. The background section has a pretty straight-forward explanation how contrail-cirrus form and the potential impact on climate. This might be useful information to share with a chemtrail believer who argues that today's jets don't create persistent contrails. If so, then why is one of the largest manufacturers of aircraft engines filing for patent protection on engines that can reduce contrail formation? Of course, the committed CT-believer will probably argue back that "they" are doing this only to make it look like today's jets still make persistent contrails...External Quote:to manage the formation of contrails by aircraft engines in a manner that reduces negative impact on the climate
I saw that Rolls Royce has a recently published patent application for an Aircraft Vapour Trail Control System. The stated objective is. The background section has a pretty straight-forward explanation how contrail-cirrus form and the potential impact on climate. This might be useful information to share with a chemtrail believer who argues that today's jets don't create persistent contrails. If so, then why is one of the largest manufacturers of aircraft engines filing for patent protection on engines that can reduce contrail formation? Of course, the committed CT-believer will probably argue back that "they" are doing this only to make it look like today's jets still make persistent contrails...External Quote:to manage the formation of contrails by aircraft engines in a manner that reduces negative impact on the climate
Less efficient engines have those lines further to the left (cooler).
Typo? I thought that MORE efficient engines had cooler exhaust. One of us has it backward.
After scanning through that patent, I am impressed at how thoroughly Rolls Royce has studied contrail formation, persistence, and it's effect on climate during the day and night. Nightime use would be most beneficial due to decreasing contrail formation and thus allowing the land below to cool, assuming there are no cloud layers below. The one problem I see is that the process involves reducing the efficiency of the engine by aprox 10% for the time period that flight is within the contrail forming area. Airlines operate on very thin margins, and even buy/lease new airplanes to get the most efficient aircraft possible (like the B787), so, unless they are penalized for making contrails, they are not likely to want to install these devices, which would themselves likely be costly if an engine has to be retrofitted.It has a very good high-level explanation of the formation and dissipation of contrails.
The patent idea is that engine efficiancy could be modified so as to, effectively, lower the Contrail Critical Temperature for the engine, thus moving the environment conditions from the "Always contrails" to the "No contrails" region on the Appleman Chart. Think of the Appleman Chart curved lines being movable. Less efficient engines have those lines further to the left (cooler).
The engine controller (pilot) may go for more power to maintain trust, or possibly, the engine parameters may not allow that.
The patent discusses routing soulutions to reduce contrails, and this is then another option.
It doesn't seem like the person even bothered to read the patent, maybe just saw the title and jumped to conclusions:External Quote:
If I could. I'm not sure what to think about the whole chemtrail thing BUT.. I would like to ask my West why is there a patent 5,104,069 there. This is a patent by Boeing for a apparatus & method for ejecting materiel from an aircraft - a sprayer. This is NOT crop dusting. It's a sprayer. I do not see to many Boeing Aircraft spraying low over farms.
It's common for attorneys who write patent applications to describe an invention more broadly than the original intended purpose, in case the invention is later used for a different purpose. That way the patent may have more value. So here, the title of the patent makes it sound like the invention has a much broader purpose than what the inventors probably contemplated.External Quote:
BACKGROUND OF THE INVENTION
Commercial aircraft include various fluid drain masts which eject fluids, such as oil, waste gases and other liquids, from one or more exterior locations on the aircraft. For example, on some jet engines oil from the engine gearbox is allowed to drain out of a mast located at the bottom of the engine nacelle.
A problem associated with conventional fluid drain masts results when the ejected oil or corrosive liquid contacts a downstream portion of the aircraft leaving an unsightly stain on the aircraft...
SUMMARY OF THE INVENTION
The present invention pertains to a device for ejecting fluid from an aircraft. In the following detailed description the present invention will be described for application in evacuating oil from an aircraft engine nacelle. It should be appreciated, however, that the present invention may be used to evacuate other fluids and gases from an aircraft.
From a quick read, it's pretty clear that the purpose of the invention is to remove leaked oil from the engine:
Removing leaked oil, etc., from the engine is already done with drain masts. This patent is simply a modification of that in order to prevent unsightly stains.External Quote:The present invention pertains to apparatus for ejecting matter, such as gases and fluids, from an aircraft so as to prevent the matter from contacting a downstream portion of the aircraft.
The great invention seems to simply be angling the drain mast downwards a bit, so it shoots away from the plane.External Quote:A problem associated with conventional fluid drain masts results when the ejected oil or corrosive liquid contacts a downstream portion of the aircraft leaving an unsightly stain on the aircraft.
The great invention seems to simply be angling the drain mast downwards a bit, so it shoots away from the plane.
I haven't read the full description, but from the Abstract, it looks like a wind-up for the chemmies.Ken Caldeira has a patent for cloud formation and precipitation.
https://www.google.com/patents/WO2014082036A1?cl=en or https://www.google.com/patents/US9526216?cl=en
View attachment 26814
Good stuff for the chemtrail crowd![]()
Yes, that is correct.I don't think it's a wind-up. It sounds like cloud seeding by ionisation, which is the mechanism by which cosmic rays are thought to seed cloud formation, isn't it?
I saw that Rolls Royce has a recently published patent application for an Aircraft Vapour Trail Control System. The stated objective is. The background section has a pretty straight-forward explanation how contrail-cirrus form and the potential impact on climate. This might be useful information to share with a chemtrail believer who argues that today's jets don't create persistent contrails. If so, then why is one of the largest manufacturers of aircraft engines filing for patent protection on engines that can reduce contrail formation? Of course, the committed CT-believer will probably argue back that "they" are doing this only to make it look like today's jets still make persistent contrails...External Quote:to manage the formation of contrails by aircraft engines in a manner that reduces negative impact on the climate
External Quote:
BACKGROUND
Condensation trails (contrails) are visible trails of water vapor that are created from aircraft engine exhaust. Contrails are often visible as white cloudy streaks across the sky, indicating a path recently traveled by an aircraft. The visibility of contrails, including the duration of time in which contrails remain visible before dissipating, is dependent upon various atmospheric conditions surrounding the aircraft, including among others, air temperature, barometric pressure, and humidity.
Because aircraft contrails form directly behind an aircraft and may be visible from anywhere from seconds to hours, contrails create a visual reference that points directly to the aircraft that creates them. Anyone that sees a contrail only has to follow the contrail to the end to see the aircraft that is the source of the contrail. For commercial and private aviation, this phenomenon is not a problem. However, for aircraft that are designed to avoid detection, a contrail can be a significant problem.
"It may be worth adding how much a patent costs. A couple of hundred pounds in the UK. http://www.ipo.gov.uk/types/patent/p-applying/p-cost.htm"I added it after you mentioned it, thanks!
If you'd have read the page you cited:-
Americanscan'tread.co.uk
External Quote:
United States Patent Application 20180178920
Kind Code A1
SWANN; Peter ; et al. June 28, 2018
Aircraft Electrically-Assisted Propulsion Control System
Abstract
This invention concerns an aircraft propulsion system in which an engine has an engine core comprising a compressor, a combustor and a turbine driven by a flow of combustion products of the combustor. At least one propulsive fan generates a mass flow of air to propel the aircraft. An electrical energy store is provided on board the aircraft. At least one electric motor is arranged to drive the propulsive fan and the engine core compressor. A controller controls the at least one electric motor to mitigate the creation of a contrail caused by the engine combustion products by altering the ratio of the mass flow of air by the propulsive fan to the flow of combustion products of the combustor. The at least one electric motor is controlled so as to selectively drive both the propulsive fan and engine core compressor.
External Quote:
Aircraft Electrically-Assisted Propulsion Control System
Abstract
This invention concerns an aircraft propulsion system in which an engine has an engine core comprising a compressor, a combustor and a turbine driven by a flow of combustion products of the combustor. At least one propulsive fan generates a mass flow of air to propel the aircraft. An electrical energy store is provided on board the aircraft. At least one electric motor is arranged to drive the propulsive fan and the engine core compressor. A controller controls the at least one electric motor to mitigate the creation of a contrail caused by the engine combustion products by altering the ratio of the mass flow of air by the propulsive fan to the flow of combustion products of the combustor. The at least one electric motor is controlled so as to selectively drive both the propulsive fan and engine core compressor.