Auxiliary Power Systems for 1975 Fighter Aircraft

1968 ◽  
Author(s):  
B. H. Nicholls ◽  
A. D. Meshew
2001 ◽  
Author(s):  
Carole J. Read ◽  
Jan H. J. S. Thijssen ◽  
Eric J. Carlson

2019 ◽  
Vol 124 ◽  
pp. 01004
Author(s):  
R. V. Vyatkin ◽  
A. N. Tikhomirov ◽  
D. A. Kolesnichenko

The article describes the design and testing of an auxiliary power system for a light commercial electric vehicle. In paper described research about load modes of auxiliary power system for maintaining performance of electric vehicle under low-charge conditions. The article describes the design work and the installation of the necessary components for the research. The authors describe the experiment of charging the traction battery from an auxiliary power source. The results of the study are presented, including an assessment of the effectiveness of using auxiliary power systems.


2015 ◽  
Vol 119 ◽  
pp. 393-406 ◽  
Author(s):  
Hadi Ebrahimi ◽  
Javad R. Gatabi ◽  
Hassan El-Kishky

1996 ◽  
Vol 118 (2) ◽  
pp. 369-374
Author(s):  
J. P. Ehrhardt ◽  
S. K. Spring

The Sundstrand Power Systems T-62T-40-7 Gas Turbine Auxiliary Power Unit (APU) was adapted from an aircraft-borne APU to a marine application on the U.S. Navy’s Landing Craft Air Cushion (LCAC). Although the LCAC APU experienced less operating time than its aircraft version, the environmental conditions that exist cause unusual wear and component failures. Component and procedural improvements have been developed to extend the reliability of the T-62T-40-7 on board the LCAC.


1945 ◽  
Author(s):  
Karl Martinez ◽  
Sidney Schnitzer ◽  
Mitchell M. Berry ◽  
Dennis Decourcey

2010 ◽  
Vol 87 (5) ◽  
pp. 1670-1678 ◽  
Author(s):  
C. Strazza ◽  
A. Del Borghi ◽  
P. Costamagna ◽  
A. Traverso ◽  
M. Santin

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