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Method and apparatus to align auxiliary aircraft equipment attitude and heading

a technology for auxiliary aircraft and mounting methods, applied in the direction of electrical apparatus casings/cabinets/drawers, process and machine control, etc., can solve the problems of prone to damage of components of these tools, gps devices which are expensive, and require repetitive periodic tool certification and calibration

Inactive Publication Date: 2005-06-09
THE BOEING CO
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  • Application Information

AI Technical Summary

Problems solved by technology

Traditional methods of measuring the attitude and heading require expensive external tooling and typically require positioning of the aircraft with respect to an absolute reference.
Such external tooling incorporates pitch and roll sensors, laser reflection systems or position receivers such as GPS devices which are expensive and require repetitive periodic tool certification and calibration.
Further, the tools must often be aircraft model specific requiring extensive duplication and inventorying of tools.
The components of these tools are often prone to damage due to their complexity.

Method used

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  • Method and apparatus to align auxiliary aircraft equipment attitude and heading
  • Method and apparatus to align auxiliary aircraft equipment attitude and heading
  • Method and apparatus to align auxiliary aircraft equipment attitude and heading

Examples

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Embodiment Construction

[0013] Most current commercial aircraft rely on an inertial reference system or unit for precise determination of aircraft attitude and heading. The inertial reference unit (IRU) is typically a line replaceable unit (LRU) that is designed for easy installation and removal. Use of the IRU as an aircraft specific tool for alignment of auxiliary equipment to be mounted to the aircraft eliminates the need for additional dedicated and complex tooling for that task.

[0014] For alignment of an auxiliary equipment element such as an antenna, a simple, compact mechanical interface assembly is provided which mates with the attachment brackets for the auxiliary equipment. The interface assembly acts as a precision locating tool for the mounting bracket and a remote platform for mounting of the IRU. An extension cable assembly is provided to connect the IRU to its avionics tray in the aircraft when mounted in the interface assembly. The IRU, in its normal mounting in the aircraft avionics tray,...

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PUM

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Abstract

Precision alignment of auxiliary equipment on an aircraft is accomplished by a locating tool for the aircraft inertial reference unit (IRU) attached to the auxiliary equipment mount. Aircraft attitude and heading are obtained using the IRU. The IRU is removed from its avionics tray in the aircraft and installed on the locating tool. The locating tool is connected for remote operation of the IRU and the IRU is operated to obtain attitude and heading. This attitude and heading is then compared to the IRU reading for the attitude and heading of the aircraft.

Description

BACKGROUND OF THE INVENTION [0001] 1. Field of the Invention [0002] This invention relates generally to the field of precision mounting of aircraft auxiliary equipment and, more particularly, to a system employing an aircraft inertial reference unit (IRU) with a remote IRU interface on precision locating tooling for alignment of the auxiliary equipment using the mounting brackets. [0003] 2. Description of the Related Art [0004] Auxiliary equipment such as antennas and receiving equipment for various avionics and other subsystems is regularly attached to aircraft during assembly or as a retrofit. Many such systems require precise calibration with respect to overall aircraft heading and attitude for proper operation in the aircraft. Traditional methods of measuring the attitude and heading require expensive external tooling and typically require positioning of the aircraft with respect to an absolute reference. Such external tooling incorporates pitch and roll sensors, laser reflectio...

Claims

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Application Information

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Patent Type & Authority Applications(United States)
IPC IPC(8): B64D45/00G06F7/00H05K7/14
CPCH05K7/1412
Inventor HUYNH, DAN NHANROTH, GARY MICHAELCAWLEY, JOHN EDWARD
Owner THE BOEING CO
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