Universal aircraft nosewheel cradle and tug assembly

• US 5,151,003 A
• Filed: 11/30/1990
• Issued: 09/29/1992
• Est. Priority Date: 11/30/1990
• Status: Expired due to Term

• Current Assignee: Lektro, Inc. (John Bean Technologies Corporation)
• Original Assignee: Eric W. Paulson
• Inventors: Zschoche, Robert A.
• Primary Examiner(s): Werner, Frank E.
• Assistant Examiner(s): ELLER JR, JAMES
• Application Number:
  US07/621,070
• Time in Patent Office: 669 Days
• Field of Search: 414/426, 414/428, 414/429, 414/430, 414/559, 280/402, 280/79.4, 180/904, 244/50
• US Class Current: 414/428
• CPC Class Codes: B64F 1/22 for handling aircraft
• CPC Class Codes: Y10S 180/904 Traction dollies for aircraft

Abstract

An aircraft tug assembly is provided for moving an aircraft on the ground. The tug assembly includes a self-propelled chassis responsive to operator control. A cradle assembly is pivotally attached to a front portion of the chassis. The cradle assembly has an adjustable nosewheel receiving apparatus comprising two lateral arms adjustably engaged with a rear gate to define a nosewheel receiving corral therebetween, with the corral sizable to accommodate varying sized aircraft nosewheels. The chassis has a winch for pulling an aircraft nosewheel onto the cradle assembly and into the corral. An optional front gate may be used to enclosed the nosewheel within the corral. Hydraulic actuators lift the cradle assembly with the nosewheel thereon so the tug assembly may move the aircraft without starting the aircraft engine.

Claims

1. An aircraft nosewheel cradle assembly for an aircraft tug, comprising:

a cradle member having an upper surface with a front edge, a transverse axis extending substantially parallel with the front edge, and a longitudinal axis perpendicular to the transverse axis and substantially parallel with the upper surface, pivot attachment means for pivotally attaching the cradle member to the tug for rotatable motion solely about said transverse axis between a lowered aircraft loading position and an elevated aircraft transport position;

means for moving said cradle member between said loading position and said transport position;

a pair of lateral substantially mutually parallel arms adjustably mounted to the upper surface of the cradle member substantially parallel with the longitudinal axis, means for adjustably mounting said lateral arms to provide lateral adjustment in a direction parallel to said transverse axis, each lateral arm having plural rear gate receiving means for mounting a rear gate thereto; and

a rear gate adjustably mounted to one of the plural rear gate receiving means on each of the lateral arms substantially parallel with the transverse axis, said plural rear gate receiving means providing longitudinal adjustment of said rear gate in a direction parallel to said longitudinal axis, so as to define an aircraft nosewheel receiving corral on the upper surface of the cradle member between the lateral arms and the rear gate, with the corral size adjustable to accommodate varying sized aircraft nosewheels.

2. An aircraft nosewheel cradle assembly according to claim 1 wherein:

the cradle member upper surface has a rear edge opposing the front edge;

the cradle assembly further includes a lateral arm guide shaft mounted to the cradle member substantially parallel with the transverse axis and adjacent the upper surface rear edge; and

each of the lateral arms is slidably mounted to the lateral arm guide shaft for movement in a direction substantially parallel to the transverse axis.

3. An aircraft nosewheel assembly according to claim 2 wherein:

the cradle member upper surface has a plurality of lateral arm positioning holes therethrough; and

each of the lateral arms has a lateral position guide pin slidably mounted thereto so as to engage one of the lateral arm positioning holes, so as to temporarily secure the lateral arms at a given position relative to the cradle member.

4. An aircraft nosewheel cradle assembly according to claim 1 wherein:

each of the lateral arms has an upper edge extending upwardly from the cradle member upper surface;

each of the plural rear gate receiving means of the lateral arms comprises a slot extending downwardly from the arm upper edge;

the rear gate includes a first wall having a first edge, with the first wall having a plurality of slots extending thereinto from the first edge; and

the lateral arm slots and the rear gate slots are alignable such that one slot on each lateral arm engages a rear gate slot.

5. An aircraft nosewheel assembly according to claim 4 wherein:

the rear gate first wall has a second edge opposing the first edge, the first wall also having a pair of opposing side edges; and

the rear gate further includes a second wall substantially perpendicular to the first wall and joined thereto along first wall second edge, the second wall having a pair of fingers each extending outwardly beyond the adjacent first wall opposing side edge, so as to allow the second wall fingers to engage the lateral arm slots when the lateral arms are positioned to receive the first wall therebetween, with the first wall substantially parallel with the cradle member upper surface.

6. An aircraft nosewheel assembly according to claim 1 wherein:

the cradle member upper surface has a rear edge opposing the front edge;

the cradle assembly further includes a rear wall extending upwardly from the cradle member upper surface rear edge and terminating in a stub shaft supporting wall which is substantially parallel to the cradle member upper surface, the cradle assembly also including a stub shaft extending upwardly from the stub shaft supporting surface; and

the rear gate has stub shaft receiving means for receiving the stub shaft so as to position the rear gate substantially coplanar with the rear wall to allow the rear wall to cooperate with the lateral arms and rear gate to form the aircraft nosewheel receiving corral.

7. An aircraft nosewheel cradle assembly according to claim 1 wherein:

each of the lateral arms includes front gate receiving means for mounting a front gate thereto; and

the assembly further includes a front gate mounted to the front gate receiving means of each lateral arm to enclose the aircraft nosewheel receiving corral.

8. An aircraft nosewheel cradle assembly according to claim 1 wherein:

the cradle member upper surface has a rear edge opposing the front edge;

the cradle member includes a back wall projecting upwardly from the upper surface adjacent said rear edge;

the assembly further includes a 3-point hitch assembly mounted to the back wall for attaching the cradle member to an aircraft tug having a 3-point hitch.

9. An aircraft nosewheel cradle assembly according to claim 1 wherein:

the cradle member upper surface includes two opposing side edges; and

the cradle member has a pair of side walls each extending upwardly from one of the upper surface side edges, each side wall including ram attachment means and said pivot attachment means for attaching the cradle assembly to the aircraft tug.

10. An aircraft tug assembly for moving an aircraft having a nosewheel, the tug assembly comprising:

a self-propelled chassis responsive to operator controlled means, the chassis having a front portion;

a nosewheel cradle assembly comprising;

a cradle member having an upper surface with a front edge, a transverse axis extending substantially parallel with the front edge, and a longitudinal axis perpendicular to the transverse axis and substantially parallel with the upper surface, pivot attachment means for pivotally attaching the cradle member to the chassis front portion for rotation solely, about said transverse axis between a lowered aircraft loading position and an elevated aircraft transport position;

means for moving said cradle member between said loading position and said transport position;

a pair of lateral substantially mutually parallel arms adjustably mounted to the upper surface of the cradle member substantially parallel with the longitudinal axis, means for adjustably mounting said lateral arms to provide lateral adjustment in a direction parallel to said transverse axis, each lateral arm having plural rear gate receiving means for mounting a rear gate thereto;

a rear gate adjustably mounted to one of the plural rear gate receiving means on each of the lateral arms substantially parallel with the transverse axis, said plural rear gate receiving means providing longitudinal adjustment of said rear gate in a direction parallel to said longitudinal axis, so as to define an aircraft nosewheel receiving corral on the upper surface of the cradle member between the lateral arms and the rear gate, with the corral size adjustable to accommodate varying sized aircraft nosewheels; and

winch means secured to the chassis for pulling the aircraft nosewheel onto the cradle member upper surface and into the aircraft nosewheel receiving corral.

11. An aircraft tug assembly according to claim 10 wherein:

the winch means comprises an electrically powered winch; and

the aircraft tug assembly further includes automatic winch shut-off means responsive to the presence of the aircraft nosewheel in the aircraft nosewheel receiving corral for deactivating the electrically powered winch when the nosewheel reaches said transport position.

12. An aircraft tug assembly according to claim 10 wherein:

the cradle member upper surface has a rear edge opposing the front edge;

the cradle assembly further includes a lateral arm guide shaft mounted to the cradle member substantially parallel with the transverse axis and adjacent the upper surface rear edge;

the cradle member upper surface has a plurality of lateral arm positioning holes therethrough; and

each of the lateral arms is slidably mounted to the lateral arm guide shaft for movement in a direction substantially parallel to the transverse axis, and each of the lateral arms has a lateral position guide pin slidably mounted thereto so as to engage one of the lateral arm positioning holes, so as to temporarily secure the lateral arms at a given position relative to the cradle member.

13. An aircraft tug assembly according to claim 10 wherein:

each of the lateral arms has an upper edge extending upwardly from the cradle member upper surface;

each of the plural rear gate receiving means of the lateral arms comprises a slot extending downwardly from the arm upper edge;

the rear gate includes a first wall having a first edge, with the first wall having a plurality of slots extending thereinto from the first edge; and

the lateral arm slots and the rear gate slots are alignable such that one slot on each lateral arm engages a rear gate slot.

14. An aircraft tug assembly according to claim 10 wherein:

the cradle member upper surface has a rear edge opposing the front edge;

the cradle member includes a back wall projecting upwardly from the upper surface adjacent said rear edge;

the aircraft tug assembly further includes a 3-point hitch; and

the cradle assembly includes a 3-point hitch assembly mounted to the back wall and attached to the tug assembly 3-point hitch.

15. An aircraft tug assembly according to claim 14 wherein:

the cradle member upper surface has a rear edge opposing the front edge and a plurality of lateral arm positioning holes therethrough;

the cradle assembly further includes a lateral arm guide shaft mounted to the cradle member substantially parallel with the transverse axis and adjacent the upper surface rear edge;

each of the lateral arms;

is slidably mounted to the lateral arm guide shaft for movement in a direction substantially parallel to the transverse axis,

has a lateral position guide pin slidably mounted thereto so as to engage one of the lateral arm positioning holes to temporarily secure the lateral arms at a given position relative to the cradle member,

has an upper edge extending upwardly from the cradle member upper surface,

plural rear gate receiving means each comprises a slot extending downwardly from the arm upper edge, and

has front gate receiving means for mounting a front gate thereto;

the rear gate includes;

a first wall having opposing first and second edges, with the first wall having a plurality of slots extending thereinto from the first edge, the first wall also having a pair of opposing side edges, and

a second wall substantially perpendicular to the first wall and joined thereto along first wall second edge, the second wall having a pair of fingers each extending outwardly beyond the adjacent first wall opposing side edge, so as to allow the second wall fingers to engage the lateral arm slots when the lateral arms are positioned to receive the first wall therebetween, with the first wall substantially parallel with the cradle member upper surface;

the lateral arm slots and the rear gate slots are alignable such that one slot on each lateral arm engages a rear gate slot; and

the assembly further includes a front gate mounted to the front gate receiving means of each lateral arm to enclose the aircraft nosewheel receiving corral.

16. An aircraft tug assembly according to claim 10 wherein:

the cradle member upper surface includes two opposing side edges;

the cradle member has a pair of side walls each extending upwardly from one of the upper surface side edges, each side wall including ram attachment means and said pivot attachment means for attaching the cradle assembly to the chassis;

the chassis includes a pivot attachment attached to the cradle member pivot attachment means; and

the aircraft tug assembly further includes an actuator coupling the cradle member ram attachment means to the chassis.

17. An aircraft tug assembly according to claim 16 wherein:

the cradle member upper surface has a rear edge opposing the front edge and a plurality of lateral arm positioning holes therethrough;

the cradle assembly further includes a lateral arm guide shaft mounted to the cradle member substantially parallel with the transverse axis and adjacent the upper surface rear edge;

each of the lateral arms;

is slidably mounted to the lateral arm guide shaft for movement in a direction substantially parallel to the transverse axis,

has a lateral position guide pin slidably mounted thereto so as to engage one of the lateral arm positioning holes to temporarily secure the lateral arms at a given position relative to the cradle member,

has an upper edge extending upwardly from the cradle member upper surface,

plural rear gate receiving means each comprises a slot extending downwardly from the arm upper edge, and

has front gate receiving means for mounting a front gate thereto;

the rear gate includes;

a first wall having opposing first and second edges, with the first wall having a plurality of slots extending thereinto from the first edge, the first wall also having a pair of opposing side edges, and

a second wall substantially perpendicular to the first wall and joined thereto along first wall second edge, the second wall having a pair of fingers each extending outwardly beyond the adjacent first wall opposing side edge, so as to allow the second wall fingers to engage the lateral arm slots when the lateral arms are positioned to receive the first wall therebetween, with the first wall substantially parallel with the cradle member upper surface;

the lateral arm slots and the rear gate slots are alignable such that one slot on each lateral arm engages a rear gate slot; and

the assembly further includes a front gate mounted to the front gate receiving means of each lateral arm to enclose the aircraft nosewheel receiving corral.