Combiner mounting and stowage mechanism

• US 4,664,475 A
• Filed: 08/14/1985
• Issued: 05/12/1987
• Est. Priority Date: 08/14/1985
• Status: Expired due to Term

• Current Assignee: Raytheon Company (Rtx Corporation)
• Original Assignee: Hughes Aircraft Company (Rtx Corporation)
• Inventors: Ferrer, John J.
• Primary Examiner(s): Corbin, John K.
• Assistant Examiner(s): Lemmo, Vincent J.
• Application Number:
  US06/765,895
• Time in Patent Office: 636 Days
• Field of Search: 350/174, 350/601, 350/632, 350/3.7, 350/3.71, 350/3.72
• US Class Current: 359/15
• CPC Class Codes: B64D 43/00 Arrangements or adaptations of instruments arrangements of cameras B64D47/08; aeronautical measuring instruments per se G01C
• CPC Class Codes: G02B 2027/0156 with optionally usable elements
• CPC Class Codes: G02B 27/0149 characterised by mechanical features G02B27/0176 takes precedence

Abstract

A mounting and stowage mechanism erects a head-up display combiner into the pilot'"'"'s line-of-sight. One end of a crank is mounted on the combiner and is pivoted on a first link which is pivoted to a frame. A support link is pivoted on the combiner and on a drag link which is pivoted to the frame. A connecting link is pivoted to both the first link and the outer pivot of the drag link to complete a compound 4-bar linkage which controls the path of the combiner between the erected position and a stowed position out of the pilot'"'"'s line-of-sight. Manual control is through a handle which is mounted on a slider for linear motion and is connected to the end of the crank remote from the combiner. The mechanism is rendered insensitive to motion in the combiner-erect position by assuring that the instant centers of the links carrying the combiner are located at twice the focal length from the combiner along a line that runs through the center of curvature of the combiner and its focal point. The mechanism thus reduces optical errors caused by play or vibration in the mechanism.

Claims

1. A combiner mounting and storage mechanism comprising:

a frame for fixing with respect to the airframe of an aircraft;

first and second links each respectively pivoted on a first pivot on said frame for pivotal movement with respect to said frame;

mounting means for carrying a combiner;

a support lever secured to said mounting means and pivotally mounted on a second pivot on said first link; and

a support link pivotally connected to said mounting means and pivotally connected to said second link, said mechanism being constructed and arranged to move said combiner from a stowed position to an active position, the combiner for mounting in said mounting means having a curvature about a center of curvature which defines a central radius, said pivots of said first link and said pivots of said support link being substantially in line with a point about twice the focal length of the combiner along its radius of curvature when said combiner is in the active position.

2. The mechanism of claim 1 wherein a connecting link is pivotally connected to the pivotal connection between said second and support links and is pivotally connected to said first link intermediate said pivots thereon so as to form a fully constrained linkage mechanism.

3. The mechanism of claim 2 further including a stop positioned to engage between said support lever and said connecting link when said combiner is in the errect position to load said mechanism and inhibit vibration thereof.

4. The mechanism of claim 3 wherein a stop in said mechanism engages between said connecting link and said support link when said combiner is in the stowed position so that said mechanism is loaded in the stowed position to minimize vibration.

5. The mechanism of claim 2 wherein a stop in said mechanism engages between said connecting link and said support link when said combiner is in the stowed position so that said mechanism is loaded in the stowed position to minimize vibration.

6. A combiner mounting and storage mechanism comprising:

a frame for fixing with respect to the airframe of an aircraft;

first and second links each respectively pivoted on a first pivot on said frame for pivotal movement with respect to said frame;

mounting means for carrying a combiner;

a support lever secured to said mounting means and pivotally mounted on a second pivot on said first link; and

a support link pivotally connected to mounting means and pivotally connected to said second link, said mechanism being constructed and arranged to move said combiner from a stowed position to an active position, the combiner having a curvature which defines a central radius, a point along the radius of curvature at about twice the focal length of the combiner and an intersection line being defined through said point at about right angles to the radius, said pivots of said first link and said pivots of said support link defining lines which intersect substantially on said intersection line when said combiner is in the active position.

7. The mechanism of claim 6 wherein a holographic optical element combiner is mounted in said mounting means.

8. The mechanism of claim 6 wherein a connecting link is pivotably connected to the pivotal connection between said second and support links and is pivotally connected to said first link intermediate said pivots thereon so as to form a fully constrained linkage mechanism.

9. The mechanism of claim 8 further including a stop positioned to engage between said support lever and said connecting link when said combiner means is in the erect position to load said mechanism and inhibit vibration thereof.

10. The mechanism of claim 9 wherein a stop in said mechanism engages between said connecting link and said support link when said combiner is in the stowed position so that said mechanism is loaded in the stowed position to minimize vibration.

11. The mechanism of claim 8 wherein a stop in said mechanism engages between said connecting link and said support link when said combiner is in the stowed position so that said mechanism is loaded in the stowed position to minimize vibration.

12. A combiner mounting and storage mechanism comprising:

a frame for fixing with respect to the airframe of an aircraft;

first and second links each respectively pivoted on a first pivot on said frame for pivotal movement with respect to said frame;

mounting means for carrying a combiner;

a support lever secured to said mounting means and pivotally mounted on a second pivot on said first link; and

a support link pivotally connected to said mounting means and pivotally connected to said second link, said mechanism being constructed and arranged to move said combiner from a stowed position to an active position, said links and support lever being constructed and arranged to constrain the combiner to motion related to its arc of curvature when in the active position.

13. A mounting and stowage mechanism for a combiner optical element comprising:

mounting means for the combiner optical element;

a support lever connected to said mounting means;

a frame;

a first link pivotally connected to said frame at a first pivot point, said support lever being pivotally connected to said first link at a second pivot point of said first link;

a support link having first and second pivot points by which it is respectively pivotally connected to said mounting means and to a second pivot so that said mounting means moves from a position where it is in an active position to a stowed position, a point being defined at a distance approximately equal to twice of the focal length of the combiner along its radius of curvature, a line through said pivot points of said support link being directed substantially at said point when said mounting means is in the active position and a line through said pivot points of said first link passing substantially through said point when said mounting means is in the active position so that motion of said first link and said support link close to the active position do not change movement of said point.

14. The mechanism of claim 13 wherein there is a second link pivotably connected to said frame at a first pivot point thereon, said second link being pivotally connected to said support link at a second pivot thereof.

15. The mechanism of claim 14 wherein there is a connecting link pivotably connected to said second pivot of said support link and pivotally connected to a third pivot point on said first link intermediate said first and second pivot points thereof.

16. The mechanism of claim 15 wherein there is a stop between said lever and said connecting link positioned so that said stop engages when said mounting means is in the erected position in order to load said pivots pins to reduce vibration freedom of said mechanism.

17. The mechanism of claim 16 wherein there is a stop between said support link and said connecting link which engages when said mechanism is in the stowage position so that when said stop is engaged, said pivots are loaded to reduce vibration freedom of said mechanism.

18. The mechanism of claim 15 wherein there is a stop between said support link and said connecting link which engages when said mechanism is in the stowage position so that when said stop is engaged, said pivots are loaded to reduce vibration freedom of said mechanism.

19. The mechanism of claim 15 wherein there is a manually operable handle connected to said lever so that said mechanism can be moved between its stowage position and its erect position.

20. The mechanism of claim 19 wherein there is a linear guideway mounted on said frame and a slide is movable within said linear guideway and said handle is mounted on said slide, and further including a control link pivotally connected between said slide and said support lever so that motion of said handle along its linear guideway controls the motion of said mounting means.

21. The mechanism of claim 20 wherein said control link is positioned so that it moves to retain said mechanism in the erect position.

22. The mechanism of claim 21 further including a stop between said slide and its linear guideway to releaseably retain said slide in its guideway in the stowage position to retain said support link against its stop on said connecting link to retain said mechanism in the stowage position.

23. The mechanism of claim 20 further including a stop between said slide and its linear guideway to releaseably retain said slide in its guideway in the stowage position to retain said support link against its stop on said connecting link to retain said mechanism in the stowage position.