IP Library Granted Patent US 8,473,189
Granted Patent B2
US 8,473,189 · App. 13/121,502 · Granted Jun 25, 2013

Helicopter having collision avoidance apparatus

Inventor: Kessler Christoph (Braunschweig, DE)
Assignee: Deutsches Zentrum für Luft- und Raumfahrt e.V.
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Quick Facts
Patent No.
US 8,473,189
App. No.
13/121,502
Granted
Jun 25, 2013
Kind
B2
Abstract

The invention relates to a helicopter, comprising a tail jib ( 12 ), at least one distance sensor ( 16.1 ) attached to the tail jib ( 12 ) for capturing a distance (A) from an object ( 18 ) that may be present in a surrounding area of the tail jib ( 12 ), and an electric evaluation unit ( 20 ), which is connected to the distance sensors ( 16 ) and equipped to calculate a position of the object ( 18 ) relative to the helicopter ( 10 ). According to the invention, a collision avoidance apparatus is provided, which is designed to avoid a collision of a person with the tail jib ( 12 ).

Claims (29)

1. A helicopter having

(a) a tail boom,

(b) at least one proximity sensor which is fitted to the tail boom, for detection of a distance to an object which is present approximately in the vicinity of the tail boom, and

(c) an electrical evaluation unit, which is connected to the proximity sensors and is designed to calculate a position of the object relative to the helicopter,

(d) the helicopter having a collision avoidance apparatus, which is designed to prevent a person from colliding with the tail boom,

(e) wherein said evaluation unit is designed to stop the tail rotor when the object is within a predetermined minimum distance of the tail rotor, and to check whether the helicopter is on the ground and to shut down the main rotor if the torque of the main rotor is high enough to cause rotational movement of the helicopter.

2. The helicopter as claimed in claim 1 , wherein that the collision avoidance apparatus is a warning apparatus for emission of a warning signal which can be perceived in the vicinity of the tail boom.

3. The helicopter as claimed in claim 1 the helicopter having

(i) a second proximity sensor and

(ii) at least one third proximity sensor,

(iii) with at least two of the proximity sensors differing with respect to their range, their resolution, their sensor direction and/or their sensor principle.

4. The helicopter as claimed in claim 1 , wherein

a tail rotor is attached to the tail boom,

with at least one proximity sensor being fitted at the center of rotation of the tail rotor.

5. The helicopter as claimed in claim 1 , wherein the evaluation unit is designed to calculate a speed of the object relative to the helicopter.

6. The helicopter as claimed in claim 1 , wherein the evaluation unit is designed

to compare the at least one position of the object with a protection area around the helicopter, and/or to extrapolate a trajectory of the object from the position of the object and its speed and

to output a signal when the object is in a protection area around the helicopter, and/or will be located there within a predetermined time interval.

7. The helicopter as claimed in claim 6 , wherein the evaluation unit is designed

to display the objects which are present in the vicinity on a chart of the area around the tail boom and,

to display the chart by means of a display appliance in a cockpit of the helicopter.

8. The helicopter as claimed in claim 1 , wherein

at least one proximity sensor has a sensor direction downward, and

the evaluation unit is designed to output a signal if a longitudinal attitude angle of the helicopter would lead to an impact with the tail boom.

9. A method for operation of a helicopter having a tail boom, having the following steps:

(a) automatic detection of a distance between the tail boom and an object which is present approximately in the vicinity of the tail boom,

(b) outputting a warning signal, which can be perceived in the vicinity of the tail boom,

(c) stopping the tail rotor if the distance is less than a predetermined minimum distance, and

(d) checking whether the helicopter is on the ground and shutting down the main rotor if the helicopter is on the ground and the torque of the main rotor is high enough to cause rotational movement of the helicopter.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded May 21, 2013
From: KESSLER, CHRISTOPH
To: DEUTSCHES ZENTRUM FUR LUFT- UND RAUMFAHRT E.V.
Reel/Frame 030458/0042 →
Priority Claims (1)
DE 10 2008 058 029 · Nov 18, 2008 · national
Continuity (1)
Related Publication 20110178711A1 · Jul 21, 2011