being operable to pivot said mast about said axis between horizontal and inclined positions relative to said platform means, the end of said piston and cylinder means connected to said mast being connected thereto between said axis and said inner end of said mast, said axis being closer to one end of said frame means than the other end end thereof and the end of said piston and cylinder means connected to said frame means being connected to said other end of said frame means, stop means on said mast and said frame means interengaging to locate said mast in said inclined position, and means to brace said mast in said inclined position against displacement relative to said frame means and platform means, said mast in one of said orientations of said frame means and in said horizontal position of said mast being disposed in a storage position between said opposite ends of said platform means.

11. Apparatus according to claim 10, wherein said stanchion mast comprises first and second telescopically and slidably interengaged mast members, and means to interconnect said mast members against relative displacement in any one of a plurality of selectable relative axial positions to provide for said mast to be adjustable in length.

12. Apparatus according to claim 11, and winch means on said mast, said winch means including crank means, and means for selectively mounting said winch means on said mast for said crank means to be accessible from opposite sides of said mast.

13. Apparatus according to claim 11, wherein said means to brace said mast includes a first brace member between said mast and said other end of said frame and a second brace member between said mast and said platform means and extending laterally of said mast, each said first and second brace members having an end detachably fastened to said mast, and said mast including means on laterally opposite sides thereof for fastening said end of said second brace member thereto.