DE2132494A1 - Antriebssystem fuer Senkrechtstart - Google Patents
Antriebssystem fuer SenkrechtstartInfo
- Publication number
- DE2132494A1 DE2132494A1 DE19712132494 DE2132494A DE2132494A1 DE 2132494 A1 DE2132494 A1 DE 2132494A1 DE 19712132494 DE19712132494 DE 19712132494 DE 2132494 A DE2132494 A DE 2132494A DE 2132494 A1 DE2132494 A1 DE 2132494A1
- Authority
- DE
- Germany
- Prior art keywords
- units
- openings
- nacelle
- passage
- compressor
- 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.)
- Pending
Links
- 239000007789 gas Substances 0.000 claims description 22
- 230000007704 transition Effects 0.000 claims description 11
- 238000011144 upstream manufacturing Methods 0.000 claims description 5
- 230000006835 compression Effects 0.000 claims description 3
- 238000007906 compression Methods 0.000 claims description 3
- 238000007789 sealing Methods 0.000 claims 4
- 230000000903 blocking effect Effects 0.000 claims 2
- 238000010276 construction Methods 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 230000007246 mechanism Effects 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000000414 obstructive effect Effects 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
- B64C29/0008—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded
- B64C29/0016—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers
- B64C29/0025—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers the propellers being fixed relative to the fuselage
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US5192370A | 1970-07-02 | 1970-07-02 |
Publications (1)
Publication Number | Publication Date |
---|---|
DE2132494A1 true DE2132494A1 (de) | 1972-01-13 |
Family
ID=21974229
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE19712132494 Pending DE2132494A1 (de) | 1970-07-02 | 1971-06-30 | Antriebssystem fuer Senkrechtstart |
Country Status (6)
Country | Link |
---|---|
US (1) | US3700189A (fr) |
BE (1) | BE769445A (fr) |
CA (1) | CA936514A (fr) |
DE (1) | DE2132494A1 (fr) |
FR (1) | FR2097150B1 (fr) |
GB (1) | GB1349775A (fr) |
Families Citing this family (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4474345A (en) * | 1982-07-30 | 1984-10-02 | Ltv Aerospace And Defence Company | Tandem fan series flow VSTOL propulsion system |
SE450480B (sv) * | 1982-08-30 | 1987-06-29 | Tech Gerete Und Entwicklungsge | Styvvingad flygkropp |
US5082079A (en) * | 1990-05-04 | 1992-01-21 | Aerovironment, Inc. | Passively stable hovering system |
US5070955A (en) * | 1990-05-04 | 1991-12-10 | Aerovironment, Inc. | Passively stable hovering system |
US5390877A (en) * | 1993-06-25 | 1995-02-21 | Rolls Royce Plc | Vectorable nozzle for aircraft |
US6138946A (en) * | 1997-08-07 | 2000-10-31 | Saiz; Manuel Munuoz | Device for lift and to reduce resistance to aircraft advance |
US7493914B2 (en) * | 2005-07-20 | 2009-02-24 | Welker, Inc. | Newtonian thrust cowl array |
WO2009146084A2 (fr) * | 2008-04-02 | 2009-12-03 | Kodzo Obed Abledu | Véhicules aériens à roue tourbillonnante |
US20100193643A1 (en) * | 2008-12-31 | 2010-08-05 | Sidelkovskiy Dmitriy B | Lift fan system |
DE102014213215A1 (de) | 2014-07-08 | 2016-01-14 | Lilium GmbH | Senkrechtstarter |
US20180362171A1 (en) * | 2017-06-15 | 2018-12-20 | Donald Butler Curchod | Advanced drag reduction system for jet aircraft |
DE102020113490B4 (de) * | 2020-05-19 | 2022-08-11 | Dr. Ing. H.C. F. Porsche Aktiengesellschaft | Luftfahrzeug |
US11801991B1 (en) * | 2022-04-19 | 2023-10-31 | Kihomac, Inc. | Advanced aerial, internal carriage-compatible travel pod |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3066890A (en) * | 1953-01-23 | 1962-12-04 | Lockheed Aircraft Corp | Supersonic aircraft |
US3179353A (en) * | 1958-02-04 | 1965-04-20 | Ryan Aeronautical Co | Jet powered ducted fan convertiplane |
US3347496A (en) * | 1966-05-03 | 1967-10-17 | Ryan Aeronautical Co | Engine air inlet system for supersonic v/stol aircraft |
US3488018A (en) * | 1968-03-13 | 1970-01-06 | Us Navy | Ducted propulsion units for vtol aircraft |
-
1970
- 1970-07-02 US US51923A patent/US3700189A/en not_active Expired - Lifetime
-
1971
- 1971-03-23 CA CA108424A patent/CA936514A/en not_active Expired
- 1971-06-30 DE DE19712132494 patent/DE2132494A1/de active Pending
- 1971-07-02 FR FR7124371A patent/FR2097150B1/fr not_active Expired
- 1971-07-02 GB GB3110671A patent/GB1349775A/en not_active Expired
- 1971-07-02 BE BE769445A patent/BE769445A/fr unknown
Also Published As
Publication number | Publication date |
---|---|
GB1349775A (en) | 1974-04-10 |
US3700189A (en) | 1972-10-24 |
FR2097150B1 (fr) | 1974-03-22 |
CA936514A (en) | 1973-11-06 |
BE769445A (fr) | 1971-11-16 |
FR2097150A1 (fr) | 1972-03-03 |
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