US3286467A

US3286467A - Plural needle electrode electrostatic thrust device

Info

Publication number: US3286467A
Application number: US426700A
Authority: US
Inventors: Robert E Hunter
Original assignee: Individual
Current assignee: Individual
Priority date: 1965-01-19
Filing date: 1965-01-19
Publication date: 1966-11-22
Anticipated expiration: 1983-11-22

Description

Nov. 22, 1966 R. E. HUNTER 3,286,467

PLURAL NEEDLE ELECTRODE ELECTROSTATIC THRUST DEVICE Filed Jan. 19, 1965 2 Sheets-Sheet 1 INVENTOR. fOEF/Pf f. fill/V769 Nov. 22, 1966 R. E. HUNTER 3,286,467

PLURAL NEEDLE ELECTRODE ELECTROSTATIC THRUST DEVICE 43 I EI 44 INVENTOR.

+ 4903547 f. l/l/IVT BYWUIPW/QW flrrae 65' United States Patent "ice 3,286,467 PLURAL NEEDLE ELECTRODE ELECTROSTATIC THRUST DEVICE Robert E. Hunter, Waynesville, Ohio, assignor to the United States of America as represented by the Secretary of the Air Force Filed Jan. 19, 1965, Ser. No. 426,700 3 Claims. (Cl. 60-202) The invention described herein may be manufactured and used by or for the United States Government for governmental purposes without the payment to me of any royalty thereon.

This invention relates to an electrostatic thrust device which uses electrostatically accelerated charged particles to provide the thrust.

One object of the invention is to provide an electrostatic thrust device which makes the use of conventional focusing and acceleration electrodes and charge neutralizing apparatus unnecessary.

A further object of the invention is to provide an electrostatic thrust device which has a more compart construction than prior art devices.

These and other objects will be more fully understood from the following detailed description taken with the drawing, wherein:

FIG. 1 is an isometric schematic view of a thrust device according to one embodiment of the invention;

FIG. 2 is an electric field plot for a portion of the device of FIG. 1; and,

FIG. 3 is an isometric schematic of a modification of the thrust portion of the device of FIG. 1.

Experimental research has been conducted for some time on the production of charged particles by spraying liquids from the ends of capillary needles maintained at a high positive electrical potential.

It has always been assumed that, when such thrust devices are built, they will incorporate more-or-less conventional ion optic electrode configurations with beam neutralization by electrons. However, the particle emission characteristics of the needles are such as to provide particles of various sizes (-charg-e-to-mass ratio) in a widely divergent stream. These two properties promise to make the focusing and acceleration of beams of these particles 2. very serious problem. Interception of some of the particles by the accelerating electrodes would cause erosion of the electrodes and severely limit the lifetime and re liability of the thrustor.

According to this invention, an array of capillary apertured electrodes are provides, each spaced from the adjacent electrodes and, each connected to an electrical potential of a polarity opposite to that of its immediate neighbor. All of the electrodes of one polarity are connected to a common propellent reservoir with another reservoir being provided for the electrodes of opposite polarity.

Reference is now made to FIG. 1 of the drawing which shows a block of insulating material having a plurality of positively charged capillary needles 11 and a plurality of negatively charged capillary needles 12 projecting therethrough. A liquid propellant is supplied to the positively charged needles 11 from a propellent supply 14 through

tubes

15, 16, 17 and 18. Liquid propellant from propellent supply 20 is supplied to the negatively charged needles 12 through

tubes

21, 22, 23 and 24. The liquid propellant is under pressure in propellent supplies 14 and 20. The positive voltage is supplied to needles 11 from a positive high-voltage supply connected to tube 15 and the negative voltage is supplied to needles 12 from a negative high-voltage supply connected to tube 21. Pres- 3,286,467 Patented Nov. 22, 1966

sure control devices

26 and 27 control the pressure of the fluid supplied to the needles 11 and 12.

One device built used needles with an inside diameter of 6 mils and a length of 1 /2 inches. The needles were spaced .788 inch along the

tubes

16, 17, 18, 22, 23 and 24. The rows of negative needles 12 were spaced from the rows of positive needles by a distance of .394 inch. The insulation material used for block 10 was Teflon. A mixture of 5 grams sodium iodide per milliliters of glycerin was used as the propellant for both the positive and negative needle-s. The supply tank gauge pressure was 5 psi. With the positive and negative needles held at voltage of plus 4 kilovolts and minus 4 kilovolts, respectively, a paper pendulum hung in front of the device was deflected at an angle of 7 degrees from the vertical. The deflection of the paper pendulum was found to be less at lower needle voltages. When used in a vacuum such as for space use, other pressures and voltages would be used. Also, other propellants could be used such as sodium bromide in glycerin, sulfuric acid in glycerin, or other propellent materials commonly used in charged particles acceleration devices.

One possible theory of the operation of the device will be given with reference to FIG. 2. The alternate needles 11 and 12 of opposite polarity set up fringe fields as shown schematically at 31 in FIG. 2. The charged particles are then accelerated by these field lines and would return to the electrode of opposite polarity if they were not met by charges of opposite polarity and neutralized. However, since they are neutralized, they continue to flow at a high velocity away from the needle electrode structure.

Other structure and arrangements than shown in FIG. 1 may be used. For example, as shown in FIG. 3, elongated capillary channel electrodes or other capillary apertured electrodes may be substituted for the needle electrodes. FIG. 3 shows a block of insulation material 10' as in FIG. 1, with a plurality of elongated positively charged capillary channel electrodes 40 with elongated apertures 41, alternatively spaced from a plurality of elongated negatively charged capillary channel electrodes 43 with elongated apertures 44. The remaining structure may be the same as in FIG. 1 and, therefore, is not shown in this figure.

While two propellent supply tanks have been shown, the propellant may be supplied from one tank when the same propellant is used for both positively and negatively charged electrodes, if a sufliciently high-resistance path is provided, between the electrodes and propellent supply, to keep leakage current to an acceptable level. Also, other materials and arrangements than those shown and described may be used. The number of needles shown is merely for illustrative purposes as more or less needles may be used in an actual device.

There is thus provided an electrostatic thrust device which may be used to electrostatically accelerate charged particles.

While certain specific embodiments have been described in detail, many changes may be made without departing from the general principles and scope of the invention.

I claim:

1. An electrostatic thrust device, comprising: a plurality of uniformly spaced capillary aperture electrodes; means for providing a flow of propellent fluid material through said electrodes; means for mounting said electrodes for directing streams of propellant into the ambient; means for connecting certain of said electrodes at a high positive potential; means for connecting the remainder of said electrodes at a high negative potential; said electrodes at a high positive potential being interspersed between and adjacent said electrodes at a high negative potential with each electrode being at an opposite electrical polarity than each of the immediately adjacent electrodes, said electrodes being located in predetermined positions for electrically accelerating sa-id streams of 5 propellant solely through the interaction of the electric fields between said electrodes for producing an electrically neutralized flow of high velocity particles into the ambient.

2. The device as recited in claim 1 wherein said capillary aperture electrodes are needle electrodes.

3. The device as recited in claim 1 wherein said capillary aperture electrodes are channel electrodes.

References Cited by the Examiner UNITED STATES PATENTS 3,052,088 9/1962 Davis et al 6035.5

3,116,433 12/1963 Yeates.

3,122,822 3/1964 Schultz et a1. 60-35.5

3,157,988 11/1964 Schultz 60-355 X 10 MARK NEWMAN, Primary Examiner.

CARLTON R. CROYLE, Examiner.

Claims

1. AN ELECTROSTATIC THRUST DEVICE, COMPRISING: A PLURALITY OF UNIFORMLY SPACED CAPILLARY APERTURE ELECTRODES; MEANS FOR PROVIDING A FLOW OF PROPELLENT FLUID MATERIAL THROUGH SAID ELECTRODES; MEANS FOR MOUNTING SAID ELECTRODES FOR DIRECTING STREAMS OF PROPELLANT INTO THE AMBIENT; MEANS FOR CONNECTING CERTAIN OF SAID ELECTRODES AT A HIGH POSITIVE POTENTIAL; MEANS FOR CONNECTING THE REMAINDER OF SAID ELECTRODES AT A HIGH NEGATIVE POTENTIAL; SAID ELECTRODES AT A HIGH POSITIVE POTENTIAL BEING INTERSPERSED BETWEEN AND ADJACENT SAID ELECTRODES AT A HIGH NEGATIVE POTENTIAL WITH EACH ELECTRODE BEING AT AN OPPOSITE ELECTRICAL POLARITY WITH EACH ELECTRODE BEING AT AN OPPOSITE ELECTRODES, SAID ELECTRODES BEING LOCATED IN PREDETERMINED POSITIONS FOR ELECTRICALLY ACCELERATING SAID STREAMS OF PROPELLANT SOLELY THROUGH THE INTERACTION OF THE ELECTRIC FIELDS BETWEEN SAID ELECTRODES FOR PRODUCING AN ELECTRICALLY NEUTRALIZED FLOW OF HIGH VELOCITY PARTICLES INTO THE AMBIENT.