CH398189A - Propulseur à réaction pour aérodyne - Google Patents
Propulseur à réaction pour aérodyneInfo
- Publication number
- CH398189A CH398189A CH1444362A CH1444362A CH398189A CH 398189 A CH398189 A CH 398189A CH 1444362 A CH1444362 A CH 1444362A CH 1444362 A CH1444362 A CH 1444362A CH 398189 A CH398189 A CH 398189A
- Authority
- CH
- Switzerland
- Prior art keywords
- aerodyne
- jet thruster
- thruster
- jet
- aerodyne jet
- Prior art date
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
- F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
- F02K3/025—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the by-pass flow being at least partly used to create an independent thrust component
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
- F02K1/002—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto with means to modify the direction of thrust vector
- F02K1/004—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto with means to modify the direction of thrust vector by using one or more swivable nozzles rotating about their own axis
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2220/00—Application
- F05D2220/30—Application in turbines
- F05D2220/32—Application in turbines in gas turbines
- F05D2220/328—Application in turbines in gas turbines providing direct vertical lift
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Supercharger (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB43888/61A GB976854A (en) | 1961-12-07 | 1961-12-07 | Aircraft propulsion apparatus |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CH398189A true CH398189A (fr) | 1965-08-31 |
Family
ID=10430769
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CH1444362A CH398189A (fr) | 1961-12-07 | 1962-12-07 | Propulseur à réaction pour aérodyne |
Country Status (3)
| Country | Link |
|---|---|
| US (1) | US3117750A (fr) |
| CH (1) | CH398189A (fr) |
| GB (1) | GB976854A (fr) |
Families Citing this family (23)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE1168168B (de) * | 1962-08-18 | 1964-04-16 | Daimler Benz Ag | Zweikreis-Gasturbinenstrahltriebwerk |
| GB947809A (en) * | 1962-08-24 | 1964-01-29 | Rolls Royce | Gas turbine vertical lift engine |
| GB991220A (en) * | 1963-04-25 | 1965-05-05 | Rolls Royce | Aircraft |
| GB1103571A (en) * | 1963-10-28 | 1968-02-14 | Bristol Siddeley Engines Ltd | Aircraft jet propulsion engines |
| DE1198131B (de) * | 1964-02-12 | 1965-08-05 | Daimler Benz Ag | Zweikreis-Gasturbinenstrahltriebwerk |
| DE1281853B (de) * | 1965-03-26 | 1968-10-31 | Ver Flugtechnische Werke Ges M | Senkrecht startendes und landendes Flugzeug |
| US3320749A (en) * | 1965-10-04 | 1967-05-23 | Gen Motors Corp | Regenerative fan engine |
| US3416754A (en) * | 1966-05-19 | 1968-12-17 | Gen Electric | Vectorable exhaust nozzle |
| US3424382A (en) * | 1966-05-20 | 1969-01-28 | Gen Electric | Split plug vectorable exhaust nozzle |
| US3446460A (en) * | 1966-12-23 | 1969-05-27 | Steven L Schecter | Jet and rocket engine powered air-borne vehicles |
| GB1370887A (en) * | 1970-09-26 | 1974-10-16 | Secr Defence | Aircraft and gas turbine engines therefor |
| US3779282A (en) * | 1971-11-08 | 1973-12-18 | Boeing Co | Annulus inverting valve |
| GB1514421A (en) * | 1976-01-10 | 1978-06-14 | Plessey Co Ltd | Transmission of movement to a unit mounted on a rotatable carrier |
| US4569199A (en) * | 1982-09-29 | 1986-02-11 | The Boeing Company | Turboprop engine and method of operating the same |
| US4864820A (en) * | 1987-10-22 | 1989-09-12 | United Technologies Corporation | Exhaust nozzle |
| US4962641A (en) * | 1989-02-28 | 1990-10-16 | Elizabeth Ghougasian | Pulse jet engine |
| GB2469614B (en) * | 1989-03-14 | 2011-03-23 | British Aerospace | Jet Propulsion Efflux Outlets |
| US5666803A (en) * | 1995-08-14 | 1997-09-16 | Windisch; D. Anthony | Vectored thrust compressor for remote controlled aircraft |
| CA2490886A1 (fr) * | 2002-06-28 | 2004-01-08 | Ashley Christopher Bryant | Groupe moteur a air canalise |
| US8960592B1 (en) | 2011-07-19 | 2015-02-24 | D. Anthony Windisch | VTOL propulsion for aircraft |
| CN105667782A (zh) * | 2014-11-22 | 2016-06-15 | 吴建伟 | 一种复合式垂直起降飞行器 |
| WO2019191460A1 (fr) * | 2018-03-29 | 2019-10-03 | AvionOne Innovations, LLC | Éléments de canalisation porteurs permettant la sustentation et la poussée d'un aéronef |
| US11661183B2 (en) | 2020-03-16 | 2023-05-30 | D. Anthony Windisch | Small light vertical take-off and landing capable delta wing aircraft |
Family Cites Families (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2428330A (en) * | 1943-01-15 | 1947-09-30 | Armstrong Siddeley Motors Ltd | Assembly of multistage internalcombustion turbines embodying contrarotating bladed members |
| GB881662A (en) * | 1957-01-29 | 1961-11-08 | Bristol Siddeley Engines Ltd | Improvements in or relating to gas turbine jet propulsion engine units for aircraft and also jet propelled aircraft |
| US3056258A (en) * | 1960-01-26 | 1962-10-02 | Bristol Siddeley Engines Ltd | Aircraft propulsion power units |
-
1961
- 1961-12-07 GB GB43888/61A patent/GB976854A/en not_active Expired
-
1962
- 1962-12-06 US US242825A patent/US3117750A/en not_active Expired - Lifetime
- 1962-12-07 CH CH1444362A patent/CH398189A/fr unknown
Also Published As
| Publication number | Publication date |
|---|---|
| US3117750A (en) | 1964-01-14 |
| GB976854A (en) | 1964-12-02 |
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