Landing device for a low gravity lander

Patent metadata

Field	Value
Publication number	US-10179663-B2
Application number	US-201615209316-A
Country	US
Kind code	B2
Filing date	Jul 13, 2016
Priority date	Jul 15, 2015
Publication date	Jan 15, 2019
Grant date	Jan 15, 2019

Abstract

A landing device for a low gravity lander having a main body. The landing device comprises a number of leg-like rods attached to the main body, wherein, in a deployment position of the rods, each of the number of rods is inclined with regard to a plane of a first side surface of the main body such that the rods substantially extend in a direction of movement of the low gravity lander. Furthermore, the number of rods is made such that they bend or buckle under forces within a predetermined range by an impact due to a landing on a landing surface, thereby absorbing an impact momentum.

First claim

The invention claimed is:

1. A landing device for a low gravity lander having a main body, the landing device comprising a number of leg-like rods attached to the main body, wherein, in a deployment position of the rods during landing, each of the rods is inclined with regard to a plane of a first side surface of the main body such that the rods substantially extend in a direction of movement of the low gravity lander during landing, and wherein the rods are configured to bend or buckle under forces within a predetermined range by an impact due to the landing on a landing surface, thereby absorbing an impact momentum,
wherein, in a stowing position, the rods are stowed above each other such that the rods substantially extend parallel to the plane of the first side surface.

2. The landing device according to claim 1 , wherein the number of rods is greater than 3 or equals 4.

3. The landing device according to claim 1 , wherein a length of the rods is determined as a function of an inclination angle with regard to the plane of the first side surface and an expected roughness of the landing surface such that no part of the landing surface is supposed to contact the main body.

4. The landing device according to claim 1 , wherein a length of the rods is determined as a function of stowage space such that, in a stowage position, the rods do not extend beyond the plane of the first side surface of the main body.

5. The landing device according to claim 1 , wherein an inclination angle of the number of rods with regard to the plane of the first side surface is in a range between 120° and 150° or particularly 135°.

6. The landing device according to claim 1 , wherein the number of rods extends, in the deployment position, beyond lateral edges of the first side surface.

7. The landing device according to claim 1 , wherein the rods are hollow.

8. The landing device according to claim 1 , wherein a thickness and/or material of the rods is determined as a function of expected impact momentum.

9. The landing device according to claim 1 , wherein a free end of at least some of the rods is bent.

10. The landing device according to claim 1 , wherein a free end of at least some of rods is fitted with a disc.

11. The landing device according to claim 1 , wherein the rods are deployable by a swiveling mechanism.

12. The landing device according to claim 1 , wherein, in a stowing position, the rods are held/locked by a single hold down device.

13. The landing device according to claim 1 , wherein the landing device comprises an activatable launch lock to prevent premature deployment, the launch lock being a time release device which enables a deployment of the rods from their stowage position to their deployment position upon a triggering event.

14. The landing device according to claim 1 , wherein the main body comprises a second side surface arranged opposite to the first side surface of the main body, wherein a further number of leg-like rods is assigned to or attached to the second side surface.

15. A low gravity lander comprising a main body and a landing device according to claim 1 .

Assignees

• Airbus Ds Gmbh

Inventors

• Knirsch Ulrich

Classifications

• B64G1/2228 Primary

  characterised by the hold-down or release mechanisms · CPC title

• B64G1/62 Primary

  Systems for re-entry into the earth's atmosphere; Retarding or landing devices · CPC title

• B64G1/222

  for deploying structures between a stowed and deployed state · CPC title

• B64G2001/1071

  Operations & Transport · mapped topic

• B64G1/625

  Landing devices; Undercarriages · CPC title