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Engine can be
fabricated in
your own
workshop
using sheet
metal and
tubing
Click to hear
engine run (193 kb).
Order Online
- or -
by Phone, Fax, or Mail
Plans available in 20-lb, 40-lb,
80-lb, and
130-lb thrust sizes
Plans Include...
Standard Plans...
4 - (or more) 24 x
36 inch drawings
on bond with full-
size patterns
for
the engine thrust
size of your choice
(sheet-count varies
according to
engine thrust)
1 - Technical and
assembly manual
Deluxe Plans...
4 - Complete sets
of construction
drawings
on bond;
one for each thrust
size engine (19
sheets total)
1 - Technical and
assembly manual
1 - CD-ROM with
technical and
assembly manual,
2D CAD files in dxf
and AutoCAD dwg
formats, 3D
models for all
engine sizes, plus
video clips. 3D
files can be
exported
to iges,
Pro-E, SolidWorks,
and other
common formats
using the program
on the CD.
Detailed
Description of the Gluhareff Plans Packages Prices...
Standard...$75
Deluxe...$150


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Gluhareff Pressure Jet Engine
A Jet You Can Build From Plans

Mpeg Video is 1.2 MB |
The dream of personal flight
goes back to Icarus, the mythical character who made wings of wax and feathers, then
soared too close to the sun. Today the vision is lived out in modern form with machines
such as flying platforms, rocket propulsion backpacks, and fixed-wing ultralight aircraft.
But the idea of a VTOL machine - a personal helicopter - holds a special fascination for
those of us who are smitten.
When Eugene M. Gluhareff
examined the technical challenges of personal flight from his
perspective as a helicopter design engineer, it quickly became obvious
that the absence of a suitable blade-tip powerplant was the missing
ingredient. So he designed his own powerplant specifically for this type
of application. Today's pressure jet engine is the result of some 30
years of refinement. And you can build the engine yourself following the
step-by-step instructions in our comprehensive plans package.
The Gluhareff Pressure Jet engine is a remarkably simple device made of thin-wall
stainless steel tubing and sheet metal. Inside, it contains only a length of coiled steel
tubing (the fuel line), which gasifies and super-heats the incoming liquid propane before
it is injected at supersonic speed at the top of the intake stack. The engine has no
moving parts, yet it is fully throttleable. Thrust is controlled by opening or closing a
valve in the propane supply line. To start the engine, simply open the fuel valve then
press a button to send current to a small spark plug mounted at the rear of the combustion
chamber. After a 10-15 second warm-up to stabilize the flame front, the engine is ready
for full-throttle operation. To stop the engine, simply turn off the fuel supply.
One of the most remarkable aspects of the engine is that it works at all. Prior to Mr.
Gluhareff's design, engineers had understood that it was possible to produce thrust by
using the energy of pressurized propane to induce the fuel/air mixture. Calculations,
however, indicated a maximum thrust of only about 3 to 5 pounds, and extremely high
specific fuel consumption (fuel consumed per unit of power output). The secret to the
success of the Gluhareff Pressure Jet is its sonically tuned intake stack, which results
in far greater thrust and far lower specific fuel consumption.
Three intake stages are sized according to the length of the sound waves produced when
the engine is running. The sound waves acting against the intake stack translate into a
pumping action that pressurizes the incoming fuel/air mixture. This pressurizing action is
similar in effect to that of the turbine in a turbojet engine. If the intakes are not in
tune, the small 20-lb thrust engine, for example, produces only about 3-5 pounds of
thrust. The fish-mouth cut at the rear of the tailpipe also has sonic effects.
It reduces noise and increases thrust.
Building the jet requires some sheet metal forming, but much of it can be assembled from
stock materials. For example, the exhaust pipe, combustion chamber, and fuel lines are cut
from thin-wall stainless steel tubing. The intake stages, the diffuser skirt that
blends the final intake stage into the combustion chamber, and the transition piece
between the combustion chamber and the exhaust pipe are hand formed. You can spin the nose
cone on an ordinary home workshop woodworking lathe, or purchase it ready-made from the
source listed in the plans. By doing the fabricating and welding yourself, total building
costs can be held to little more than the cost of the sheet metal, tubing, and fittings.
Specifications
Engine |
G8-2-20 |
G8-2-40 |
G8-2-80 |
G8-2-130 |
Length
(inches/mm) |
36/914.4 |
38.5/978 |
45/1143 |
48/1219 |
Intake to CL
Burner
(inches/mm) |
25.5/647.7 |
27.5/698.5 |
36/914.4 |
37/939.8 |
Weight
(lbs/kg) |
5.5/2.5 |
11/5 |
21/9.53 |
24.5/11.12 |
SFC Static
(lbs fuel per lb thrust per hour) |
4.8 |
4.6 |
4.2 |
*1.33/0.77 |
SFC Dynamic**
(lbs fuel per lb thrust per hour) |
1.67 |
N/A |
N/A |
N/A |
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*Oval intake/round intake
**With ram air intake, SFC declines with increased speed. SFC at 293 ft/sec (89.4 m/sec)
is approximately 1/3 of static value. |
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About the Inventor Eugene M. Gluhareff was a graduate Aeronautical Engineer from the Rensselaer
Polytechnic Institute in Troy, New York. He was a key figure in the history of the
helicopter almost from its inception, working directly under Igor I. Sikorsky and
side-by-side with Igor A. Sikorsky, Chief of Aeronautics at Sikorsky Aircraft Corp.
In addition to producing many conventional helicopter designs, he also pioneered the
single-bladed rotor system, and invented the Kerosene Fueled Valveless Pulse Jet engine,
which was used to power the world's first single-bladed one-man helicopter (of his
design). Later he developed a Delta-Wing Convertiplane for the USAF, which utilized a
foldable single-blade rotor with a blade-tip cold-jet power system. He was Project
Engineer on the Top Sergeant pulse-jet powered helicopter, and developed the XH-26 one-man
tip jet powered helicopter for the USAF.
In the early 1960's, Mr. Gluhareff developed rotary wing drones for the U.S. Navy. After
joining Douglas Aircraft Co. in 1963, he worked as Design Engineer Scientist on the Saturn
Rocket and was in charge of the sequence of events from firing to parking orbit on
subsequent launchings. Following the Saturn program, he became Specialist in the design of
Rocket Stabilization Systems for ejection seats and space capsules.
In 1972, he established EMG Engineering in Gardena, California, where he continued the
development of the propane-fueled pressure jet engine featured here. Building this
remarkable jet engine is a fulfilling and inexpensive way of owning an important piece of
aviation history.
About the Plans
Our plan-set is based on Mr. Gluhareff's original drawings, technical documents,
hand-written construction notes, and photographs. Theoretical information in the
manual was taken from the Technical Handbook provided by Mr. Gluhareff with the GTS-15
Teaching Stand, which was used by universities to teach the principles of jet engine
operation. The step-by-step construction procedures in the technical manual were
derived from Mr. Gluhareff's professional notes and drawings on the various procedures
used to hand-build engines in his workshop. Photographs in the manual showing
the engine at various stages of construction were scanned from original photos taken in
Mr. Gluhareff's workshop for internal documentation purposes. Until now, these
construction procedures and photographs have never been published.
Although the textual material has been slightly edited and the original illustrations
have been recreated on computer, great care was taken to insure that the new material is
an accurate replication of the original work. This plan-set is the only authorized
and updated work available of Mr. Gluhareff's original material. Click
for a detailed description of the plan-set.
EMG-300 Helicopter

The EMG-300 helicopter was the last project developed by Mr. Gluhareff.
This helicopter was specifically designed around the G8-2 jet, and was first
test-piloted by Eugene M. Gluhareff. Click on the image for details.
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