Passenger door with deployable lower step

Patent metadata

Field	Value
Publication number	US-11186353-B2
Application number	US-201916696099-A
Country	US
Kind code	B2
Filing date	Nov 26, 2019
Priority date	Nov 27, 2018
Publication date	Nov 30, 2021
Grant date	Nov 30, 2021

Abstract

A mobile platform with a passenger door system having stairs with one or more deployable lower steps and associated methods for deployment and/or stowing of such lower steps are disclosed. In one embodiment, the method comprises using movement of the door to drive a movement of a handrail associated with the stairs, and using the movement of the handrail to drive a movement of the one or more lower steps.

First claim

What is claimed is:

1. An aircraft comprising:
a fuselage;
a door pivotally coupled to the fuselage, the door having an interior side facing an interior of the aircraft when the door is closed and an exterior side facing an exterior of the aircraft when the door is closed, the interior side of the door defining an airstair permitting passengers to board the aircraft when the door is open, the airstair having a lower step deployable from a stowed configuration when the door is closed to a deployed configuration when the door is open, the airstair including a plurality of non-deployable steps that are higher than the lower step when the door is open;
a handrail associated with the airstair, the handrail being deployable from a stowed configuration when the door is closed to a deployed configuration when the door is open, a deployment of the handrail being coordinated with an opening of the door, the handrail being drivingly coupled to the lower step via a mechanism including:
a rotatable first shaft drivingly coupled to the handrail so that the deployment of the handrail drives a rotation of the first shaft; and
a rotatable second shaft drivingly coupled to the first shaft and to the lower step so that rotation of the first shaft drives a rotation of the second shaft, and that the rotation of the second shaft drives a deployment of the lower step;
a first connecting rod having a first end coupled to the first shaft via a first crank and an opposite second end; and
the second shaft drivingly coupled to the second end of the first connecting rod so that rotation of the first shaft causes movement of the first connecting rod which drives the rotation of the second shaft,

wherein the mechanism is hidden from view by the plurality of non-deployable steps.

2. The aircraft as defined in claim 1 , wherein:
the handrail is pivotally coupled to the fuselage and coupled to the door via a support link;
a first end of the support link is pivotally coupled to the handrail;
an opposite second end of the support link is pivotally coupled to the door; and
the second end of the support link is drivingly coupled to the first shaft so that rotation of the support link caused by the deployment of the handrail drives the rotation of the first shaft.

3. The aircraft as defined in claim 1 , comprising a second crank coupled for common rotation with the second shaft, wherein:
the second shaft is parallel and spaced apart from the first shaft; and
the second end of the first connecting rod is coupled to the second crank so that movement of the first connecting rod causes rotation of the second shaft.

4. The aircraft as defined in claim 3 , wherein the second shaft is drivingly coupled to the lower step via a second connecting rod.

5. The aircraft as defined in claim 4 , wherein the second connecting rod is coupled to the second shaft via a third crank coupled for common rotation with the second shaft.

6. The aircraft as defined in claim 5 , wherein:
the lower step is a first lower step that is a lowermost step on the airstair when the door is open;
the airstair comprises a second lower step immediately succeeding the first lower step;
the second lower step is deployable from a stowed configuration when the door is closed to a deployed configuration when the door is open; and
the first and second lower steps are coupled together for coordinated deployment.

7. The aircraft as defined in claim 6 , wherein:
the first lower step is rotatable about a first rotation axis;
the second lower step is rotatable about a second rotation axis different from the first rotation axis;
the second connecting rod is coupled to the second lower step to cause rotation of the second lower step about the second rotation axis; and
the second lower step is drivingly coupled to the first lower step via an arm to cause rotation of the first lower step about the first rotation axis.

8. The aircraft as defined in claim 1 , wherein:
the lower step is a first lower step that is a lowermost step on the airstair when the door is open;
the airstair comprises a second lower step immediately succeeding the first lower step;
the second lower step is deployable from a stowed configuration when the door is closed to a deployed configuration when the door is open; and
the first and second lower steps are coupled together for coordinated deployment.

9. The aircraft as defined in claim 1 , wherein the handrail is drivingly coupled to the lower step via a load transfer path defined by:
a support link having a first end pivotally coupled to the handrail and an opposite second end;
the rotatable first shaft drivingly coupled to the second end of the support link;
the rotatable second shaft drivingly coupled to the second end of the first connecting rod via a second crank; and
a second connecting rod having a first end coupled to the second shaft via a third crank and an opposite second end drivingly coupled to the lower step.

10. A passenger door system for a mobile platform, the system comprising:
a door configured to be pivotally coupled to a structure of the mobile platform, the door having an interior side facing an interior of the mobile platform when the door is closed and an exterior side facing an exterior of the mobile platform when the door is closed, the interior side of the door defining stairs permitting passengers to board the mobile platform when the door is open, the stairs comprising a lower step deployable from a stowed configuration when the door is closed to a deployed configuration when the door is open, the stairs including a plurality of non-deployable steps that are higher than the lower step when the door is open;
a handrail associated with the stairs, the handrail being deployable from a stowed configuration when the door is closed to a deployed configuration when the door is open, a deployment of the handrail being coordinated with an opening of the door, the handrail being drivingly coupled to the lower step via a mechanism including:
a rotatable first shaft drivingly coupled to the handrail so that the deployment of the handrail drives a rotation of the first shaft; and
a rotatable second shaft drivingly coupled to the first shaft and to the lower step so that rotation of the first shaft drives a rotation of the second shaft, and that rotation of the second shaft drives a deployment of the lower step;
a first connecting rod having a first end coupled to the rotatable first shaft via a first crank and an opposite second end; and
the rotatable second shaft drivingly coupled to the second end of the first connecting rod so that rotation of the first shaft causes movement of the first connecting rod which drives the rotation of the rotatable second shaft,

wherein the mechanism is hidden from view by the plurality of non-deployable steps.

11. The system as defined in claim 10 , wherein:
the handrail is coupled to the door via a support link;
a first end of the support link is pivotally coupled to the handrail;
an opposite second end of the support link is pivotally coupled to the door; and
the second end of the support link is drivingly coupled to the first shaft so that rotation of the support link caused by the deployment of the handrail drives the rotation of the first shaft.

12. The system as defined in claim 10 , comprising:
a second crank coupled for common rotation with the second shaft;
wherein:
the second shaft is parallel and spaced apart from the first shaft; and
the second end of the first connecting rod is coupled to the second crank so that movement of the first connecting rod causes rotation of the second shaft.

13. The syst

Assignees

• Bombardier Inc

Inventors

• Savidge John Richard

Classifications

• B64C1/1423 Primary

  Passenger doors · CPC title

• B64C1/1461

  Structures of doors or surrounding frames · CPC title

• B64C1/24 Primary

  Steps mounted on, and retractable within, fuselages · CPC title