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Patent 2731783 Summary

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Claims and Abstract availability

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(12) Patent Application: (11) CA 2731783
(54) English Title: THE FIRST PRACTICAL INTERSTELLAR PROPULSION ENGINE
(54) French Title: LE PREMIER SYSTEME DE PROPULSION INTERSTELLAIRE PRATIQUE
Status: Deemed Abandoned and Beyond the Period of Reinstatement - Pending Response to Notice of Disregarded Communication
Bibliographic Data
(51) International Patent Classification (IPC):
  • H02N 99/00 (2006.01)
  • B64G 1/40 (2006.01)
  • F03G 1/00 (2006.01)
  • F03H 99/00 (2009.01)
  • H02K 53/00 (2006.01)
  • H02N 11/00 (2006.01)
(72) Inventors :
  • NABIPOUR, HOSSEIN (Iran (Islamic Republic of))
(73) Owners :
  • HOSSEIN NABIPOUR
(71) Applicants :
  • HOSSEIN NABIPOUR (Iran (Islamic Republic of))
(74) Agent:
(74) Associate agent:
(45) Issued:
(22) Filed Date: 2011-02-22
(41) Open to Public Inspection: 2011-05-26
Examination requested: 2011-02-22
Availability of licence: N/A
Dedicated to the Public: N/A
(25) Language of filing: English

Patent Cooperation Treaty (PCT): No

(30) Application Priority Data: None

Abstracts

English Abstract


This novel engine is capable of steadily pushing a spacecraft through the
vacuum of space
without the need for any fuel burned or any high-velocity gases expelled to
propel the vehicle
forward. In each cycle, a moving ball comes to a stop and reverses its
direction of movement; this
cycle then repeats itself through impact collision, meaning the ball keeps
bouncing off the engine's
frame. In physics, this is called an elastic collision, whereby the ball
transfers its momentum to the
engine's frame and re-gains it by bouncing back. Akin to a "Newton's cradle",
a set of stationary
solid spheres/balls arranged symmetrically and held in place by wire ropes in
the shape of a semi-
circle (180 degrees) or a quarter-circle (90 degrees) act as the medium,
through which the
instantaneous energy of impact (impulse) of one dynamic ball is transferred to
the other. For this
closed cycle to continue to work indefinitely, two electromagnets are used to
add enough kinetic
energy to the dynamic balls in order to account for the energy losses in each
cycle. By creating a
perfectly elastic 'collision' between the dynamic ball and the engine's frame,
both the momentum
and kinetic energy of the ball are conserved. As a result, a net impulse
(force applied over a period
of time) is repeatedly added to the engine's frame and subsequently to the
spacecraft, causing it to
gradually gain momentum and accelerate.


Claims

Note: Claims are shown in the official language in which they were submitted.


Claims:
1- This engine with its basic mechanical components and its unique design and
configuration as illustrated in different views in figures A, B, C, and D is
the semi-circle
style capable of generating linear thrust and force. A quadrant style of the
same concept
(not shown in the drawings) would generate equal linear thrust and force in
two
perpendicular directions.
2- That such a novel design has never been patented or invented before
anywhere in the
world and is solely the result of my own observations and unrelenting
experiments.
3- That other than space/interstellar propulsion applications, this engine
could primarily be
used for power generation purposes on a larger scale in a green and
environmentally
friendly way.

Description

Note: Descriptions are shown in the official language in which they were submitted.


CA 02731783 2011-02-22
1
Application for patent in Canada
Feb. 22, 2011
Invention: The first practical interstellar propulsion engine
Inventor: Hossein Nabipour
Background:
Over the last decades, many attempts have been made to come up with a space
propulsion
system or engine, fully capable of traversing the vacuum of outer space
without burning and
expelling any gases. Inventions or ideas in this field are known as `reaction-
less drive' or `reaction-
less thrust' systems. According to the known laws of nature, no one object can
start to move from
rest and accelerate in one direction without pushing another object in the
opposite direction. As
Newton discovered, for every action force in one direction, there is an equal
reaction force in the
opposite direction. Therefore for a spacecraft (a mass) to accelerate forward
there has to be a second
external mass pushed backward, and that is how present space rockets and
shuttles propel
themselves by ejecting high-speed gases. Similarly, ships and submarines push
against the water,
cars push against the ground, airplanes push air backwards... all move forward
by pushing an
external mass backward. The law of conservation of momentum applies to such
interactions of
masses, whether on earth or out there in the vacuum of space, far away from
any gravitational
sources.
Physics of the collision phenomenon:
This engine is a practical application and utilization of a very basic yet
fundamental
phenomenon, in which two solid spheres/balls collide with each other in an
elastic manner, i.e. the
combined kinetic energies of the two objects and their combined momentum is
the same before and
after the collision. In an inelastic collision, however, only the momentum
part stays the same, but
the kinetic energy will not be the same, since some of it is dissipated or
lost during the impact. A
`Newton's cradle' shows exactly the elastic collision between the balls and
that how energy of
impact or impulse travels linearly through the balls and out from the other
end. This engine draws
upon such an amazing phenomenon and puts it into a useful and practical
application- generating
instantaneous linear force or thrust.

CA 02731783 2011-02-22
2
Description and specifications:
Figure A shows a 3-D view of the engine's concept. A rigid U-shape or L-shape
frame, a
few solid balls, two spiral springs, some wire ropes, and two electromagnets
comprise the main and
basic mechanical components of the engine. In this engine, the energy of
impact passes through a
set of balls, almost linearly, but in a circular pattern. As the number of
stationary balls/spheres
increases, the angle of each segment of the quadrant or a semi-circle
decreases. Having 45 or more
balls installed on the perimeter of a quadrant, the radial angle from centre
to centre of each ball
reduces to only 2 degrees or smaller. By doing so, a curve is divided up into
smaller linear
segments, and starts to show linear characteristics, thereby minimizing the
outward radial reaction
forces to almost zero. Once this is achieved, a ball moving in one direction
can be brought to rest by
colliding it against one side of the stationary balls, passing its energy
(impulse) through the
stationary balls, and finally transferring it to the ball on the other side,
causing almost no unwanted
radial reaction on the balls installed on the perimeter. Balls are arranged
and installed on the
perimeter of the quadrant or semi-circle to only have one degree of freedom,
i.e. in both X and Y
directions they are restrained by wire ropes, Z is the axis passing through
center to center of the
balls and tangent to the circle, along which the balls are free to move and
vibrate.
The semi-circle engine illustrated in Figures A, B, C, and D, does not show
the actual
number of stationary balls. In order for the engine to work and generate
thrust, at least 45-50
stationary balls are required to be assembled on a quadrant design, and 90-100
balls on a semi-circle
design. The quadrant or semi-circle styles are two different designs of the
same concept. There are
only two dynamic/colliding balls in either semi-circle or quadrant design, as
in a Newton's cradle
when only one ball is raised and released. The electromagnets are used to pull
or push the dynamic
balls at the exact moment they come to a stop and reverse direction. And the
chassis or frame acts as
the second mass, to which balls collide elastically and rebound, thereby no
energy is lost. A typical
wire rope attachment to the stationary balls is shown in Fig. A (note: all
stationary balls should have
the same restraints, however not shown in Fig. A). Wire ropes or similar
flexible light-weight
materials are used since there should be no significant masses attached to the
stationary balls as any
unwanted extra mass attached or connected to them would dissipate energy,
resulting in substantial
loss of energy and rendering the engine completely ineffective. As for the
material the balls are
made out of, the harder and the tougher, the better. Tungsten Carbide, for
instance, is approximately
3 times tougher and stiffer than stainless steel, making it a good choice of
material for the
manufacturing of the balls.

Representative Drawing
A single figure which represents the drawing illustrating the invention.
Administrative Status

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Please note that "Inactive:" events refers to events no longer in use in our new back-office solution.

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Event History

Description Date
Time Limit for Reversal Expired 2016-02-23
Application Not Reinstated by Deadline 2016-02-23
Revocation of Agent Requirements Determined Compliant 2015-06-04
Revocation of Agent Request 2015-05-25
Inactive: Office letter - MF 2015-04-14
Inactive: Office letter 2015-04-14
Letter Sent 2015-03-05
Reinstatement Request Received 2015-02-24
Inactive: Correspondence - MF 2015-02-24
Reinstatement Requirements Deemed Compliant for All Abandonment Reasons 2015-02-24
Maintenance Request Received 2015-02-24
Deemed Abandoned - Failure to Respond to Maintenance Fee Notice 2015-02-23
Reinstatement Request Received 2015-02-20
Inactive: Correspondence - MF 2015-02-20
Inactive: Adhoc Request Documented 2014-12-19
Inactive: Office letter 2014-10-30
Letter sent 2014-05-26
Inactive: Correspondence - MF 2014-05-20
Inactive: Office letter 2014-04-15
Extension of Time for Taking Action Request Received 2014-03-10
Deemed Abandoned - Failure to Respond to Maintenance Fee Notice 2014-02-24
Inactive: Office letter 2014-02-05
Inactive: Correspondence - Formalities 2014-01-10
Inactive: Correspondence - MF 2014-01-10
Inactive: Adhoc Request Documented 2013-12-17
Maintenance Request Received 2013-02-15
Amendment Received - Voluntary Amendment 2012-11-23
Amendment Received - Voluntary Amendment 2011-09-20
Inactive: S.30(2) Rules - Examiner requisition 2011-08-01
Letter sent 2011-05-26
Advanced Examination Determined Compliant - paragraph 84(1)(a) of the Patent Rules 2011-05-26
Application Published (Open to Public Inspection) 2011-05-26
Inactive: Cover page published 2011-05-25
Amendment Received - Voluntary Amendment 2011-05-19
Inactive: Office letter 2011-05-11
Inactive: S.30(2) Rules - Examiner requisition 2011-05-04
Inactive: Correspondence - Prosecution 2011-04-28
Inactive: Office letter 2011-03-31
Inactive: IPC assigned 2011-03-29
Early Laid Open Requested 2011-03-22
Inactive: Advanced examination (SO) fee processed 2011-03-22
Inactive: Advanced examination (SO) 2011-03-22
Inactive: IPC assigned 2011-03-21
Inactive: IPC assigned 2011-03-21
Inactive: IPC assigned 2011-03-16
Letter sent 2011-03-09
Inactive: IPC assigned 2011-03-08
Inactive: First IPC assigned 2011-03-08
Inactive: IPC assigned 2011-03-08
Inactive: Filing certificate - RFE (English) 2011-03-03
Filing Requirements Determined Compliant 2011-03-03
Inactive: Office letter 2011-03-03
Letter Sent 2011-03-03
Application Received - Regular National 2011-03-03
All Requirements for Examination Determined Compliant 2011-02-22
Request for Examination Requirements Determined Compliant 2011-02-22
Inactive: Advanced examination (SO) 2011-02-22
Small Entity Declaration Determined Compliant 2011-02-22

Abandonment History

Abandonment Date Reason Reinstatement Date
2015-02-24
2015-02-23
2015-02-20
2014-02-24

Maintenance Fee

The last payment was received on 2015-02-24

Note : If the full payment has not been received on or before the date indicated, a further fee may be required which may be one of the following

  • the reinstatement fee;
  • the late payment fee; or
  • additional fee to reverse deemed expiry.

Please refer to the CIPO Patent Fees web page to see all current fee amounts.

Fee History

Fee Type Anniversary Year Due Date Paid Date
Application fee - small 2011-02-22
Request for examination - small 2011-02-22
Advanced Examination 2011-03-22
MF (application, 2nd anniv.) - small 02 2013-02-22 2013-02-15
MF (application, 3rd anniv.) - small 03 2014-02-24 2015-02-24
Reinstatement 2015-02-24
Owners on Record

Note: Records showing the ownership history in alphabetical order.

Current Owners on Record
HOSSEIN NABIPOUR
Past Owners on Record
None
Past Owners that do not appear in the "Owners on Record" listing will appear in other documentation within the application.
Documents

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Document
Description 
Date
(yyyy-mm-dd) 
Number of pages   Size of Image (KB) 
Description 2011-02-22 2 115
Drawings 2011-02-22 1 65
Abstract 2011-02-22 1 36
Claims 2011-02-22 1 20
Representative drawing 2011-05-02 1 15
Cover Page 2011-05-05 2 60
Claims 2011-05-19 1 39
Drawings 2012-11-23 1 40
Acknowledgement of Request for Examination 2011-03-03 1 176
Filing Certificate (English) 2011-03-03 1 157
Notice: Maintenance Fee Reminder 2012-11-26 1 119
Notice: Maintenance Fee Reminder 2013-11-25 1 120
Courtesy - Abandonment Letter (Maintenance Fee) 2014-04-22 1 172
Second Notice: Maintenance Fee Reminder 2014-08-25 1 127
Notice: Maintenance Fee Reminder 2014-11-25 1 120
Courtesy - Abandonment Letter (Maintenance Fee) 2015-03-05 1 173
Notice of Reinstatement 2015-03-05 1 164
Second Notice: Maintenance Fee Reminder 2015-08-25 1 119
Notice: Maintenance Fee Reminder 2015-11-24 1 128
Correspondence 2011-03-03 1 16
Correspondence 2011-03-22 2 69
Correspondence 2011-03-31 1 12
Fees 2013-02-15 1 135
Correspondence 2014-01-02 4 205
Correspondence 2014-01-10 1 56
Correspondence 2014-02-05 1 18
Correspondence 2014-03-10 1 80
Correspondence 2014-04-15 1 24
Correspondence 2014-05-20 2 147
Correspondence 2014-10-30 1 37
Correspondence 2015-01-15 2 227
Correspondence 2015-02-20 2 65
Fees 2015-02-20 2 64
Fees 2015-02-24 1 124
Fees 2015-02-24 3 90
Correspondence 2015-04-14 1 32
Correspondence 2015-04-14 1 35
Correspondence 2015-05-25 2 54