DE3627322A1 - Turbojet - Google Patents

Turbojet

Info

Publication number
DE3627322A1
DE3627322A1 DE19863627322 DE3627322A DE3627322A1 DE 3627322 A1 DE3627322 A1 DE 3627322A1 DE 19863627322 DE19863627322 DE 19863627322 DE 3627322 A DE3627322 A DE 3627322A DE 3627322 A1 DE3627322 A1 DE 3627322A1
Authority
DE
Germany
Prior art keywords
nozzle
cow horn
cow
balanced
thrust
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Ceased
Application number
DE19863627322
Other languages
German (de)
Inventor
Erfinder Wird Nachtraeglich Benannt Der
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
WERDING, HANS, 4520 MELLE, DE
Original Assignee
Individual
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to DE19863627322 priority Critical patent/DE3627322A1/en
Publication of DE3627322A1 publication Critical patent/DE3627322A1/en
Ceased legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/14—Gas-turbine plants characterised by the use of combustion products as the working fluid characterised by the arrangement of the combustion chamber in the plant
    • F02C3/16—Gas-turbine plants characterised by the use of combustion products as the working fluid characterised by the arrangement of the combustion chamber in the plant the combustion chambers being formed at least partly in the turbine rotor or in an other rotating part of the plant
    • F02C3/165—Gas-turbine plants characterised by the use of combustion products as the working fluid characterised by the arrangement of the combustion chamber in the plant the combustion chambers being formed at least partly in the turbine rotor or in an other rotating part of the plant the combustion chamber contributes to the driving force by creating reactive thrust
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K7/00—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof
    • F02K7/005—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof the engine comprising a rotor rotating under the actions of jets issuing from this rotor

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Jet Pumps And Other Pumps (AREA)
  • Other Liquid Machine Or Engine Such As Wave Power Use (AREA)

Abstract

Published without abstract.

Description

Bei einer herkömmlichen Rakete und einem Strahltriebwerk bewir­ ken Rückstoß und Durchfluß den Vortrieb.With a conventional rocket and a jet engine recoil and flow the propulsion.

Mit meiner Neuerung leite ich den Gasstrahl durch ein konisches und gebogenes Rohr und mehrere Verbrennungskammern. In dem spi­ ralförmigen Rohr wandel ich den Gasstrahldruck in Druck- und Unterdruckzonen um, die auf die Rohrwandung wirken und die sy­ metrisch gelagerte Düse in Drehung bringt. Die Länge meines spiralförmigen, konischen Schlangenrohres und die Anzahl der Verbrennungskammern, die im Verhältnis zur ersten Verbrennungs­ kammer stehen, bestimmen Verbrennungsgrad, Lärmstärke, Wir­ kungsgrad und Gasmenge.With my innovation, I direct the gas jet through a conical one and bent tube and several combustion chambers. In the spi raliform tube I convert the gas jet pressure into pressure and Vacuum zones around, which act on the pipe wall and the sy metric nozzle rotates. The length of mine spiral, conical snake tube and the number of Combustion chambers that are in proportion to the first combustion standing chamber, determine degree of combustion, noise level, we efficiency and amount of gas.

Bei optimalem Verhältnis erreiche ich restlose Verbrennung, Ge­ räuschlosigkeit bei hohem Wirkungsgrad.With an optimal ratio I achieve complete combustion, Ge noiselessness with high efficiency.

Auf meiner Zeichnung "2" habe ich ein Pulso-Strahl­ triebwerk mit meinem düsenförmigen Abströmrohr, drehbar gela­ gert, als Luftblatttrieb gezeichnet, bei "1" ein Strahltrieb­ werk und auf Blatt "3" das System.On my drawing "2" I have a pulsed jet engine with my nozzle-shaped outflow pipe, rotatably mounted, drawn as an air bladed drive, at "1" a jet engine and on sheet "3" the system.

Vorteil der Neuerung:
Da eine Reihe von Energieumsetzungsprozesse und deren Verluste vermieden werden, niedrige Fertigungskosten, geräuscharme, vollkommene Verbrennung, geringe Wartungskosten, leichte Bau­ weise.Advantage of the innovation:
Because a number of energy conversion processes and their losses are avoided, low manufacturing costs, low-noise, perfect combustion, low maintenance costs, lightweight construction.

Claims (8)

Oberbegriff:
StrahltriebturbineGeneric term:
Jet engine turbine Kennzeichnender Teil:
Kuhhorn- oder schlangenförmige Gasab­ strömdüse.Characteristic part:
Cow horn or serpentine gas outlet nozzle. Oberbegriff/Merkmale:
Abströmrohr sieht wie ein Kuhhorn oder eine Schlange aus.General term / characteristics:
Drain pipe looks like a cow horn or a snake. Erfinderische Merkmale:
Eine herkömmliche Impulsorakete oder Ex­ plosionsraum mit der kuhhornförmigen Abströmdüse setzt die ge­ samte Energie, in dem Kuhhorn aus Blech, in Schub um. Atmosphä­ rischer Rückstoß erfolgt nicht, so daß diese Technik im Welt­ raum ihre Höchstleistung erreicht und dort unendlich zu be­ schleunigen ist.Inventive features:
A conventional impulse rocket or explosion room with the cowhorn-shaped outflow nozzle converts the entire energy, in the cow horn made of sheet metal, into thrust. Atmospheric recoil does not occur, so that this technology achieves its maximum performance in space and can be accelerated there infinitely. Raumfahrzeuge mit dieser Technik ausgerüstet können Lichtge­ schwindigkeit erreichen.Spacecraft equipped with this technology can light reach speed. Bei Verwendung des Kuhhorns als Turbine hat sie als weiteres Merkmal: daß Fliehkräfte ausgelöst werden, sie also nicht ausgewuchtet werden brauchen und nur geringe Lagerkräfte auftreten.When using the cow horn as a turbine, it has as another characteristic: that centrifugal forces are triggered, ie do not need to be balanced and only low bearing forces occur. Wie die Abströmdüse als Tragfläche profiliert oder mit einem Luftblatt verbunden werden bei pendelbarer Aufhängung Flieh-, Kreisel-, Wind- und Düsenschubkräfte selbständig ausbalanciert und ein Auswuchten unnötig.Like the discharge nozzle profiled as a wing or with a Air sheet can be connected with pendulum suspension centrifugal, Gyro, wind and nozzle thrust independently balanced and balancing unnecessary. Alle Schrauben, Eisenbleche, Splinte, Rohre, die zur Fertigung nötig sind, sind Normteile.All screws, iron sheets, split pins, pipes that are used in manufacturing standard parts are necessary.
DE19863627322 1986-08-12 1986-08-12 Turbojet Ceased DE3627322A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
DE19863627322 DE3627322A1 (en) 1986-08-12 1986-08-12 Turbojet

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19863627322 DE3627322A1 (en) 1986-08-12 1986-08-12 Turbojet

Publications (1)

Publication Number Publication Date
DE3627322A1 true DE3627322A1 (en) 1988-06-01

Family

ID=6307219

Family Applications (1)

Application Number Title Priority Date Filing Date
DE19863627322 Ceased DE3627322A1 (en) 1986-08-12 1986-08-12 Turbojet

Country Status (1)

Country Link
DE (1) DE3627322A1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE10118373B4 (en) * 2001-04-12 2009-04-09 Josef Geimer Rotary ramjet engine as drive unit in stationary and mobile applications

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DD15849A (en) *
GB314722A (en) * 1928-09-11 1929-07-04 Hans Strauscheid A reaction gas turbine
DE557859C (en) * 1928-11-28 1932-08-29 Explorotor A G Rotary engine whose impeller is provided with channels for the passage of the propellant
US2644301A (en) * 1949-02-08 1953-07-07 Karlby Henning Ram jet turbine
US2978205A (en) * 1958-09-29 1961-04-04 Ryan Aeronautical Co Tip-jet driven ducted fan for aircraft
US3008293A (en) * 1957-05-18 1961-11-14 Snecma Intermittently-operating thermo-propulsive duct designed for driving a shaft and applicable to rotary wing aircraft
US3677503A (en) * 1968-07-31 1972-07-18 Carlos A Freeman Jr Reaction--impulse--counterrotating--airfoil

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DD15849A (en) *
GB314722A (en) * 1928-09-11 1929-07-04 Hans Strauscheid A reaction gas turbine
DE557859C (en) * 1928-11-28 1932-08-29 Explorotor A G Rotary engine whose impeller is provided with channels for the passage of the propellant
US2644301A (en) * 1949-02-08 1953-07-07 Karlby Henning Ram jet turbine
US3008293A (en) * 1957-05-18 1961-11-14 Snecma Intermittently-operating thermo-propulsive duct designed for driving a shaft and applicable to rotary wing aircraft
US2978205A (en) * 1958-09-29 1961-04-04 Ryan Aeronautical Co Tip-jet driven ducted fan for aircraft
US3677503A (en) * 1968-07-31 1972-07-18 Carlos A Freeman Jr Reaction--impulse--counterrotating--airfoil

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE10118373B4 (en) * 2001-04-12 2009-04-09 Josef Geimer Rotary ramjet engine as drive unit in stationary and mobile applications

Similar Documents

Publication Publication Date Title
US4204799A (en) Horizontal wind powered reaction turbine electrical generator
CA2220147A1 (en) Multistage two-phase turbine
GB1602235A (en) Crossover duct
KR920008359A (en) Centrifugal compressor with pipe diffuser and collector
GB1602939A (en) Crossover duct assembly primarily for multi-stage compressors
US2947139A (en) By-pass turbojet
RU2087376C1 (en) Water-jet propeller
US4141219A (en) Method and turbine for extracting kinetic energy from a stream of two-phase fluid
DE3627322A1 (en) Turbojet
WO2002002935A1 (en) Fluid channelling spiro-helical rotor with slides
US3877835A (en) High and low pressure hydro turbine
US2804747A (en) Gas turbine power plant with a supersonic centripetal flow compressor and a centrifugal flow turbine
US4201049A (en) Turbine power plant
DE3126749A1 (en) Wind rotor with air flow guide stator
US3221496A (en) Ramjet motor with multi-stage burning
DE2713555A1 (en) Turbine power output enhancement method - has pump which accelerates flow of fluid supplied to turbine
CN214944759U (en) Gas trapping device for space air suction type electric propulsion system
GB2074249A (en) Power Plant
EP0188445A1 (en) Torque assist device for a multi-barrel weapon.
RU2073111C1 (en) Vortex-type windmill plant
US4514137A (en) Method for driving two-phase turbines with enhanced efficiency
DE4024199A1 (en) Tube ring turbine system - has internal pressure generated by combustion
RU1795224C (en) Flue device
CN214930747U (en) Collimating structure for gas trapping device
RU2805400C1 (en) Pressure-vacuum wind power plant

Legal Events

Date Code Title Description
8127 New person/name/address of the applicant

Owner name: WERDING, HANS, 2800 BREMEN, DE

8127 New person/name/address of the applicant

Owner name: WERDING, HANS, 4520 MELLE, DE

8181 Inventor (new situation)

Free format text: ERFINDER IST ANMELDER

8110 Request for examination paragraph 44
8131 Rejection