BE652447A - - Google Patents
Info
- Publication number
- BE652447A BE652447A BE652447DA BE652447A BE 652447 A BE652447 A BE 652447A BE 652447D A BE652447D A BE 652447DA BE 652447 A BE652447 A BE 652447A
- Authority
- BE
- Belgium
Links
Classifications
-
- 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
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/16—Aircraft characterised by the type or position of power plants of jet type
- B64D27/20—Aircraft characterised by the type or position of power plants of jet type within, or attached to, fuselages
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/38—Adjustment of complete wings or parts thereof
- B64C3/40—Varying angle of sweep
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C30/00—Supersonic type aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Toys (AREA)
- Transmission Devices (AREA)
- Harvesting Machines For Specific Crops (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US305266A US3188025A (en) | 1963-08-29 | 1963-08-29 | Means for take-off, cruise, and landing of subsonic and supersonic aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| BE652447A true BE652447A (ja) |
Family
ID=23180100
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| BE652447D BE652447A (ja) | 1963-08-29 |
Country Status (5)
| Country | Link |
|---|---|
| US (1) | US3188025A (ja) |
| BE (1) | BE652447A (ja) |
| DE (1) | DE1271557B (ja) |
| GB (1) | GB1074387A (ja) |
| NL (1) | NL6409997A (ja) |
Families Citing this family (27)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3341153A (en) * | 1965-01-13 | 1967-09-12 | Fatouras Sam | Rudderless jet aircraft |
| US3666211A (en) * | 1970-03-12 | 1972-05-30 | Mc Donnell Douglas Corp | Trijet aircraft |
| GB1262419A (en) * | 1970-07-09 | 1972-02-02 | Rolls Royce | Aircraft engine mountings |
| DE2641468C2 (de) * | 1976-09-15 | 1985-06-13 | Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn | Flugzeug mit oberhalb der Tragflügel angeordneten Triebwerken |
| IT1152763B (it) | 1982-01-25 | 1987-01-14 | Ind Aeronautiche E Meccaniche | Aeromobile perfezionato |
| US4629147A (en) * | 1984-10-16 | 1986-12-16 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Over-the-wing propeller |
| US4901950A (en) * | 1986-12-31 | 1990-02-20 | Judge Richard J | Aircraft fuselage |
| US4955559A (en) * | 1988-01-26 | 1990-09-11 | Trw Inc. | Thrust vector control system for aerospace vehicles |
| US5529263A (en) * | 1992-10-21 | 1996-06-25 | The Boeing Company | Supersonic airplane with subsonic boost engine means and method of operating the same |
| US6394392B1 (en) | 1999-10-19 | 2002-05-28 | Trimbach Turbine, Ltd. | Aircraft having multiple fuselages |
| GB2359052B (en) * | 2000-02-09 | 2003-09-17 | Rolls Royce Plc | Engine arrangement |
| US7802756B2 (en) * | 2000-02-14 | 2010-09-28 | Aerovironment Inc. | Aircraft control system |
| WO2001058756A2 (en) * | 2000-02-14 | 2001-08-16 | Aerovironment Inc. | Aircraft |
| EP1478569B1 (en) | 2002-01-30 | 2009-09-23 | Gulfstream Aerospace Corporation | Fuselage shaping and inclusion of spike on a supersonic aircraft for controlling and reducing sonic boom |
| US6698684B1 (en) | 2002-01-30 | 2004-03-02 | Gulfstream Aerospace Corporation | Supersonic aircraft with spike for controlling and reducing sonic boom |
| US20060157613A1 (en) * | 2005-01-19 | 2006-07-20 | Adamson Eric E | Supersonic aircraft with active lift distribution control for reducing sonic boom |
| CA3071172A1 (en) | 2005-12-15 | 2008-04-17 | Gulfstream Aerospace Corporation | Isentropic compression inlet for supersonic aircraft |
| US7770841B2 (en) * | 2006-12-22 | 2010-08-10 | Calvin Burgess | Inverted airfoil pylon for an aircraft |
| US8393158B2 (en) * | 2007-10-24 | 2013-03-12 | Gulfstream Aerospace Corporation | Low shock strength inlet |
| WO2012144907A1 (en) * | 2011-03-09 | 2012-10-26 | Gunnar Rosenlund | Propulsion system |
| US9120552B2 (en) * | 2011-09-13 | 2015-09-01 | Gennady Trofimovich KRESHCHISHIN | Fuselage and method for reducing drag |
| WO2014126855A1 (en) | 2013-02-14 | 2014-08-21 | Gulfstream Aerospace Corporation | Systems and methods for controlling a magnitude of a sonic boom |
| IL249908B (en) | 2016-12-28 | 2021-12-01 | Israel Aerospace Ind Ltd | Aircraft pylon |
| FR3074477B1 (fr) * | 2017-12-06 | 2019-12-20 | Airbus Operations | Avion a configuration evolutive en vol |
| US11279496B2 (en) * | 2018-02-21 | 2022-03-22 | Sikorsky Aircraft Corporation | System for reliable landing gear contact with identification of the surface |
| CN108750073B (zh) * | 2018-05-29 | 2020-06-23 | 北京航空航天大学 | 一种兼顾亚音速及超音速气动性能的可变机翼前缘 |
| WO2020142332A1 (en) * | 2018-12-31 | 2020-07-09 | DZYNE Technologies Incorporated | Drag recovery scheme for nacelles |
Family Cites Families (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US1806680A (en) * | 1931-05-26 | Adjustable engine por aircraft | ||
| DE341993C (ja) * | ||||
| GB169408A (en) * | 1920-12-30 | 1921-09-29 | Max Winckelmann | Improvements in hydro-aeroplanes |
| US1714416A (en) * | 1927-06-27 | 1929-05-21 | Cannistra Giuseppe | Aircraft |
| US1752012A (en) * | 1928-04-21 | 1930-03-25 | George Y Lauchin | Aeroplane |
| FR690450A (fr) * | 1929-02-23 | 1930-09-19 | Avion à moteur remplaçable en vol | |
| US2863620A (en) * | 1952-10-04 | 1958-12-09 | Sud Aviation | Jet-propelled aircraft |
| US2971725A (en) * | 1954-12-31 | 1961-02-14 | Sud Est Aviat Soc Nat De Const | Aircraft take-off and landing apparatus |
| US2973166A (en) * | 1955-04-21 | 1961-02-28 | Stahmer Bernhardt | Turbine principle helicopter-type blade for aircraft |
| DE961151C (de) * | 1956-02-18 | 1957-04-04 | W Blume Ingenieurbuero Fuer Le | Anordnung von TL-Triebwerken an Flugzeugen |
| GB851916A (en) * | 1957-10-21 | 1960-10-19 | Power Jets Res & Dev Ltd | Aircraft |
| DE1039846B (de) * | 1957-10-30 | 1958-09-25 | Ernst Heinkel Fahrzeugbau G M | Schwenkbare Anordnung eines Strahltriebwerkes an der Spitze einer Flugzeugtragflaeche |
| US3047255A (en) * | 1959-12-18 | 1962-07-31 | Vickers Armstrongs Aircraft | Engine mounting for swept-wing aeroplanes |
-
0
- BE BE652447D patent/BE652447A/xx unknown
-
1963
- 1963-08-29 US US305266A patent/US3188025A/en not_active Expired - Lifetime
-
1964
- 1964-08-26 DE DEP1271A patent/DE1271557B/de active Pending
- 1964-08-28 NL NL6409997A patent/NL6409997A/xx unknown
- 1964-08-28 GB GB35431/64A patent/GB1074387A/en not_active Expired
Also Published As
| Publication number | Publication date |
|---|---|
| GB1074387A (en) | 1967-07-05 |
| DE1271557B (de) | 1968-06-27 |
| US3188025A (en) | 1965-06-08 |
| NL6409997A (ja) | 1965-03-01 |