Adaptable hud mount

• US 6,072,444 A
• Filed: 06/15/1998
• Issued: 06/06/2000
• Est. Priority Date: 02/02/1998
• Status: Expired due to Fees

• Current Assignee: United States Air Force (Government of the United States of America)
• Original Assignee: United States Of America As Represented By The Secretary Of The Air Force
• Inventors: Burns, Fletcher A.
• Primary Examiner(s): Powell, Mark R.
• Assistant Examiner(s): YANG, RYAN R
• Application Number:
  US09/100,781
• Time in Patent Office: 722 Days
• Field of Search: 345/7, 345/8, 345/9, 359/630, 359/632, 340/980, 353/79, 353/13, 353/14
• US Class Current: 345/7
• CPC Class Codes: G02B 27/0149 characterised by mechanical features G02B27/0176 takes precedence

Abstract

A head up display (HUD) mounting assembly (MA) enables the secure, yet flexible mounting of major HUD components within vehicles and particularly within the cockpit of an aircraft. Flexibility is desirable because of slight movement of airframe members during maneuvers and changing temperature and air pressure conditions, yet stability must be maintained in order to preserve optical alignment between the HUD projector and image combiner components. The inventive MA provides an integrated support for the HUD projector and image combiner thus improving optical stability over discretely mounted systems. The MA has a relatively rigid support arm attached to two end brackets, where one is a spring bracket and the other is an anti-twist bracket. The brackets are mounted to the ceiling of an aircraft cockpit to support the arm and to resiliently hold the HUD components in optical alignment.

Claims

1. A mounting assembly (MA) for mounting head-up display (HUD) components in the cabin or cockpit of a vehicle comprising,

a) an arm for supporting a HUD projector and image combiner in optical alignment,

b) at least two mounting means for connecting said arm to said vehicle at spaced-apart points on said arm wherein at least one of said mounting means resiliently connects said arm to said vehicle.

2. The MA of claim 1 wherein one of said mounting means resiliently connects said arm to said vehicle while another mounting means pivotably connects said arm to said vehicle, which latter mounting means is able to twist or turn relative to said arm.

3. The arm of claim 2 wherein said vehicle is an airframe and said MA is mounted in the cockpit thereof.

4. The MA of claim 3 wherein the mounting means that can twist or turn, is a spherical bearing which connects one end of said arm to said airframe.

5. The MA for claim 3 wherein said spherical bearing has a forked member of two tines which receive therebetween a tongue member having a spherical bearing therein which engages the sides of said two tines so as to permit roll, pitch, yaw, twisting and turning between tongue and forked member.

6. The MA of claim 3 wherein the flexible mounting means is a bent spring member which connects one end of said arm to said airframe for resilient support therebetween.

7. The MA of claim 2 wherein said support arm runs fore and aft in a cabin or cockpit of a vehicle, the forward end of said arm being connected to a vehicle surface by an anti-twist mounting means and the aft end of said arm being connected to a vehicle surface by a resilient mounting means.

8. The MA of claim 1 wherein said support arm is adapted to hold an aft mounted projector and a forward mounted image combiner in desired relative positions and alignment.

9. The MA of claim 1 wherein said support arm has a bend between mounting points of said MA to said vehicle, to more closely conform with the contour of the latter.