Aircraft video monitor deployment and retraction apparatus

• US 5,583,735 A
• Filed: 01/18/1994
• Issued: 12/10/1996
• Est. Priority Date: 01/18/1994
• Status: Expired due to Fees

• Current Assignee: Hollingsead International Incorporated
• Original Assignee: Hollingsead International Incorporated
• Inventors: Pease, Raymond J., Rice, Mark X.
• Primary Examiner(s): FLEMING, FRITZ M
• Application Number:
  US08/183,606
• Time in Patent Office: 1,057 Days
• Field of Search: 248/917-924, 348/825, 348/826, 348/827, 361/170, 361/681, 361/682, 307/9.1, 307/119, 307/122, 307/124, 312/7.2, 353/79
• US Class Current: 361/170
• CPC Class Codes: A47B 81/065 rotationally
• CPC Class Codes: B64D 11/0015 Arrangements for entertainment or communications, e.g. radio, television
• CPC Class Codes: B64D 11/00153 Monitors mounted on or in the seat other than the seat back
• CPC Class Codes: H04N 5/64 Constructional details of receivers, e.g. cabinets or dust covers furniture aspects of television cabinets A47B81/06
• CPC Class Codes: Y10S 248/917 Video display screen support

Abstract

A video monitor deployment/retraction apparatus includes a frame located in an aircraft overhead compartment and a monitor pivotally mounted on the frame for rotation between a stored and a deployed position. A spring biases the monitor to its stored position where is releasably retained by a locking mechanism. A solenoid and actuating arms selectively disable the locking mechanism to allow the monitor to be lowered to its deployed position and enable a latching mechanism when the monitor has reached its deployed position to retain the monitor in that position. The latching means is disabled when the monitor is bumped by a passenger while in the deployed position to allow the spring to return the monitor to the stored position.

Claims

1. In a video screen deployment and retraction apparatus for use in an overhead storage compartment of an aircraft the combination comprising:

a) a frame adapted to be mounted in the compartment;

b) a video screen mounted in the frame for pivotal movement about a pivotal axis between a stored portion and a deployed operational position for viewing by passengers;

c) bias means for biasing the screen toward its stored position;

d) latching means for holding the screen in its deployed position; and

e) latching release means including a solenoid responsive to a predetermined movement of the screen in either direction about its pivotal axis in the deployed position for disabling the latching means whereby the biasing means retracts the screen to its stored position, the latching means including means for energizing the solenoid and the latching release means including means for deenergizing the solenoid.

2. The invention of claim 1 further including a locking pin for selectively holding the screen in its stored position, the solenoid being coupled to the locking pin and whereby the latching means includes means for energizing the solenoid to disable the locking pin whereby the screen may be pivoted from its stored to its deployed position when the locking pin is disabled.

3. The invention of claim 1 further including means for controlling the rate of movement of the screen from its deployed to its stored position.

4. The invention of claim 3 wherein the means for de-energizing the solenoid includes a latching switch responsive to movement of the screen from its deployed position in a clockwise or counterclockwise direction in excess of about 2-10 degrees about the pivot axis.

5. The invention of claim 4 wherein the latching release means further includes a cam carried by the screen for activating the latching switch to energize the solenoid when the screen is moved to its deployed position and to de-energize the solenoid when the screen is rotated clockwise or counterclockwise in excess of said 2-10 degrees from the deployed position.

6. The invention of claim 5 further including a handle coupled to the screen whereby an operator may deploy the screen by rotating the handle.

7. The invention of claim 6 further including means for allowing the handle to rotate through an angle within the range of about 10°

-20°

before engaging the screen in its stored position.

8. A video monitor deployment and retraction apparatus for use in an aircraft overhead storage compartment having a generally horizontally oriented bottom wall with an opening therein to accommodate the monitor in its stored position comprising:

a) a frame mounted in the storage compartment;

b) a video monitor positioned within the opening and mounted on a shaft rotatably carried by the frame, the monitor being arranged to rotate with the shaft between a stored position in which the monitor is located within the compartment facing the opening therein and a deployed position in which the monitor is located in a downwardly extending position for viewing by an aircraft passenger;

c) a spring coupled between the shaft and the frame for biasing the monitor to the stored position;

d) a source of current;

e) a solenoid;

f) a locking arm and a latching pin coupled to the solenoid, the locking pin being arranged to retain the monitor in the stored position when the solenoid is not connected to the current source and to release the monitor from the stored position when the solenoid is connected to the current source, the latching arm being arranged to retain the monitor in the deployed position when the solenoid is connected to the current source and to release the monitor from the deployed position when the solenoid is not connected to the current source;

g) first and second switches connected between the current source and the solenoid;

h) means for operating the first and second switches in response to the position of the monitor so that the solenoid is connected to the current source when the monitor is in the stored position and in the deployed position to allow the monitor to be lowered to the deployed position and retained in that position; and

i) means responsive to the movement of the monitor through a pre-set angle within the range of about 2°

-10°

on either side of the deployed position for operating one of the switches to disconnect the solenoid from the current source to allow the spring to return the monitor to the stored position.

9. The invention of claim 8 wherein the means for operating the switches to connect the solenoid to the current source includes first and second cams responsive to the position of the monitor.

10. The invention of claim 9 wherein the first cam is arranged to operate the first switch to connect the solenoid to the current source when the monitor is in the stored position.

11. The invention of claim 10 wherein the first and second cams are arranged to connect the first and second switches in series between the current source and the solenoid when the monitor is in the deployed position.

12. The invention of claim 11 wherein the second cam is arranged to operate the second switch to disconnect the solenoid from the first switch and current source when the monitor is moved through said pre-set angle relative to the deployed position, whereby the spring will rotate the monitor to its stored position.

13. The invention of claim 8 further including means for controlling the rate of rotation of the monitor between its deployed and stored positions.

14. The invention of claim 13 wherein the rate of rotation controlling means includes a hydraulic cylinder.

15. The invention of claim 8 further including a handle rotatably mounted on the shaft and arranged to engage the monitor and rotate the monitor to its deployed position.

16. The invention of claim 15 further including a handle return spring for biasing the handle in a direction to rotate the handle to a stored position within the compartment.

17. The invention of claim 16 wherein the handle is arranged to rotate through a predetermined angle within the range of about 10°

-30°

from its stored position before engaging the monitor whereby an operator may grasp the handle and rotate it through said predetermined angle against only the handle return spring.

18. The invention of claim 8 wherein the means for operating the first switch to connect the solenoid to the current source includes a gear train and a rack, the rack being arranged to move linearly in response to rotational movement of the monitor.

19. The invention of claim 18 wherein the latching arm is arranged to engage and prevent movement of the rack when the monitor is in the deployed position.

20. A video monitor deployment and retraction apparatus for use in an aircraft overhead storage compartment having a generally horizontally oriented bottom wall with an opening therein to accommodate the monitor in its stored position comprising:

a) a frame mounted in the storage compartment;

b) a video monitor positioned within the opening and pivotally mounted to the frame, the monitor being arranged to rotate between a stored position in which the monitor is located substantially within the compartment facing the opening therein and a deployed position in which the monitor is located in a downwardly extending position for viewing by an aircraft passenger;

c) bias means for biasing the monitor to its stored position;

d) a locking pin for selectively retaining the monitor in the stored position;

e) a latching arm for selectively retaining the monitor in the deployed position when enabled;

f) a solenoid coupled to the locking pin and the latching arm, the locking pin retaining the monitor in the stored position when the solenoid is deenergized and the latching arm retaining the monitor in the deployed position when the solenoid is energized;

g) means for energizing the solenoid when the monitor has reached the deployed position;

h) means for selectively deenergizing the solenoid when the monitor is in the deployed position to allow the bias means to return the monitor to the stored position; and

i) the means for deenergizing the solenoid including means responsive to a predetermined minimum rotational movement of the monitor in a clockwise or counterclockwise direction from its deployed position.

21. The invention of claim 20 wherein the means for deenergizing the solenoid further includes means responsive to a failure of electrical power in the aircraft.

22. The invention of claim 20 further including a handle rotatably mounted on the frame and arranged to engage the monitor and rotate the monitor to its deployed position.

23. The invention of claim 22 further including a handle return spring for biasing the handle in a direction to rotate the handle to a stored position within the compartment.

24. The invention of claim 23 wherein the handle is arranged to rotate through a predetermined angle within the range of about 10°

-30°

from its stored position before engaging the monitor whereby an operator may grasp the handle and rotate it through said predetermined angle against only the handle return spring.

25. The invention of claim 20 further including means for controlling the rate of movement of the monitor from its deployed to its stored position.

26. The invention of claim 31 wherein the means for de-energizing the solenoid includes a latching switch responsive to movement of the monitor from its deployed position in a clockwise or counterclockwise direction about the pivot axis.

27. The invention of claim 26 wherein the means for selectively deenergizing the solenoid further includes a cam carried by the monitor for rotation therewith and a switch responsive to movement of the cam.