Accession Number:

ADA169483

Title:

Component Improvement Program Task 83-01, 36E133 Air Turbine Starter,

Descriptive Note:

Corporate Author:

ALLIED BENDIX AEROSPACE UTICA NY FLUID POWER DIV

Personal Author(s):

• Williams,L.

Report Date:

1986-02-01

Pagination or Media Count:

36.0

Abstract:

The objective of this task was to replace the mechanical cutout switch with a solid-state electronic cutout switch to improve accuracy and reliability of the automatic start cycle termination in the S-3A and F-14A aircraft. The function of the cutout switch is to terminate the start cycle at a predetermined speed. It was determined that the existing electronic circuit can be used for the 36E133123 with only a minor resistor change to accommodate the subject units cutout speed. Breadboard testing was successfully completed and satisfactorily demonstrated feasibility.

Descriptors:

• *ELECTRONIC SWITCHES
• TEST METHODS
• ACCURACY
• RELIABILITY
• NAVAL AIRCRAFT
• BREADBOARD MODELS
• RESISTORS
• ENGINE STARTERS
• TURBINE COMPONENTS

Subject Categories:

• Jet and Gas Turbine Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE