Title: Hydrogen powered toy rocket utilizing hydrogen from the electrolysis of water
Abstract: A toy rocket assemblage including a chamber containing water and an anode and cathode and a power supply for the anode and cathode to generate oxygen and hydrogen in the chamber. A plenum chamber for collecting the oxygen and hydrogen gasses. A toy rocket on a launch tube in communication with the plenum chamber and a glow wire igniter in the plenum chamber which when heated ignites the oxygen and hydrogen gas mixture to drive the rocket off of the launch tube into the atmosphere.
Patent Number: 6,945,495 Issued on 09/20/2005 to Lund,   et al.
| Inventors:
|
Lund; Bruce D. (Chicago, IL);
Starrick; Michael (Maywood, IL)
|
| Assignee:
|
Lund and Company Invention, L.L.C. (Chicago, IL)
|
| Appl. No.:
|
889525 |
| Filed:
|
July 12, 2004 |
| Current U.S. Class: |
244/63; 124/71 |
| Intern'l Class: |
B64F 001/04 |
| Field of Search: |
244/169,63,74
124/71,73-77
89/7
60/203
204/262
446/56,52
|
References Cited [Referenced By]
U.S. Patent Documents
Primary Examiner: Barefoot; Galen
Attorney, Agent or Firm: Much Shelist Freed Denenberg Ament & Rubenstein, PC
Parent Case Text
This application is a continuation-in-part of application Ser. No. 10/348,830
filed Jan. 22, 2003, now U.S. Pat. No. 6,820,840, entitled Hydrogen Powered Toy
Rocket Utilizing Hydrogen from the Electrolysis of Water which was a continuation
of provisional application 60/353,161 filed Jan. 30, 2002 entitled Toys and Power
Driven Equipment Utilizing Hydrogen From the Electrolysis of Water.
Claims
1. A toy rocket assembly including a first chamber containing a water solution,
an anode and a cathode in said chamber, a power supply for said anode and cathode
to generate by electrolysis oxygen and hydrogen in said chamber, a plenum chamber
for collecting the hydrogen and oxygen gasses from the electrolysis of water in
the first chamber, a launch tube in communication with said plenum, a toy rocket
disposed over said launch tube and igniting means for exploding said oxygen and
hydrogen mixture in said plenum chamber to drive said rocket off of said launch
tube into the atmosphere.
2. A toy rocket assemblage as set forth in claim 1 in which the igniting means
in said plenum chamber includes a glow wire.
3. A toy rocket assemblage as set forth in claim 2 in which the plenum chamber
in which the glow wire is located is generally spherical.
4. A toy rocket assemblage as set forth in claim 1 in which the anode and cathode
in said first chamber ARE separated by a mesh member that allows for constant flow
of liquid between the cathode and anode.
5. A toy rocket assemblage as set forth in claim 1 in which an LED is provided
and illuminated when electricity is being supplied to the anode and cathode.
6. A toy rocket assemblage as set forth in claim 5 in which an LED is provided
and illuminated when the rocket is ready to launch.
Description
BACKGROUND OF THE INVENTION
It is well known to use electrolysis to separate water into its hydrogen and
oxygen
components. However, the designing and building of a reusable toy rocket assemblage
using the components of electrolysis has always been believed to be unattainable
and uneconomical and thus while desirable has eluded legions of designers and developers.
SUMMARY OF THE INVENTION
In accordance with the present invention there has been developed a novel toy
system that uses simple and inexpensive sources of power and ignition systems to
bring about the electrolysis of water and ignite the hydrogen component and capture
the explosive power obtained therefrom to power a toy rocket. The power generated
is directed in a simple, and efficient and safe manner to drive the toy rocket.
Other features and advantages will be apparent from the following drawings
and descriptions thereof in which;
FIG. 1 is a perspective view of the toy rocket launcher assembly showing the
rocket located on a launch tube prior to firing;
FIG. 2 is an enlarged view, partially broken away of Detail A, to illustrate
the chamber wherein electrolysis takes place and hydrogen and oxygen are generated;
FIG. 3 is an enlarged view, partially broken away of Detail B, to illustrate
the glow wire in the plenum chamber which is energized to explode the hydrogen
and oxygen gas mixture to launch the rocket; and
FIG. 4 is a perspective view similar to FIG. 1 with the rocket in the blast-off position.
Referring to FIGS. 1,
2 and
3, the various components of
the rocket assembly will be described.
The rocket assembly
20 includes a toy rocket
22 comprising a tubular
housing
23 that is positioned for launching on a launch tube
24.
The tubular housing
23 is provided with fins
25. It is to be noted
that the water to be used for the supply of hydrogen and oxygen gases is introduced
through the launch tube
24 which is merely one way that this can be done.
The rocket assembly includes a base assembly
26 above which is located
a chamber
27 into which the water is poured and wherein the anode
34
and cathode
38 are located. Included in the base assembly are battery packs
30 for supplying power to the various components requiring power. Specifically,
wire
32 directs electricity to the anode
34 and wire
36 feeds
electricity to the cathode
38.
A power switch
39 controls the flow of electricity to a safety switch
(not
shown) through wires
45 and
46 allowing electricity to the anode
34 and the cathode
38 in chamber
27 to bring about the electrolysis
of the water to generate oxygen gas
29 and hydrogen gas
31 therein,
which gasses
29,
31 are collected in the plenum chamber
40.
In chamber
27 the anode
34 and the cathode
38 are separated
by a mesh
49 that allows for the constant flow of liquid between the cathode
38 and anode
34. If desired, citric acid could be added to accelerate
electrolysis. It is further noted that there is an LED
52 which is illuminated
when electricity is being supplied to anode
34 and cathode
38.
Also located in plenum chamber
40 is a glow wire assembly
42 which
when electricity is provided thereto by activating the ignition switch
44
the hydrogen-oxygen gas mixture in chamber
40 explodes to drive the rocket
off its launch tube as shown in FIG. 4.
METHOD OF OPERATION
In FIG. 1 the system is in an intermediate stage wherein the power switch 39
is turned on to start the electrolysis that functions to provide oxygen gas 29
and hydrogen gas 31 in chamber 27, plenum 40 and launch tube
24. The rocket 22 sits atop the launch tube 24 and acts as
the upper seal while the anode 34 and the cathode 38 generate hydrogen
gas 31 and oxygen gas 29 in chamber 27. When sufficient amounts
of hydrogen gas 31 and oxygen gas 29 have been generated in chamber
27, plenum 40 and launch tube 24, electrolysis stops by a
generation control switch (not shown) and LED 54 is illuminated and the
rocket is ready to launch. An explosive hydrogen and oxygen gas mixture surrounds
the glow wire 42 located in plenum 40. The ignition switch 44
provides electricity to the glow wire 42 through wires 47 and 48
in conjunction with level switch 56 and the hydrogen gas mixture explodes
with a large force to launch the rocket as shown in FIG. 4.
The above process can be repeated and provides an endless source of enjoyment
for the user.
It is to be noted that while a single common chamber containing the anode and
cathode is employed in the instant embodiment, separate chambers can be used for
generating hydrogen and oxygen and a valve means for controlling the flow of gasses
to the plenum chamber 40 as disclosed in the co-pending parent application
Ser. No. 10/348,830 filed Jan. 22, 2003. In this embodiment a glow wire would be
used for ignition. In each of the embodiments the unit could be operated by a remote
control for ignition.
It is intended to cover by the appended claims all modifications and embodiments
that fall within the true spirit and scope of the invention.
*