Apparatus for the optical inspection of the thermal protection tiles of a space shuttle
An apparatus for the inspection of the heat shield of a space shuttle has a drive so that it can automatically undertake an examination of the tiles of the heat shield. The apparatus moves over the surface with the aid of the drive, and images of the region to be inspected are produced with the aid of a camera. For these images, the tiles are illuminated subsequently by light sources from different directions, as a result of which the tiles can be reliably evaluated with regard to possible defects.
1. An apparatus for optical inspection of thermal protection tiles ( 11 ) of a surface ( 16 ) of a space shuttle comprising a support frame (S) which bears a camera (K) and at least two light sources (B),
the light sources (B) and the camera (K) being oriented towards the intended place of said surface ( 16 ), whereby the light sources (B) can be driven separately by a controller (C),
said support frame (S) has an actuator, which is able to move said camera (K) in a certain distance towards said surface (F) of the space shuttle,
wherein said actuator comprises a jet propulsion (P) which independently moves the frame in a space around the space shuttle.
2. The apparatus as claimed in claim 1 , wherein said support frame (S) comprises a spacer (D) which defines said certain distance between said camera (K) and said surface (F).
3. An apparatus for optical inspection of thermal protection tiles ( 11 ) of a surface ( 16 ) of a space shuttle comprising a support frame (S) which bears a camera (K) and at least two light sources (B),
the light sources (B) and the camera (K) being oriented towards the intended place of said surface ( 16 ), whereby the light sources (B) can be driven separately by a controller (C),
said support frame (S) has an actuator, which is able to move said camera (K) in a certain distance towards said surface (F) of the space shuttle,
wherein said support frame (S) comprises rolls (R) which move the apparatus along said surface of the space shuttle.
4. The apparatus as claimed in claim 2 , wherein said support frame (S) comprises a jet propulsion (P 1 ) which generates a propulsive force normal towards of the surface.
5. The apparatus as claimed in claim 1 , wherein said support frame (S) comprises a screen (N) for the purpose of shadowing a region of said surface to be inspected from the sun light.
6. The apparatus as claimed in claim 1 , wherein the light sources emit light of the same wavelength.
7. The apparatus as claimed in claim 1 ,
wherein the support frame (S) bears exactly four light sources (B).
8. The apparatus as claimed in claim 4 , wherein the support frame (S) bears exactly four light sources (B).
9. The apparatus as claimed in claim 3 , wherein said support frame (S) comprises a spacer (D) which defines said certain distance between said camera (K) and said surface (F).
10. The apparatus as claimed in claim 9 , wherein said support frame (S) comprises a jet propulsion (P 1 ) which generates a propulsive force normal towards of the surface.
11. The apparatus as claimed in claim 3 , wherein said support frame (S) comprises a screen (N) for the purpose of shadowing a region of said surface to be inspected from the sun light.
12. The apparatus as claimed in claim 3 , wherein the light sources emit light of the same wavelength.