IP Library › Granted Patent US 10,486,790
Granted Patent B2
US 10,486,790 · App. 15/335,574 · Granted Nov 26, 2019

Maintenance step for a helicopter

Inventors: Christoph Steindl (Neusab, DE); Dominik Strobel (Fuenfstetten, DE)
Assignee: AIRBUS HELICOPTERS DEUTSCHLAND GmbH
B64C1/24B60R3/02
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Quick Facts
Patent No.
US 10,486,790
App. No.
15/335,574
Granted
Nov 26, 2019
Kind
B2
Abstract

A maintenance step for a helicopter, comprising: a casing that is adapted for integration into a lateral shell of a fuselage of a helicopter, and a step member that is pivotally mounted to the casing, wherein a stirrup unit is pivotally mounted to the step member, the stirrup unit comprising at least a first and a second section, the second section being telescopically mounted to the first section.

Claims (28)

1. A maintenance step for a helicopter, comprising:

a casing that is adapted for integration into a lateral shell of a fuselage of a helicopter, the casing includes a frame which is closed by a rear wall that is provided for closing up the lateral shell, and

a step member that is pivotally mounted to the casing,

wherein

a stirrup unit is pivotally mounted to the step member, the stirrup unit comprising at least a first and a second section, the second section is telescopically mounted to the first section;

wherein the step member is pivotally mounted to the casing around a first axis and the stirrup unit is pivotally mounted to the step member around a second axis, wherein the first axis and the second axis are perpendicular.

2. The maintenance step according to claim 1 , wherein the second section of the stirrup unit is at least approximately U-shaped and provides an ascendable stepping area.

3. The maintenance step according to claim 2 , wherein the ascendable stepping area is provided with anti-slip means.

4. The maintenance step according to claim 2 , wherein the stirrup unit comprises a third section that connects the first section to the second section, the third section is telescopically mounted to the first section and is further telescopically mounted to the second section.

5. The maintenance step according to claim 4 , wherein the stirrup unit is provided with securing pins that are adapted for restricting telescopic movement of the first, second and third sections relative to each other.

6. The maintenance step according to claim 1 , wherein the step member is provided with anti-slip means.

7. The maintenance step according to claim 1 , wherein a locking device is provided for locking the step member in the casing in a closed state of the maintenance step.

8. The maintenance step according to claim 1 , wherein the casing is provided with an overhang that is adapted for blocking the step member in an opened state of the maintenance step.

9. The maintenance step according to claim 1 , wherein the step member comprises a stepping plate that is provided with a covering plate, the covering plate is implemented as a filling part that is adapted for creating at least approximately a continuous surface with a lateral shell of a fuselage of a helicopter to which the maintenance step is mountable.

10. The maintenance step according to claim 9 , wherein the covering plate is attached to the stepping plate by means of associated fixing elements.

11. The maintenance step according to claim 1 , wherein an attachment rope or rod is provided, the attachment rope or rod is adapted for securing the step member in an opened state of the maintenance step to a lateral shell of a fuselage of a helicopter to which the maintenance step is mountable.

12. The maintenance step according to claim 1 , wherein a retaining element is provided, the retaining element is adapted for releasably retaining the stirrup unit at the step member in a retracted state of the stirrup unit.

13. The maintenance step according to claim 1 , wherein shim plates are associated with the step member, the shim plates is adapted for enabling a horizontal alignment of the step member independent of a respective inclination angle of the casing.

14. The maintenance step according to claim 1 , wherein the casing is provided with at least one slope that is adapted for preventing water accumulation in the casing.

15. A helicopter with a fuselage that comprises a lateral shell to which a maintenance step according to claim 1 is mounted.

16. A maintenance step for a helicopter, comprising:

a casing that is adapted for integration into a lateral shell of a fuselage of a helicopter, the casing includes a frame which is closed by a rear wall that is provided for closing the lateral shell, and

a step member that is pivotally mounted to the casing,

a stirrup unit is pivotally mounted to the step member, the stirrup unit comprising at least a first and a second section, the second section is telescopically mounted to the first section; and

wherein the step member is pivotally mounted to the casing around a first axis and the stirrup unit is pivotally mounted to the step member around a second axis, wherein the first axis and the second axis are offset relative to one another in a range between 30° and 60°.

17. The maintenance step according to claim 16 , wherein the second section of the stirrup unit is at least approximately U-shaped and provides an ascendable stepping area.

18. The maintenance step according to claim 17 , wherein the stirrup unit comprises a third section that connects the first section to the second section, the third section is telescopically mounted to the first section and is further telescopically mounted to the second section.

19. The maintenance step according to claim 16 , wherein the step member comprises a stepping plate that is provided with a covering plate, the covering plate is implemented as a filling part that is adapted for creating at least approximately a continuous surface with a lateral shell of a fuselage of a helicopter to which the maintenance step is mountable.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Oct 27, 2016
From: STEINDL, CHRISTOPH; STROBEL, DOMINIK
To: AIRBUS HELICOPTERS DEUTSCHLAND GMBH
Reel/Frame 040148/0089 →
Priority Claims (1)
EP 15400050 · Oct 29, 2015 · regional
Continuity (1)
Related Publication 20170121008A1 · May 4, 2017
Cited By (2)
US 12,545,190 US 12,662,233