Automatic video projection screen
First Claim
1. A screen for an aircraft video projection system wherein said system generates a projected image, comprising:
- first and second rotatable pulleys oriented substantially parallel relative to each other, said first and second pulleys each having a cylindrical shape and said first pulley further including an interior hollow;
a belt having a viewing surface, wherein said belt is positioned in contact around said first and second pulleys and is moveable between a viewing position in which said viewing surface is exposed for display of said projected image and a stored position in which said viewing surface is hidden;
detection means for detecting whether said viewing surface is exposed or hidden; and
rotating means for rotating said first pulley to move said belt to said viewing position upon detection that said viewing surface is hidden, wherein said rotating means is affixed within said hollow.
3 Assignments
0 Petitions
Accused Products
Abstract
A screen for an aircraft video projection system. The screen includes a frame for attachment to an aircraft cabin surface and cylindrically shaped first and second pulleys rotatably mounted to the frame. In addition, the first and second pulleys are oriented substantially parallel relative to each other and the first pulley includes an interior hollow. The screen further includes a belt having a viewing surface and an indexing hole adjacent to the viewing surface. The belt is positioned in contact around the first and second pulleys and is moveable between a viewing position in which the viewing surface is exposed for display of the projected image and a stored position in which the viewing surface is hidden. The belt also serves as a heat absorbing layer. A light sensor is positioned opposite the belt. The light sensor serves to detect the presence of the indexing hole. In particular, if the indexing hole is positioned opposite the sensor, the sensor indicates that the viewing surface is exposed. Further, if the indexing hole is not positioned opposite the indexing hole, the sensor indicates that the viewing surface is hidden. In addition, the screen includes a gearmotor affixed within the hollow. The gearmotor serves to rotate the first pulley to move the belt to the viewing position upon detection that the viewing surface is hidden, wherein the gearmotor is affixed within the hollow.
21 Citations
19 Claims
-
1. A screen for an aircraft video projection system wherein said system generates a projected image, comprising:
-
first and second rotatable pulleys oriented substantially parallel relative to each other, said first and second pulleys each having a cylindrical shape and said first pulley further including an interior hollow; a belt having a viewing surface, wherein said belt is positioned in contact around said first and second pulleys and is moveable between a viewing position in which said viewing surface is exposed for display of said projected image and a stored position in which said viewing surface is hidden; detection means for detecting whether said viewing surface is exposed or hidden; and rotating means for rotating said first pulley to move said belt to said viewing position upon detection that said viewing surface is hidden, wherein said rotating means is affixed within said hollow. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9)
-
-
10. A screen for an aircraft video projection system wherein said system generates a projected image, comprising:
-
a frame for attachment to an aircraft cabin surface; first and second pulleys rotatably mounted to said frame and oriented substantially parallel relative to each other, said first and second pulleys each having a cylindrical shape and said first pulley further including an interior hollow for defining an inner wall; a belt having a viewing surface, wherein said belt is positioned in contact around said first and second pulleys and is moveable between a viewing position in which said viewing surface is exposed for display of said projected image and a stored position in which said viewing surface is hidden; detection means for detecting whether said viewing surface is exposed or hidden; and a gearmotor having a disc element affixed to said inner wall, said gearmotor being adapted to rotate said disc element and thus said first pulley to move said belt to said viewing position upon detection that said viewing surface is hidden. - View Dependent Claims (11, 12, 13, 14, 15, 16)
-
-
17. An aircraft video projection system, comprising:
-
a frame for attachment to an aircraft cabin surface; first and second pulleys rotatably mounted to said frame and oriented substantially parallel relative to each other, said first and second pulleys each having a cylindrical shape and said first pulley further including an interior hollow for defining an inner wall; projection means for generating a projected image; a belt having a viewing surface and an indexing hole adjacent said viewing surface, wherein said belt is positioned in contact around said first and second pulleys and is moveable between a viewing position in which said viewing surface is exposed for display of said projected image and a stored position in which said viewing surface is hidden, said belt being fabricated from a flexible sheet of thin metal for further use of said belt as a heat absorption layer; a sensor for detecting said indexing hole, said sensor being located opposite said belt wherein if said hole is opposite said sensor, light generated by said sensor is not reflected back to said sensor thus indicating that said viewing surface is exposed and wherein if said hole is not opposite said sensor, light generated by said sensor is reflected back to said sensor thus indicating that said viewing surface is hidden; and a gearmotor having a disc element affixed to said inner wall, said gearmotor being adapted to rotate said disc element and thus said first pulley to move said belt to said viewing position upon detection that said viewing surface is hidden. - View Dependent Claims (18, 19)
-
Specification