18. The Solution
We must interpose a third Air Mass Motion System No.3 between the ACTION (Air Mass Motion System No.1) and the REACTION (Air Mass Motion System No.2) halves, that is, between the Aircraft's TWO Air Mass Motion Systems and the Aircraft's structure formed by it's jet engine. This 3rd Air Mass Motion System must be interposed between the end of the ACTION half of its Motion System (Motion System No.1) and the start of its REACTION half (Motion System No.2) thereby interconnecting the end of the ACTION half of it's Motion System with the start of it's REACTION half.
This makes possible the establishment of a controllable Air Space around that part of the Aircraft's structure formed by it's jet engine/engines . This in it's turn makes possible the establishment of an infinitely variable gearing between the Motion Energy possessed by Air Mass Motion Systems No's 1& 2 as they jointly act and interact within this controlled Air Space upon the Aircraft's structure formed by it's jet engine.
This solution comprises of a SYSTEM called an, AIR VELOCITY GEARBOX wherein there is established a third AIR MASS MOTION SYSTEM (No.3) interposed between the ACTION (Air Mass Motion System No.1) & REACTION (Air Mass Motion System No.2) halves comprising the existing Aircraft's Motion System. The SYSTEM makes possible the establishment of the necessary separation between the ACTION and REACTION halves of the conventionally configured Aircraft's Air Mass Motion System transforming it in the process into a properly structured and sequenced Air Mass Motion System"Cycle". The resulting SYSTEM enables us thereby to establish direct computerised control over the differences between the interacting Air Velocities of the ACTION (Air Mass Motion System No.1) and REACTION (Air Mass Motion System No.2) as they jointly act and interact upon the Aircraft's structure relative to the RESULTANT Aircraft Velocity at, all demand conditions.
Remember, in terms of Motion Physics as this pertains to the Propulsive Efficiency of the Aircraft we are not concerned with how the propulsive power of the Aircraft is actually achieved comprising the thrust power invested in Air Mass Motion Systems No's 1 & 2. Here, we are only concerned with how efficiently and closely, the Air Mass MotionVelocity Energy of these combined Air Mass Motion Systems as they jointly act and interact upon the Aircraft's structure matches, the RESULTING Aircraft Velocity. In other words, the GEARING between the rate of the thrust force delivered to the Aircraft engine's mounting bolts relative to it's RESULTING Velocity at, all demand conditions.
|
