# US 7,411,194 B1 · Aviation vision apparatus

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- Number: US 7,411,194 B1
- Document ID: US7411194B1
- Status: Granted
- Kind: B1
- Application number: 11/594,028
- Filed: 2006-11-08
- Published: 2008-07-24
- Granted: 2008-08-12
- Earliest claimed: 2005-11-09
- Assignees: Kollsman, Inc.
- Inventors: Jonathan Everett; John A. Gagnon; Athanasios Pashos; Roberto Rodriguez; Richard Wolfe
- Web page: https://patentgrep.com/patent/US7411194B1

## CPC

- B60R 11/04: Mounting of cameras operative during drive; Arrangement of controls thereof relative to the vehicle
- H04N 23/20: for generating image signals from infrared radiation only
- H04N 25/674: based on the scene itself, e.g. defocusing
- B60R: VEHICLES, VEHICLE FITTINGS, OR VEHICLE PARTS, NOT OTHERWISE PROVIDED FOR
- H04N: PICTORIAL COMMUNICATION, e.g. TELEVISION

## Abstract

An aviation vision apparatus. Its purpose assists a pilot's ability to fly an aircraft by providing increased visibility. The apparatus features an uncooled IR sensor for vision enhancement. An integrated window assembly is provided which permits the sensor to obtain its imagery. The apparatus also has an integrated aerodynamic enclosure. The apparatus features electronics responsible for window assembly window control functions and IR sensor control. The apparatus is a single line replaceable unit that receives control commands from the aircraft's head-down display or other control modules. The unit also provides for the video display.

## Claims

### Claim 1

An aviation vision apparatus to enhance a pilot's ability to fly an aircraft, said
apparatus comprising:
an uncooled IR sensor having a focal plane array;
an integrated window assembly associated with said sensor, said integrated window assembly including a selectively activated non-uniform correction (NUC) flag providing defocused radiant reference energy for correction of a response from an imaged scene of the focal plane array of the sensor;
wherein said sensor and said integrated window assembly are placed within an integrated fairing enclosure.

### Claim 2 (depends on 1)

The apparatus of claim 1 further comprising:
a heater control system for command and control of said IR sensor.

### Claim 3 (depends on 2)

The apparatus of claim 2 wherein the focal plane array is based on microbolometers.

### Claim 4 (depends on 3)

The vision apparatus of claim 3 wherein said apparatus is mounted to an aircraft using only a mounting plate.

### Claim 5 (depends on 4)

The vision apparatus of claim 4 wherein said mounting plate can be boresighted.

### Claim 6 (depends on 1)

The aviation vision apparatus of claim 1 wherein said fairing enclosure is aerodynamically shaped.

### Claim 7 (depends on 1)

The aviation vision apparatus of claim 1 wherein the non-uniform correction flag comprises an infrared Fresnel lens.

### Claim 8 (depends on 1)

The aviation vision apparatus of claim 1 wherein correction of the focal plane array response of the sensor from an imaged scene is not from an opaque-non-uniformity correction flag.

### Claim 9 (depends on 1)

The aviation vision apparatus of claim 1 wherein the correction flag presents to the sensor an out-of-focus image of a current scene during non-uniformity correction (NUC).

### Claim 10 (depends on 9)

The aviation vision apparatus of claim 9 wherein the NUC radiance scene has the average radiance of the scene to be imaged thereby minimizing differences between the NUC temperature and the NUC scene radiance at each array pixel whereby residual non-uniformity correction errors are reduced.