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Patent

Propulsion system control

A Bland, +1 more
TLDR
In this paper, a propulsion and control system that includes gas generator means which discharges high energy gases into ducting is connected to at least two thrust units for converting the high-energy gases into propulsive thrusts.
Abstract
A propulsion and control system that includes gas generator means which discharges high energy gases into ducting which is connected to at least two thrust units for converting the high energy gases into propulsive thrusts. A separate pressure controller is associated with each thrust unit for restricting the flow of high energy gases to the thrust unit and thereby increasing back pressure in the ducting upstream from the pressure controllers and at the discharge end of the gas generator means. The two pressure controllers are operable independently of each other and the operation of either one increases the back pressure. Contemporaneously, with the increase in back pressure the gas generator means automatically discharges gases at an even higher energy level and as a result the thrust unit downstream from the pressure controller which is not operated delivers greater thrust, while the thrust unit downstream from the operated pressure controller delivers about the same amount of thrust.

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Citations
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References
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V/stol aircraft

TL;DR: In this article, a V/STOL aircraft comprises a fuselage having tandem wings which are offset lengthwise and vertically, and identical propulsion units are provided in each wing half.