IT8920618A0 - Veicolo per volo ipersonico. - Google Patents
Veicolo per volo ipersonico.Info
- Publication number
- IT8920618A0 IT8920618A0 IT8920618A IT2061889A IT8920618A0 IT 8920618 A0 IT8920618 A0 IT 8920618A0 IT 8920618 A IT8920618 A IT 8920618A IT 2061889 A IT2061889 A IT 2061889A IT 8920618 A0 IT8920618 A0 IT 8920618A0
- Authority
- IT
- Italy
- Prior art keywords
- vehicle
- hypersonic flight
- hypersonic
- flight
- Prior art date
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
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C30/00—Supersonic type aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
- B64D33/02—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
- B64D33/02—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
- B64D2033/0253—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes specially adapted for particular type of aircraft
- B64D2033/026—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes specially adapted for particular type of aircraft for supersonic or hypersonic aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Testing Of Engines (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US07/223,826 US5082206A (en) | 1988-07-25 | 1988-07-25 | Hypersonic flight vehicle |
Publications (1)
Publication Number | Publication Date |
---|---|
IT8920618A0 true IT8920618A0 (it) | 1989-05-24 |
Family
ID=22838114
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
IT8920618A IT8920618A0 (it) | 1988-07-25 | 1989-05-24 | Veicolo per volo ipersonico. |
Country Status (3)
Country | Link |
---|---|
US (1) | US5082206A (it) |
GB (1) | GB8911909D0 (it) |
IT (1) | IT8920618A0 (it) |
Families Citing this family (20)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2680831A1 (fr) * | 1991-08-28 | 1993-03-05 | Gen Electric | Procede pour etablir le profil de l'entree de la nacelle d'un moteur a turbine a gaz d'avion et entree de nacelle ainsi que nacelle obtenues a l'aide de ce procede. |
US5317866A (en) * | 1992-09-18 | 1994-06-07 | Her Majesty The Queen In Right Of Canada, As Represented By The Minister Of National Defence Of Her Majesty's Canadian Government | Free-flying tubular vehicle |
US5301901A (en) * | 1993-01-29 | 1994-04-12 | General Electric Company | Telescoping centerbody wedge for a supersonic inlet |
US5546745A (en) * | 1994-06-27 | 1996-08-20 | General Electric Company | Scramjet combustor having a two-part, aft-facing step with primary and secondary fuel injector discharge orifices |
US7240878B2 (en) * | 1996-05-13 | 2007-07-10 | Andrew James Towne | High wing monoplane aerospace plane based fighter |
US6578798B1 (en) * | 2002-04-08 | 2003-06-17 | Faruk Dizdarevic | Airlifting surface division |
US7328571B2 (en) * | 2004-11-29 | 2008-02-12 | United Technologies Corporation | Semi-axisymmetric scramjet flowpath with conformal nozzle |
US7721989B2 (en) * | 2006-03-01 | 2010-05-25 | The Boeing Company | Multi-path inlet for aircraft engine |
US7600714B2 (en) * | 2006-04-20 | 2009-10-13 | Honeywell International Inc. | Diffusing air inlet door assembly |
GB0707512D0 (en) | 2007-04-18 | 2007-05-30 | Go Science Ltd | Annular airborne vehicle |
US7988088B2 (en) * | 2008-06-05 | 2011-08-02 | Konstantinovskiy Alexandr | Tubular air transport vehicle |
MX2008015544A (es) * | 2008-12-05 | 2010-06-04 | Luis Enrique Lopez Davila | Ala con forma de cuadrado perfecto entubado. |
US8256706B1 (en) * | 2009-10-08 | 2012-09-04 | The Boeing Company | Integrated hypersonic inlet design |
US10232937B2 (en) * | 2012-12-07 | 2019-03-19 | Hypermach Aerospace Industries, Inc. | Hypersonic aircraft |
CN103174520B (zh) * | 2013-04-03 | 2015-02-11 | 南京航空航天大学 | 亚音速出流高外压内乘波式进气道及其设计方法 |
US11204000B2 (en) | 2017-03-24 | 2021-12-21 | Raytheon Company | Flight vehicle engine with finned inlet |
US11261785B2 (en) | 2017-06-06 | 2022-03-01 | Raytheon Company | Flight vehicle air breathing engine with isolator having bulged section |
US10590848B2 (en) | 2017-06-06 | 2020-03-17 | Raytheon Company | Flight vehicle air breathing propulsion system with isolator having obstruction |
US11002223B2 (en) | 2017-12-06 | 2021-05-11 | Raytheon Company | Flight vehicle with air inlet isolator having wedge on inner mold line |
US11053018B2 (en) | 2018-06-27 | 2021-07-06 | Raytheon Company | Flight vehicle engine inlet with internal diverter, and method of configuring |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1050923A (it) * | 1900-01-01 | |||
GB911074A (en) * | 1959-01-28 | 1962-11-21 | English Electric Co Ltd | Improvements in and relating to ram jet propelled aircraft |
US3027118A (en) * | 1959-01-28 | 1962-03-27 | English Electric Co Ltd | Ram jet propelled aircraft |
US3041827A (en) * | 1959-02-25 | 1962-07-03 | Curtiss Wright Corp | Supersonic inlet |
US3161379A (en) * | 1962-08-23 | 1964-12-15 | Bristel Siddeley Engines Ltd | Aircraft powerplant |
US4194519A (en) * | 1964-11-18 | 1980-03-25 | The United States Of America As Represented By The Secretary Of The Navy | Hypersonic modular inlet |
-
1988
- 1988-07-25 US US07/223,826 patent/US5082206A/en not_active Expired - Fee Related
-
1989
- 1989-05-24 IT IT8920618A patent/IT8920618A0/it unknown
- 1989-05-24 GB GB898911909A patent/GB8911909D0/en active Pending
Also Published As
Publication number | Publication date |
---|---|
US5082206A (en) | 1992-01-21 |
GB8911909D0 (en) | 1989-07-12 |
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