US2758441A

US2758441A - Glow plug igniter structure

Info

Publication number: US2758441A
Application number: US269192A
Authority: US
Inventors: Emil O Kalil; Sidney G Rumbold; Pool Douglas G Vander
Original assignee: MW Kellogg Co
Current assignee: MW Kellogg Co
Priority date: 1952-01-31
Filing date: 1952-01-31
Publication date: 1956-08-14
Anticipated expiration: 1973-08-14

Description

Aug. 14, 1956 E. o. KALlL ETAL GLOW PLUG IGNITER STRUCTURE 2 Sheets-Sheet 1 Filed Jan. 31, 1952 I INVENTORS. EMIL O. KALIL- v SIDNEY O. RUMBOLD DOUGLAS G.VANDER POOL BY ,Z

ATTORNEY 1956 E. o. KALIL ETAL GLOW PLUG IGNITER STRUCTURE Filed Jan. 31, 1952 2 SheetsSheet 2 m s V o i W W m IIILUW \h v LR A r mm KIG .GS E N L ID V a WSW Y B a W mm w N mm om ATTORNEY GLOW PLUG IGNIIER STRUCTURE Emil O. Kalil, Brooklyn, N. Y., and Sidney G. Rumbold,

Bergenfield, and Douglas G. Vander Pool, Bloomingdale, N. J., assignors to The M. W. Kellogg Com-.

pany, Jersey City, N. J., a corporation of Delaware Application January 3 1, 1952, Serial No. 269,192 2 Claims. (Cl. 60-3932) This invention relates to the combustion apparatus in a jet propulsion or similar device, and more particularly is directed to a structure which ignites a mixture of two or more fluid propellant components, the resultant flame being used to start a reaction in the combustion chamber of a jet propulsion or similar device.

It is an object of this invention to provide an improved means for igniting a mixture of two or more fluid propellant components.

It is another object of this invention to provide an improved igniter structure whereby an ignition flame is secured without undue wear resulting thereto.

It is a further object to apply the means for igniting mixed fluid propellant components to the start of the combustion process in a jet propulsion or similar device.

Another further object of this invention is to apply a means for ignition to the combustion of non-hypergolic propellant components, e. g. oxidizer and fuel, in rocket thrust cylinders and the like.

These and other objects and advantages of this invention will become apparent from a reading of the following description of preferred embodiments thereof as illustrated in the accompanying drawings in which:

Fig. 1 is a partly cross sectional view of a general form of an igniter structure, taken along line 1-1 of Fig. 2.

Fig. 1a is a similar cross sectional view of a modification of the general form of igniter structure disclosed in Fig. 1.

Fig. 2 is a sectional view taken along the lines 2-2 of Fig. 1.

Fig. 3 is a view, similar to that of Fig. 1, of a preferred form of igniter structure.

Fig. 4 is a sectional view taken along line 4-4 of Fig. 3.

Fig. 5 is a diagram showing the application of the igniter structure of Fig. 3 to a gas generating device.

Referring to the drawings, the embodiment of the invention as illustrated in Fig. 1, discloses an igniter structure 10, consisting of a tubular body 11, of substantial cylindrical shape, with an open end 12, and a heating element 13, mounted at the center of the opposite closed end 14. The heating element can be a conventional type, electrically operated glow plug, consisting of either platinum or nichrome wires, which may or may not be supported on a ceramic core. Also the wires may be enclosed in a metal or ceramic jacket. The use of a common spark plug is not proscribed in this igniter structure.

At 15 and 16 are disclosed oppositely spaced injectors for the admission of fluid propellant components (e. g. oxidizer and fuel respectively), which are inserted in

undercut orifices

17 and 18, in the wall of the tubular body adjacent the heating element 13, and directed at right angles toward it. The propellant components can be admitted either in the form of a hollow cone, atomizing spray or as a stream, and generally are nitric acid as the oxidizer and either a hydrocarbon or ammonia as the fuel. The depth of the undercut of the

orifices

17 and 18 is limited, so that the injection of the propellant components is not adversely affected, yet there is suflicient protection from the heat of combustion to heating, of the injector tips.

In Fig. l, the injected propellant components are disclosed directed against the heating element. In the event that hollow cone, atomizing spray injection is used, con-' tact of the propellant components with the heating element is made adjacent the locus of contact of the opposed spray cones and, depending on the dimensions of the cones and length of heating element, either along one- I When stream injection is used, the injectors can be directed at the heating ole-1 ment for a splash and spray effect from the impinge-;

or two curves of intersection.

ment of the streams therewith or they may be aimed .to provide the same. effect by contact of opposed streams away from the heating element. Furthermore, the;in---; jectors can belocated so that the propellant component sprays or streams impinge on each other downstream of the heating element as shown in Fig. 1a, the

injectors

15, 16, being inserted in downstream located

undercut orifices

17a and 18a.

- In the modification illustrated in Figs. 3 and 4, an igniter structure is disclosed at 20, consisting of a cylindrical body 21, an outlet or exit nozzle 22, and a plurality of equally spaced heating elements 23 (for purposes of illustration, three are shown), inserted radially into the chamber defined by the cylindrical body and the closed ends 24, at the center of which,

injectors

25 and 26 are inserted in

undercut orifices

27 and 28, for the respective admission of the fluid propellant components of oxidizer and fuel (e. g. nitric acid and a hydrocarbon such as gasoline). These injectors may be either the hollow cone, atomizing spray type or the stream type and are directed so that the loci of the impingements of the cone sprays or streams are in the vicinity of the mid-points of the radially inserted heating elements.

In this manner, the portions of the heating elements surfaces in a single igniter structure, any one of them is capable of'starting the required ignition, because only a very small fraction of the total of the propellant components injected enter into the initial ignition.

The means for mixing the injected fluid propellant components on or in the vicinity of the heating elements provides an ignitable mixture of propellant components at the most favorable location for ignition, while the mixing of the total injected flow provides an ignitable mass for sustaining the combustion after start of the ignition at any of the heating elements.

Fig. 5 discloses a specific application of the preferred form of igniter structure, disclosed in Figs. 3 and 4, to a gas generator 30. (A combustion chamber of a jet propulsion device is just as pertinent for an illustration.) The gas generator has a generally cylindrical body wall 31, and end wall 32, on which the igniter structure. is mounted and opposite end wall 33, with outlet 34 mounted thereon. Oxidizer and fuel injectors are shown respectively at 35 and 36, inserted through

undercut orifices

37 and 38 and so located that the injected components are in the path of the flame from the igniter structure.

2,758,441 I Patented Aug. 14,v d

PI'EVCIlt overciiemieal reaction of combustion wi th" the' result that thbrd'is a s'tabl'el operation at a; predetermined teritp'e'ratu'rwdver' the entire gas generator unit. The-excess fuel" is admittedby injectors 39- inserted through undercut orifices 40 and the quantity can be' varied so that the" exitt g'as temperatures are controlled over a Wide range 00 reproduc'eable limits. In this manner, the initial fian'l'e' from the ignite'r structure may be increased into a flame of a'ny' siz'e' desired. a

Although many changes canbe made in the disclosed apparatus" without departing fromthe scope of the inventidntit is intended that. all matter contained in the above description and shown in accompanying draw ingu shall be interpretedas illustrative" and not limitativbb 7 What is claimed is? i 11- Anigniter structure for theiniti'ation-of the combustio'n' ofi a plurality of fluid propellant components comprising ahollow substantially cylindrical body having closed ends and an outlet opening intermediate said ends; means mounted on said ends for admitting" fluid propellant components into said body, means for igniting said components comprising a heating element, said first mentioned means being arranged in opposed relationship and located for contact of the admitted components to occur at the approximate mid-point of said last mentioned means.

2. The combination of elements as set out in claim 1 wherein said last mentioned means comprise a plurality of equally spaced glow plugs, inserted radially into said body substantially intermediate the ends thereof.

References Cited in the file of this patent UNITED STATES PATENTS

Claims

1. AN IGNITER STRUCTURE FOR THE INITIATION OF THE COMBUSTION OF A PLURALITY OF FLUID PROPELLANT COMPONENTS COMPRISING A HOLLOW SUBSTANTIALLY CYLINDRICAL BODY HAVING CLOSED ENDS AND AN OUTLET OPENING INTERMEDIATE SAID ENDS, MEANS MOUNTED ON SAID ENDS FOR ADMITTING FLUID PROPELLANT COMPONENTS INTO SAID BODY, MEANS FOR INGITING SAID COMPONENTS COMPRISING A HEATING ELEMENT, SAID FIRST MENTIONED MEANS BEING ARRANGED IN OPPOSED RELATIONSHIP AND LOCATED FOR CONTACT OF THE ADMITTED COMPONENTS TO OCCUR AT THE APPROXIMATE MID-POINT OF SAID LAST MENTIONED MEANS.