IP Library Granted Patent US 9,720,011
Granted Patent B2
US 9,720,011 · App. 14/357,538 · Granted Aug 1, 2017

Monitoring device and method for monitoring a movement profile of a user in the region of an actuating element of an aircraft or spacecraft

Inventor: Christian Riedel (Bliedersdorf, DE)
Assignee: Airbus Operations GmbH
G01P13/00B64C1/1407B64D25/14B64D45/00B64G1/66B64D2045/004
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Quick Facts
Patent No.
US 9,720,011
App. No.
14/357,538
Granted
Aug 1, 2017
Kind
B2
Abstract

A monitoring device for monitoring a movement profile of a user in the region of an actuating element of an aircraft or spacecraft, having at least one movement sensor which is configured to detect a first monitoring space of the monitoring device and at the same time a second monitoring space of the monitoring device which differs from the first monitoring space. Also a method for monitoring a movement profile of a user in the region of an actuating element of an aircraft or spacecraft, with: detection of a first monitoring space of the monitoring device by at least one movement sensor; and simultaneous detection of a second monitoring space, which is different from the first monitoring space, by the at least one movement sensor.

Claims (22)

1. A monitoring device for monitoring a movement profile of a user in the region of an actuating element of an aircraft or spacecraft, comprising:

at least one movement sensor which is configured to detect a first monitoring space of the monitoring device and at the same time a second monitoring space of the monitoring device which differs from the first monitoring space;

a first detection region, which is elliptically shaped; and

a second detection region, which is elliptically shaped, the first detection region and the second detection region extending from the monitoring device along their respective major axes and overlapping each other at least in portions, the first detection region representing the first monitoring space of the monitoring device, and a differential region of the first detection region and of the second detection region, which can only be detected by the second detection region, representing the second monitoring space of the monitoring device;

wherein the detection regions are configured spatially with a length along the respective major axis of the second detection region being greater than a length along the respective major axis of the first detection region, and

wherein the major axis of the first detection region is arranged coaxially to the major axis of the second detection region.

2. The monitoring device according to claim 1 , wherein the monitoring device comprises a control device which is configured to compare an output signal from the at least one movement sensor with values of a table of values stored in the control device.

3. The monitoring device according to claim 2 , wherein first monitoring space values of the table of values are associated with the first monitoring space and second monitoring space values of the table of values are associated with the second monitoring space.

4. The monitoring device according to claim 2 , wherein associated with each door of the aircraft or spacecraft is a table of values adapted to the respective door, the table of values being stored in the control device of the monitoring device.

5. The monitoring device according to claim 1 , wherein the monitoring device has a first movement sensor to produce the first detection region and a second movement sensor to produce the second detection region.

6. The monitoring device according to claim 1 , wherein the major axis of the first detection region is arranged obliquely at an angle to the major axis of the second detection region.

7. The monitoring device according to claim 1 further comprising:

a door for an aircraft or spacecraft.

8. The monitoring device according to claim 1 further comprising an aircraft or spacecraft.

9. A method for monitoring a movement profile of a user in the region of an actuating element of an aircraft or spacecraft, comprising:

detecting a first monitoring space of the monitoring device using at least one movement sensor; and

simultaneously detecting a second monitoring space, which is different from the first monitoring space, using the at least one movement sensor;

producing a first detection region, which is elliptically shaped; and

producing a second detection region, which is elliptically shaped, the first detection region and the second detection region extending from the monitoring device along their respective major axes and overlapping one another at least in portions, the first detection region monitoring the first monitoring space of the monitoring device and a differential region of the first detection region and of the second detection region, which is only monitored by the second detection region, monitoring the second monitoring space of the monitoring device;

wherein the detection regions are configured spatially with a length along the respective major axis of the second detection region being greater than a length along the respective major axis of the first detection region, and

wherein the major axis of the first detection region is arranged coaxially to the major axis of the second detection region.

10. The method according to claim 9 , wherein, when an object moves into the first monitoring space, a first signal is output by the monitoring device and when the object moves into the second monitoring space, a second signal which is different from the first signal is output.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Sep 11, 2014
From: RIEDEL, CHRISTIAN
To: AIRBUS OPERATIONS GMBH
Reel/Frame 033720/0968 →
Priority Claims (1)
DE 10 2011 086 454 · Nov 16, 2011 · national
Continuity (2)
Provisional Application 61560493 · Nov 16, 2011
Related Publication 20140345396A1 · Nov 27, 2014