DE3101600A1 - Stratified charge gear motor with antechambers and afterburners as a turbine rotor - Google Patents

Abstract

The gear motors for internal combustion engines, for which universal applicability is claimed in the patent, operate as turbine rotors without oscillating machine parts in a housing and utilise fuels of all kinds better than all internal combustion engines hitherto by virtue of a longer and completely different utilisation of the internal combustion expansion gas over about 270 DEG of the 360 DEG of the arc of revolution. The problems of existing engines, e.g. reciprocating piston engines, are the expansion gas pressures required for a 4-stroke process of 2 x 360 DEG = 720 DEG for the mechanical power stroke, which extends over only 120 DEG . These pressures had to be sufficiently large to ensure that the remaining 600 DEG of circular arc and the instantaneously required torques were overcome with kinetic energy from the previous working cycle because the physically poor leverage, which varies widely in length during a stroke, is, after 120 DEG , at the bottom dead centre and end of the energy utilisation and the necessarily excessive energy residue is then released without being used before the next cycle. The same applies to turbine power plant types of construction due to excessively high throughputs and flow rates owing to poor frictional engagement. The solution in my engine inventions is as follows: a lightweight construction because high compressions are avoided, the ignition temperatures being those for diesel and heavy-oil combustion - with stratified charge as a rotary piston engine in combination with meshing engagement, used as turbine rotors. <IMAGE>

Description

1 SUBMITTED

Applicant number 1 UQ ti 402 - Breuhammer -

Stratified charge gear motor with pre-chambers and afterburners as turbine rotors

Description of the patent application

page 1

The invention relates to a gear motor in the first Operating phase works as a rotary piston machine with meshing engagement and is operated as a turbine drive in the second operating phase, in the stratified charge combination process. There are internal combustion-expansion gas-energy uses, in inexorable mechanical simplifications, from pressure to rotary movements implemented.

The current state of technology is far too inadequate Energy expenditure in all known internal combustion engines. One of the criticisms of the state of the art is the uncompromising clinging to mention outdated design principles, which include the inability to use the fuels to be able to use it better at all.

The object of the invention is fundamentally from previous ideas that could not be improved much to avert the conversion of energy as rigorously as it was with the transistor from the tube, in order to thereby create the prerequisites for to create better energy recovery.

According to the invention, the object is achieved by the .Existing, on the same inadequate basic principles not further complicated, but finally become simpler principles and machine components, with the oldest Construction element of the human being directly offered: the gearwheel. With appropriately modified gears, ingeniously designed Engine and reduction gear housings, are called Basis only applied principles without oscillating machine parts, which then the shortcomings of previous engines does not cling to the energy in the most diverse To be able to use fuels better at all.

This is only atimal with this invention, the combination won Rotary piston with mesh and turbine power unit on Gear base fully feasible, with a multitude of possible variations various types and add-on generators that generate fuel gases, for example, only in the reaction during operation, (e.g. carbide acetylene, hydrogen from granulate sponge tank, etc.)

Applicant number 1 408 402 - Brcuhammer -

Stratified charge gear mator with antechamber and afterburners as turbine rotors

Description of the patent application

page 2

Jabei Uird after starting, in the first layer charging step in the meshing region and beyond., The fuel control without air throttling made, which is particularly advantageous in exhaust critical partial load ranges and allows u _o a <, the immediate reaction of the engine during rapid load changes, among other factors "

In order to be able to construct this engine invention with a low overall weight, the high compression pressures of conventional engines were dispensed with! Because these high compression only have the purpose of high initial and ignition temperatures, the outdated basic principle of reciprocating and rotary piston engines in the 4-step process of 2X360 ° degrees of angle = 72 ° ^o total degrees of angle for one work cycle and the only possible approx ° Remaining angular degrees of a work cycle and the power requirement to be applied for the drive, the kinet. Energy is taken that had to be applied beforehand during the work cycle.)

In the following turbine engine part of the engine combination. According to this invention, the first stratified charge stage only has ignition functions with the residual use of the gases of the first stage. Diesel oil, heavy oil, coal dust or other fuel mixtures with combustion air, which were introduced into the afterburner according to power requirements, ₉ of the glowing gases of the first Stratified charge, always very reliably ignited as a second stratified charge “This means that high compression pressures are necessary for generating the ignition temperatures for diesel processes and can only be achieved with heavier engine designs _? no longer necessary at all, (dipole method is currently seen as the most economical in the ratio because of the temperature gradient that occurs the earliest: during the working stroke, as well as the relative excess air compared to other engines, but cannot be increased much more for οβg ο reasons «)

II! ■■ Il M '■ - - · ■ · B

Registration gummGr 1 4DG 402 - Breuhammer -

Stratified charge gear motor with antechamber and [Jachbrennern as turbine runners.

Description of the patent application

Sheet 3

The expansion gas pressure from the afterburners acts according to the load requirement , differently strong on both sides on the teeth, which now act as turbine blades Shoveling now constantly tooth chamber short-term closure areas 14 with pulsation-like pressure increases that are still constantly in response located gases, as well as shovel-like Überströmkauernen in the Stator housings, ωό these gases are deflected there supporting, then leading as thrust always hits the next toothed blade »This is how this pulsating, but steady expansions, pressurized gas guides around the stator, with these types of caverns in cascades Energy used as much as possible and the gas pressures and temperatures in the longest possible l \ life gradient, without not rotating in a circular manner. Intermediate components, implemented directly in rotary movements and this with the longest possible rotary lever effects for the torque on the rotor shaft.

This turbine combination works more positively than any other previous engines and therefore does not require a high gas throughput with the resulting flow velocities so far only through useless consumption and high tours, but not was solved by a change in the construction. This absolute force-fit of the invention is solved by the comb area and allows low speeds with relative low noise, because the react. Gases of the first stratified charge, as a flame holder for the turbine afterburner work.

The exhaust gas volume is before the still current unit outlet, with large exhaust gas charger blades for charging the stratified charges used to first of all, (later following attachments, which serve the relative complete exhaust gas conversion,) via suitable exhaust pipes and devices currently still in the Frnie to be directed.

310160Q

Applicant Mr. 1 40 84 02 - Breuhammer -

Stratified charge gear motor with pre-chambers and Wake-up burners as turbine runners.

Functional explanation for the file drawing of the patient application

Fresh air is made possible by S in area 7 with the tooth chambers sucked in at the start or after starting with 1 2 allowed, then blown in. This air is now in the areas 5 printed to show the oxygen content of the air with the Ignitable fuels from the nozzles 4 in the heat exchangers 5, mix as the first layer charge.

üas mixture arrives in the areas 7 in the tooth chambers and is relatively compacted in areas 19/20.

With 9 y the mixtures are ignited and pass through the expansion in the areas 10, because the pistons (teeth) from the ZyI. (Tooth chambers) are printed.

The glowing gases in the initial expansion phase shoot over 14 reaching, in areas 25, then in the afterburner stages, ωό fuel-air mixture of different levels depending on the power requirement , (Diesel oil, heavy oil, coal dust or gases,) as a second controlled stratified charge, due to the high expansion gas temperatures the first stratified charge can always be safely ignited. These expansions, compressed gases from the second layer charges, now hit coming from both sides of the afterburners, now on as turbine blades functioning teeth of the rotors (gears) and move them through the absolute frictional connection in the meshing area, Strong turns even on low tours, because the steadily but pulsating oxidizing gases reduce pressure and temperature to the maximum To do work, these are under energy "delivery in constant uiechsel up to the outlet, after the areas 14 over 15 pressure leading to the next rotor blades (teeth) passed, since the pressure gases deflected in the areas 15 supporting in the stator housing caverns, always able to deliver thrust to the rotors »

At the outlet, the exhaust gas volume, which has been degraded, makes its way through the Quantity, remaining work on the large-area loader shovels for the first shift charge.

Explanations on the principle of drawing up the files ^r J'_r '"■ ./. Ui-.cii.zP.iLnnt-Registration P 31 Π1 BOO. Π from 19.1.1 901,: u Ίεγ Huupt-Patenl-Registration P 25 b2 94Ü.0 in front 2G.11.1Ü75 / nhnradrnotnr with NACHBFiENNENN as turbine runner

1 = after b r η er du se for multi-fuel operation. Pipe door operation : - '. nlic: .. 2- afterburner stages with side part bores, for combustion air from the centrifugal high pressure compressor that works as a centrifugal compressor. Reduction gear, with cyclone cut-off for lubricant. 3 = coolant.
4 = flow channels for expansion gas; to the cascade stator

■ Gas guidance on the rotor thrust surfaces in all forms. 5 = heat exchanger.

6 = fuel nozzles, injecting into the hot heat exchanger. 7 = exhaust gas turbine, here with radial rotor. 0 = shaft for exhaust gas turbine and charger.
9 = loader with consignor.

10 = Spray nozzles for rotor chambers with lubricants and additives. which convert U.H2O into catalysts after oxidation 11 = flow channels in the tolerance gaps.

12 = pre-compression spaces, because there is a minimum gap in point 10 area. 13 = high compression pre-chamber in the foot clearance. 14 = spark plugs in the side segments, (or nozzles in the case of Dicselb.) 15 = rotor bearings, seals of the hollow shaft areas and

Flow radial grooves with the connecting holes. 16 = Variation options for slot-controlled insertion holes in the antechamber.
17 = teeth and rotor cooling system inlet and 1B = teeth and rotor cooling system outlet that with coolant

can be operated, but also with fuel to raise the level after heat absorption in gaseous form, the Bring part to be fed. 19 = ΓΊο to rsegm en te clamping fastening s screws. 20 = ignition points of the afterburner stages, after ignition and Initial expansion (according to the reverse sickle pump principle) from the preliminary stage, which is used as a start, cycle and part load stage is provided.

Oa only principles have been listed and explained here, is every conceivable type, shape and combination with not yet listed tried and tested, but also new variations possible to the stages of development and trials of this Gear turbine engine types based on Breuhammer's ideas on a license basis and therefore further development possible for everyone.

The basic idea should be:

Replacing the energy-wasting reciprocating engine with their nonsensical necessary steering forces in later years!

.5320 Salzcjitter 21, January 19th, 1981 Horst Breuhammer Oderstrasse 70 Tel. 05341/70040

BATH ORIGINAL

Claims (1)

J! U IbUU ::. *. ::. . .- *. ^: nachqefejohtI Applicant number 1 408 402 - Breuhammer - Stratified charge gear motor with antechamber and afterburners as turbine rotors. Claims of the patent application page 1 (jjj / stratified charge gear motor with pre-chambers and afterburners as Turbine rotors, made on the basis of all types of gears una forms in meshing engagement, is characterized in that gear rotors Can be produced from all suitable materials and their combinations, with minimum clearance tolerances, similar to known turbines, however even after using the Allzujeck engine, with sealing strips and / and webs, rings and other suitable sealing parts, as well as Combinations, in and on coolable rotors and / or stators and the parts of which can be provided (12,13,18,24,6 etc.) These rotors are in a coolable stator housing with hollow shafts and slot control options, but even without these only with fixed wedges, adjustable or fixed. Z.Schichtungsladungs-Zahnradmotorjnach claims 1, characterized in that when the engine is started through the intake ducts (1) or after starting with the exhaust gas turbochargers (3), fresh air passes through the insertable and controllable air exchangers (5) into their hot areas and the like .Fuel nozzles (4) in the starting phase, low-ignition fuel. or in combination with liquid and gaseous fuels, or. even such fuels that -are suitable with attachments in the reaction before and during operation with oxidant substances for exothermic reactions in the engine, only generate (uaKarbid-acetylene, hydrogen from granular sponge tank etc ₀₎ then bring to obtain a Leichtzündgemisch for the first layer charge formed which is pressed into the tooth chambers filling areas (7), where the tooth chambers were previously sprayed from the nozzles (o) with lubricants and additives for the combing area « According to the relative densification with the calves (teeth) in the Antechamber (foot relief) of the cylinder (tooth chambers), is made by the Ignition device in the side parts (9), before, in or after the deep stone combing point, these mixtures then ignited, Applicant number 1 408 402 -Brcuhammer - Stratified charge gear motor with pre-chambers and "Jachbrennern as turbine runners. Claims of the patent application page 2 S. stratified charge gear motor according to claims 1 and 2 thereby marked that after ignition, the high-energy Expansion pressurized gases push the teeth out of the tooth chambers and get into the areas (OK), the rotors rotating Through these rotary movements, the tooth chambers conveyed (14) into the short-term closure areas, thereby These glowing gases, which are only in the initial expansion phase, receive a pulsation-like short-term increase in pressure in order to Continuous rotation (due to the subsequent ignitions of the tooth chambers in the areas (8), as well as (10) as successor,) then in the Ber, (25) any glowing gases in the afterburner and there these, with all possible devices introduced, here with blower (i6) and nozzles (17) introduced combustion air diesel or heavy oil, coal dust and other fuels that are difficult to ignite of all kinds, forms and combinations-mixtures, which on simplest in controllable pulse mode, in the pulse low pressure phase the afterburner, can be brought in with little pressure, then through the glowing expansion gases of the first Stratified charge level, always ignite safely. The gases now reacting in the afterburners expand to at the same time, on both sides on what is now called the turbine blades functioning teeth and through this pressurization, in vigorous rotary movements directly implemented because of the physically long rotary lever arm, which is only available with this invention as much as possible and, moreover, always at right angles to force-decreasing shaft for the torque works. This combination of the turbine invention works through the Comb area and the first stratified charge, which acts as an absolutely secure backwater seal and flame holder for the second stratified charge the turbine function acts, thereby more force-fitting and more economical than all known turbine engines. .. ".: .. ·, .- ■: - .. ·.: .. | naghghreicht] Applicant number 1 408 402 - Breuhammer - Stratified charge gear motor with pre-chambers and Machbrennern as turbine runners Claims of the patent application Sheet 3 4 »Stratified charge gear motor, according to claims 1 to characterized in that the compressed gases that emerge after from both sides of the afterburner thrust openings are in the relative initial phase, now in constant change to those arranged in the subsequent stator housing area Short-term tooth chamber closure sections O4), in which in the Tooth chambers a pulsation-like, short-term increase in pressure then takes place until the openings of the pass Shovel-like overflow channels (15), the caverns in the StatoTpder forms the housing, always directed to both rotors will,, The expansion pressurized gases leading the rotors exercise after the deflections in the blade-like areas (15) Supporting in these stator caverns, always on the rotor blades before that a thrust, because the excess pressure of this chamber, shortly beforehand already on its rotor blades has been released before turning this chamber into the closure area of their lead sequence e, usu / .usui. Here the pressure and temperature gradient is set to a maximum Desired zero level at the outlet after the charger rotors, (which only has the volume of the gases for charging Should have available,) energy in the chamber pressure advance process, relative completely dismantled.