Aircraft engine management system

Details Aircraft engine management system Aircraft engine management system

1992-12-08

1994-09-06

Black, Thomas G.

Boots, shoes, and leggings

364442, 36443101, 60 39281, 60 3927, 60243, G06F 1548, G06G 770

Patent

active

053453867

ABSTRACT:
An aircraft jet engine management system has a digital electronic control unit (DECU) which measures turbine blade temperature (TBT) and controls the engine in such a way as not normally to exceed a TBT normal datum, there being an over-ride facility which responds to special circumstances as represented by one or more pilot-independent inputs to the DECU to allow temporary over-ride of the TBT limitation program, at least cut-off of the over-ride being pilot-independent.

REFERENCES:
patent: 4429528 (1984-02-01), Matthews et al.
patent: 4459671 (1984-07-01), Teass et al.
patent: 4697238 (1987-09-01), Barbeau
patent: 5023797 (1991-06-01), Lappos et al.
patent: 5076048 (1991-12-01), Boston
patent: 5083277 (1992-01-01), Shutler

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