Technical Design Report
For X-EP1 One Man Craft
By
Ted Walter Schulze
Table of Contents
Technical Design
Report----------------------------------------1
1. Craft Specifications and projected
performance------3
Performance--------------------------------------------------------3
The propulsion
system-------------------------------------------4
FIGURE
1------------------------------------------------------------5
Disclosure
Notice---------------------------------------------------6
Contact-----------------------------------------------------------------6
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1. Craft Specifications and projected
performance.
The craft is designed as a flying circular disk shaped
platform that has the
following approximate specifications.
Dimensions.
1. Outside
Diameter-------------------------------------------------------------------8 feet
2. Height from the ground to the top of the disk Approximately ------28.00
inches
3. Height from the top of the disk to the top of the pilot safety ring.--46.00
inches.
4. The pilot safety ring inside diameter is ------------------------------------28.5
inches.
5. Landing support ring diameter is---------------------------------------------71.5
inches
Weights.
1. The craft weight ready to fly without the pilot is
approximately----------150 Lb.
2. The rechargeable battery pack weight is about -------------------------------40
Lb.
3. Maximum total takeoff weight with a 200 lb pilot about --------------------400
Lb
Performance.
1. Maximum flight time with standard battery
pack---------------------------60 min.
2. Maximum time in hover
mode---------------------------------------------------75 min
3. Maximum forward speed
-----------------------------------------------------120
MPH
Flight
control.
1. The power thrust direction is always straight up so to change direction the pilot must shift
his weight in the direction of the desired direction of travel. The flat top of the disk will be tilted down in
forward flight causing the airflow over the top to push the craft down, so to maintain the same altitude the pilot
must simply apply more power to compensate, at the same time the forward speed will increase. This will allow the
craft to be able to stop and reverse direction very fast by the pilot simply leaning backward. I know that this is
counter intuitive to normal aerodynamic lift that is normally needed to save fuel.
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But because the electrical
propulsion system in this craft is so very efficient the need to conserve energy is not as great. I know that the
claim that I am making about the efficiency of the power supply is hard to believe, and you will want to know more,
but I can't disclose how that is accomplished at this time.
The propulsion
system.
-------------------------------------------------------------------------------------------------
Disclosure Notice.
All rights reserved. The information in this report may contain
information that could be patentable at a later date by Ted Walter Schulze. The reader is free to use copy
and distribute freely as long as the original content is not changed or altered in any way. An original copy
is kept on file for comparison.
Contact.
Author Ted Walter Schulze , Perry City Utah.
electronpropulsion@protonmail.com
PLEASE DONATE
You can be a part of this history making
discovery by
making a small donation, so we can continue with our
R&D experiments. Our goal is to build flying prototypes
and to have full disclosure to the public of how the
technology works for the benefit of all mankind !
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