Patent ID: 7825830
Filing Date: 2010-11-02
Classification: B64D,G01D

Abstract:
1. An aircraft attitude indicator device comprising: a portable housing; a plurality of attitude sensors within said housing and said attitude sensors being structured and disposed to sense attitude of an aircraft including a level attitude, a nose up attitude, a nose down attitude, a right bank attitude, and a left bank attitude; at least one audible alarm contained within said housing, and said audible alarm being activated when at least one of said plurality of attitude sensors senses a dangerous attitude; a front display panel on said housing; a plurality of linear arrangements of light emitting indicators on said front display panel for providing a visual indication of the aircraft attitude sensed by said plurality of attitude sensors, each of said plurality of linear arrangements of light emitting indicators having at least four light emitting indicators, and said plurality of linear arrangements of light emitting indicators including: a first pair of spaced apart light emitting indicators of distinct color for indicating a nose up attitude; a second pair of spaced apart light emitting indicators of distinct color for indicating a nose down attitude; and said plurality of attitude sensors, said at least one audible alarm, said plurality of light emitting indicators, said first pair of spaced apart light emitting indicators and said second pair of spaced apart light emitting indicators being energized by a power source.