space telescope major configuration elements baffles OTA equipment NASA wow seti line 18a3 the idea girl says youtube
Anti detonation device and method for internal combustion engines us patent no 7066137 nasa wow seti line 18a3 the idea girl says youtube
H&K 416 short-stroke gas piston nasa wow seti line 18a3 the idea girl says youtube
ISS, ARMS CREW STS-131 Astronauts in space NASA wow seti line 18a3 the idea girl says youtube
Line 18a3 Baffle Invention Condenser Tubes NASA ARMS Reactor Vessel US Patents Wow SETI
part 104 of 100 videos there are more videos after this one i’ll post all then update the #.
Math Equation Wow Seti 1977 radio signal alien
14/
3/4/4/1/1/1/1/11=0.017
14/0.017=823.5294
Google 823.5294
Feb 2 2012 935 pm est
My Thoughts for Line 18 a3
I don’t if you’ve noticed but many of the “places” in regards to NASA or testing facilities
All started doing tests around 1966 or up to 1977.
The Wow SETI signal was received August 15, 1977. Within a 10 year time frame is what we have in this
Section. Some of the facilities have closed down but the test results are still being debated or worked over in the hopes of making something from them in 2012.
In this section two patents came up for new devices
Anti detonation device and method for internal combustion engines
United States Patent 7066137
Fluid flow distribution system for fluidized bed reactor US Patent 4702891
My thoughts Continued: Feb 2 2012 946 pm est
So now that we have an idea of what we can use to convert solids to liquids or gases, compression with safety valves, we can use this data to create the fuel required for a UFO Engine…
Quote:
A fluidized bed reactor (FBR) is a type of reactor device that can be used to carry out a variety of multiphase chemical reactions.
Quote:
Fluidization (or fluidisation) is a process similar to liquefaction whereby a granular material is converted from a static solid-like state to a dynamic fluid-like state. This process occurs when a fluid (liquid or gas) is passed up through the granular material.
fluid flow distribution system for fluidized bed reactor patent no 47202891 nasa wow seti line 18a3 the idea girl says youtube
notes:
Line 18a3
Baffle: A device to prevent direct fluid flow or impingement on a surface.
Baffle
An obstruction used to slow down or divert the flow of gases, liquids, sound, etc. They are found in the fuel tank, crankcase, muffler, and radiator.
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PROTECTIVE DEVICE FOR CONDENSER TUBES – Ingersoll-Rand …
www.freepatentsonline.com/3568763.html
9 Mar 1971 – A protective device for the condenser tubes of a steam surface condenser. A baffle arrangement prevents direct impingement of high velocity against the … Cooling fluid, and apparatus for preventing direct impingement of high-velocity … tubes of the tube bundles causes by the flow of high-velocity steam.
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[PDF]
1 Classification of Heat Exchangers
media.wiley.com/product_data/excerpt/10/…/0471321710.pdf
File Format: PDF/Adobe Acrobat - View as HTML
A heat exchanger is a device that is used to transfer thermal energy … the fluids are separated by a heat transfer surface, and ideally they do not mix or leak. …. flow of two (or more)fluids is required in the exchanger, there is no direct …..classes, the range of tube sizes and pitches, baffling and support plates, pressure …
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Fluid flow distribution system for fluidized bed reactor – Patent …
www.patentgenius.com/patent/4702891.html
This invention pertains to a fluid flow distributor device and system for …. the inlet flow laterally to prevent direct inpingement of liquid on the lower surface of the … The top solid baffle plate prevents direct impingement of liquid on the bottom …
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nventor: Li, et al.
Date Issued: October 27, 1987
Application: 06/730,253
Filed: May 3, 1985
Inventors: Eccles; Richard M. (Princeton, NJ)
Li; Allen S. (Morristown, NJ)
Assignee: HRI, Inc. (Lawrenceville, NJ)
Primary Examiner: Richman; Barry S.
Assistant Examiner: Johnson; William R.
Attorney Or Agent: Wilson; Fred A.
U.S. Class: 422/140; 422/143; 422/145; 422/176; 422/220; 422/311
Field Of Search: 422/140; 422/143; 422/145; 422/176; 422/220; 422/311
International Class:
U.S Patent Documents: 2559876; 2608474; 2862798; 2996361; 3414386; 3523763; 3560167; 3698876; 4221653; 4359326
Foreign Patent Documents: 197809; 0036993
Other References:
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An improved flow distribution system for a catalytic reactor plenum chamber for a gas-liquid-solids ebullated bed reactor incudes a baffled nozzle device containing at least two baffle plates usually oriented substantially normal to the nozzle inlet flow direction for providing good mixing and uniform flow distribution of gas-liquid materials in the lower portion of the plenum, used in combination with distribution grid to effect a substantially uniform flow distribution of the gas/liquid mixture upwardly into the ebullated catalyst bed. A sparger can be provided in the plenum above the baffled flow distributor device for feeding additional gas-liquid mixture into the reactor. The flow distribution system provides a substantially uniform flow distribution of the gas-liquid mixture into the ebullated bed and thereby provides fouling-free operation of the reactor.
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DATA to Look At:
A baffle arrangement prevents direct impingement of high velocity
Cooling fluid, and apparatus for preventing direct impingement of high-velocity
tubes of the tube bundles causes by the flow of high-velocity steam.
Fluid flow distribution system for fluidized bed reactor – Patent …
Fluide flow distribution system for fluidized bed reactor
US Patent 4702891
H&K 416 short-stroke gas piston
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Quote:
Direct impingement is a type of gas operation for a firearm that directs gas from a fired cartridge directly to the bolt carrier or slide assembly to cycle the action.
Unlike conventional gas-operated firearms, direct impingement does away with a separate gas cylinder, piston, and operating rod assembly. High-pressure gas acts directly upon the bolt and carrier thereby saving weight, lowering costs, and reducing the mass of the operating parts.
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Anti detonation device and method for internal combustion engines
United States Patent 7066137
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Abstract:
A flame ejector device for mounting in the spark plug aperture of an internal combustion engine whereby an inner end of the device is within the combustion chamber, the device being configured to receive a fuel-air mixture charge on the compression stroke of the piston and wherein the charge is ignited by a conventional spark plug mounted on the device, a unique arrangement and orientation of flame ejector nozzles on the inner end of the device for ejecting flame fronts toward predetermined areas within the combustion chamber to maximize fuel burning, to avoid engine knocking, and to prevent direct impingement of flame on metal portions contiguous the chamber which are susceptible to burning or heat damage.
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Inventors:
Dawson, Ralph E. (277 Camby Dr., Kingsport, TN, US)
Application Number:
10/980486
Publication Date:
06/27/2006
Filing Date:
11/03/2004
Export Citation:
Click for automatic bibliography generation
Primary Class:
123/266
Other Classes:
123/268, 123/291
International Classes:
F02B19/00; F02B19/00
Field of Search:
123/268, 123/291, 123/267, 123/293, 123/286, 123/266
View Patent Images:
Download PDF 7066137 PDF help
US Patent References:
5105780 Ignition assisting device for internal combustion engines April, 1992 Richardson 123/263
5024193 Fuel combustion system, method, and nozzle member therefor June, 1991 Graze, Jr. 123/259
4987868 Spark plug having an encapsulated center firing electrode gap January, 1991 Richardson 123/260
4930473 Swirl chamber and spark plug assembly June, 1990 Dietrich 123/266
4332224 Internal combustion engine with a main combustion chamber and an ignition chamber June, 1982 Latsch et al. 123/254
4327681 Internal combustion engine having a main combustion chamber and an ignition device inserted into an ignition chamber May, 1982 Latsch et al. 123/260
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Photos of ISS, ARMS CREW STS-131 Astronauts in space
from NASA
Arms in space. Credit: NASA
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Astronauts share a lunch on the ISS. Credit NASA wow seti line 18a the idea girl says youtube
Astronauts share a lunch on the ISS. Credit: NASA
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ISS as seen from departing space shuttle Endeavour. Credit NASA TV wow seti line 18a the idea girl says youtube
ISS as seen from departing space shuttle Endeavour. Credit: NASA TV
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A beautiful view of the shuttle and ISS during the STS-131 mission. Credit NASA wow seti line 18a the idea girl says youtube
A beautiful view of the shuttle and ISS during the STS-131 mission. Credit: NASA
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Clay Anderson during an EVA. Credit NASA spacewalk ISS 131 wow seti line 18a the idea girl says youtube
Clay Anderson during an EVA. Credit: NASA
Pasted from <http://www.universetoday.com/63176/sts-131-the-mission-in-pictures/
quote
Clay works outside the ISS during STS-131′s first EVA.
During the six-hour, 27-minute spacewalk, Anderson and Rick Mastracchio (visible in the reflection of Anderson’s helmet visor), mission specialist, helped move a new 1,700-pound ammonia tank from space shuttle Discovery’s cargo bay to a temporary parking place on the station, retrieved an experiment from the Japanese Kibo Laboratory exposed facility and replaced a Rate Gyro Assembly on one of the truss segments.
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Discovery during the rendezvous and docking with the ISS 131 on April 7, 2010. Credit NASA wow seti line 18a3 the idea girl says youtube
Discovery during the rendezvous and docking with the ISS on April 7, 2010. Credit: NASA
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Clay Anderson with a ball of water. ISS 131 Credit NASA wow seti line 18a3 the idea girl says youtube
Clay Anderson with a ball of water. Credit: NASA
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The microgravity environment of space provides a great place to play — experimenting with a water is always fun and it likely happens every mission!
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The STS-131 crew in the ISS’s Cupola. Credit: NASA
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The STS-131 crew in the ISS's Cupola in outerspace Credit NASA wow seti line 18a3 the idea girl says youtube
Love this image of the STS-131 crew in the Cupola. Pictured counter-clockwise (from top left) are NASA astronauts Alan Poindexter, commander; James P. Dutton Jr., pilot; Dorothy Metcalf-Lindenburger, Rick Mastracchio, Japan Aerospace Exploration Agency (JAXA) astronaut Naoko Yamazaki, NASA astronauts Clayton Anderson and Stephanie Wilson.
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GOOGLE A Reactor Vessel NASA and ARMS comes up.
NASA - Aerobic Rotational Membrane System (ARMS)
www.nasa.gov/centers/kennedy/news/facts/ksc/ARMS2006.html
NASA - National Aeronautics and Space Administration. › Help and Preferences … An engineer prepares a reactor vessel for testing. Image at left: Dynamac …
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NASA - Beneficial Bacteria Up in ARMS
www.nasa.gov/missions/science/f_arms_prt.htm
5 May 2004 – Inside the clear plexiglass ARMS reactor vessel, 115 tubes, called membranes, deliver gaseous oxygen to a community of bacteria. But believe …
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GOOGLE Clear plexiglass ARMS Reactor Vessel and found this image
Below:
Bioprocess engineer Tony Rector monitors the Aerobic Rotational Membrane System (ARMS) KSC NASA Wow Seti line 18a3 the idea girl says youtube
Bioprocess engineer Tony Rector monitors the Aerobic Rotational Membrane System (ARMS) in the Resource Recovery lab at Kennedy Space Center. His hand rests at the top of the reactor vessel. Inside, a series of 115 rotating membranes stretches to the bottom. Credit: NASA/KSC
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The PBRF reactor vessel with all internals removed image credit NASA plum brook reactor facility wow seti line 18a3 the idea girl says youtube
The PBRF reactor vessel with all internals removed.
Image Credit: NASA, used with permission
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NASA Plum Brook Reactor Facility Decommissioning
Pasted from <http://www.dd.anl.gov/dd_web_photos/index.php?cid=16&pid=101
The NASA Plum Brook Reactor Facility (PBRF) in the late 1960’s credit nasa wow seti line 18a3 the idea girl says youtube
The NASA Plum Brook Reactor Facility (PBRF) in the late 1960’s.
Image Credit: NASA, used with permission
Pasted from <http://www.dd.anl.gov/dd_web_photos/index.php?cid=16&pid=98
GRC Plum Brook Station Spacecraft Propulsion Facility (B-2)
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The Spacecraft Propulsion Facility at Plum Brook Station (PBS) is the world’s only facility capable of testing full-scale upper-stage launch vehicles and rocket engines under simulated high-altitude conditions.
The PBS Space Power Facility (SPF) houses the world’s largest space environment vacuum chamber. PBS also has cryogenic test facilities and a hypersonic wind tunnel.[4]
In 2008 NASA agreed to pay $33.5 million to have its Plum Brook Reactor Facility decontaminated and decommissioned.[5]
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The Zero Gravity Research Facility is a vertical vacuum chamber used for microgravity experiments. It was designated a National Historic Landmark in 1985.
The facility uses vertical drop tests in a vacuum chamber to investigate the behavior of components, systems, liquids, gases, and combustion in such circumstances.
The facility consists of a concrete-lined shaft, 28 feet (8.5 m) in diameter, that extends 510 feet (160 m) below ground level.
An aluminum vacuum chamber, 20 feet (6.1 m) in diameter and 470 feet (140 m) high, is contained within the concrete shaft. The pressure in this vacuum chamber is reduced to 13.3 newtons per square meter (1.3×10−4atm) before use.
After the closing of the JAMIC facility in Japan, the NASA Zero-G facility is the largest microgravity facility in the world.
Spacecraft Propulsion Research Facility (B-2)
Rocket Engine Test Facility
This is a facility that was designated a National Historic Landmark, but de-designated later.
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Feb 2, 2012 930 pm est
TAGS for Line 18a3:
Resource Recovery lab at Kennedy Space Center NASA KSC
Plexiglass ARMS reactor vessel
Bacteria
The PBRF Reactor Vessel
The Spacecraft Propulsion Facility (SPF)
PBS Plum Brook Station
NASA Plum Brook Reactor Facility Decommissioning
Aerobic Rotational Membrane System (ARMS)
prevents direct impingement
High-velocity
Fluid flow distribution system
Fluidized bed reactor
Catalytic reactor plenum chamber
Gas-liquid-solids ebullated bed reactor
Baffle plates
Plenum
Distribution grid
Sparger
As cylinder
Pistorn
Operating rod assembly
H&K 416 short stroke gas piston
Internal combustions engines US Patent 7066137
Fluid flow distribution system for fluidized bed reactor US Patent 4702891
Flame ejector device
Spark plug aperture
Maximize fuel burning invention
The Zero Gravity Research Facility
microgravity environment
ISS Cupola
STS-131
NASA astronauts Alan Poindexter, commander; James P. Dutton Jr., pilot; Dorothy Metcalf-Lindenburger, Rick Mastracchio, Japan Aerospace Exploration Agency (JAXA) astronaut Naoko Yamazaki, NASA astronauts Clayton Anderson and Stephanie Wilson.
Feb 2 2012 935 pm est
My Thoughts for Line 18 a3
I don’t if you’ve noticed but many of the “places” in regards to NASA or testing facilities
All started doing tests around 1966 or up to 1977.
The Wow SETI signal was received August 15, 1977. Within a 10 year time frame is what we have in this
Section. Some of the facilities have closed down but the test results are still being debated or worked over in the hopes of making something from them in 2012.
In this section two patents came up for new devices
Anti detonation device and method for internal combustion engines
United States Patent 7066137
Fluid flow distribution system for fluidized bed reactor US Patent 4702891
Basic diagram of a fluidized bed reactor. solid gas distributor bubble particle NASA FBR wow seti line 18a3 the idea girl says youtube
Basic diagram of a fluidized bed reactor.
Pasted from
Quote:
A fluidized bed reactor (FBR) is a type of reactor device that can be used to carry out a variety of multiphase chemical reactions.
In this type of reactor, a fluid (gas or liquid) is passed through a granular solid material (usually a catalyst possibly shaped as tiny spheres) at high enough velocities to suspend the solid and cause it to behave as though it were a fluid.
This process, known as fluidization, imparts many important advantages to the FBR. As a result, the fluidized bed reactor is now used in many industrial applications.
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Quote:
Fluidization (or fluidisation) is a process similar to liquefaction whereby a granular material is converted from a static solid-like state to a dynamic fluid-like state. This process occurs when a fluid (liquid or gas) is passed up through the granular material.
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My thoughts Continued: Feb 2 2012 946 pm est
So now that we have an idea of what we can use to convert solids to liquids or gases, compression with safety valves, we can use this data to create the fuel required for a UFO Engine…
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