GB2177989A - Aircraft fuselage tails - Google Patents
Aircraft fuselage tails Download PDFInfo
- Publication number
- GB2177989A GB2177989A GB08618031A GB8618031A GB2177989A GB 2177989 A GB2177989 A GB 2177989A GB 08618031 A GB08618031 A GB 08618031A GB 8618031 A GB8618031 A GB 8618031A GB 2177989 A GB2177989 A GB 2177989A
- Authority
- GB
- United Kingdom
- Prior art keywords
- ofthe
- cross
- tail
- aircrafttail
- radius
- 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.)
- Withdrawn
Links
- 230000007704 transition Effects 0.000 claims 1
- 230000004048 modification Effects 0.000 description 23
- 238000012986 modification Methods 0.000 description 23
- 238000000926 separation method Methods 0.000 description 16
- 238000010586 diagram Methods 0.000 description 4
- 238000006073 displacement reaction Methods 0.000 description 3
- 238000009826 distribution Methods 0.000 description 2
- 230000002349 favourable effect Effects 0.000 description 2
- 230000000717 retained effect Effects 0.000 description 2
- 230000008719 thickening Effects 0.000 description 2
- 101100379080 Emericella variicolor andB gene Proteins 0.000 description 1
- 230000001427 coherent effect Effects 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C2001/0045—Fuselages characterised by special shapes
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/10—Drag reduction
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Lining And Supports For Tunnels (AREA)
- Underground Or Underwater Handling Of Building Materials (AREA)
- Lining Or Joining Of Plastics Or The Like (AREA)
- Casting Or Compression Moulding Of Plastics Or The Like (AREA)
- Main Body Construction Of Washing Machines And Laundry Dryers (AREA)
- Toys (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE19853526472 DE3526472A1 (de) | 1985-07-24 | 1985-07-24 | Rumpfheckmodifikation von flugzeugen |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| GB8618031D0 GB8618031D0 (en) | 1986-08-28 |
| GB2177989A true GB2177989A (en) | 1987-02-04 |
Family
ID=6276637
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB08618031A Withdrawn GB2177989A (en) | 1985-07-24 | 1986-07-23 | Aircraft fuselage tails |
Country Status (5)
| Country | Link |
|---|---|
| US (1) | US4712751A (enExample) |
| JP (1) | JPS6226200A (enExample) |
| DE (1) | DE3526472A1 (enExample) |
| FR (1) | FR2585326B3 (enExample) |
| GB (1) | GB2177989A (enExample) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| USD308663S (en) | 1987-05-06 | 1990-06-19 | The Boeing Company | Airplane |
| US4953812A (en) * | 1987-11-13 | 1990-09-04 | The Boeing Company | Aircraft configuration with aft mounted engines and method |
| US4976396A (en) * | 1987-11-13 | 1990-12-11 | The Boeing Company | Aircraft configuration with aft mounted engines |
Families Citing this family (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE4404810C2 (de) * | 1994-02-16 | 1999-12-09 | Daimler Chrysler Aerospace | Rumpfheck für ein Verkehrsflugzeug |
| US5692704A (en) * | 1995-06-07 | 1997-12-02 | Buttgereit; Volker | Body tail unit for a commercial aircraft |
| US5677508A (en) * | 1995-08-15 | 1997-10-14 | Hughes Missile Systems Company | Missile having non-cylindrical propulsion section |
| US5908175A (en) * | 1997-11-19 | 1999-06-01 | Magnes; Gene | One-piece airplane tail-cone with inspection door(s) |
| DE102010045588B4 (de) * | 2010-09-16 | 2017-04-06 | Airbus Operations Gmbh | Rumpfsegment für ein Luftfahrzeug |
| ES2709346T3 (es) * | 2015-03-06 | 2019-04-16 | Airbus Operations Gmbh | Mamparo de presión trasero extendido |
| CN117279831A (zh) * | 2021-03-10 | 2023-12-22 | Zsm控股有限责任公司 | 后机身向上偏折的飞机机身构型 |
Family Cites Families (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE674433C (de) * | 1937-05-08 | 1939-04-14 | Messerschmitt Boelkow Blohm | An Luftfahrzeugen angeordnete, aus Wellblech bestehende Aussenbeplankung |
| FR1114301A (fr) * | 1954-04-05 | 1956-04-11 | Procédé économique de construction cellulaire | |
| US3023860A (en) * | 1957-03-18 | 1962-03-06 | Floyd P Ellzey | Body construction |
| US3955781A (en) * | 1974-03-10 | 1976-05-11 | Andrei Nikolaevich Tupolev | Supersonic aircraft with the engines disposed under the delta wing middle portion |
-
1985
- 1985-07-24 DE DE19853526472 patent/DE3526472A1/de active Granted
-
1986
- 1986-07-16 US US06/886,792 patent/US4712751A/en not_active Expired - Lifetime
- 1986-07-23 GB GB08618031A patent/GB2177989A/en not_active Withdrawn
- 1986-07-23 FR FR8610711A patent/FR2585326B3/fr not_active Expired
- 1986-07-24 JP JP61172924A patent/JPS6226200A/ja active Pending
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| USD308663S (en) | 1987-05-06 | 1990-06-19 | The Boeing Company | Airplane |
| US4953812A (en) * | 1987-11-13 | 1990-09-04 | The Boeing Company | Aircraft configuration with aft mounted engines and method |
| US4976396A (en) * | 1987-11-13 | 1990-12-11 | The Boeing Company | Aircraft configuration with aft mounted engines |
Also Published As
| Publication number | Publication date |
|---|---|
| JPS6226200A (ja) | 1987-02-04 |
| FR2585326A1 (fr) | 1987-01-30 |
| DE3526472C2 (enExample) | 1987-05-07 |
| GB8618031D0 (en) | 1986-08-28 |
| FR2585326B3 (fr) | 1987-10-16 |
| US4712751A (en) | 1987-12-15 |
| DE3526472A1 (de) | 1987-02-05 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| GB2177989A (en) | Aircraft fuselage tails | |
| EP0525912B1 (en) | Wing/winglet configurations and methods for aircraft | |
| EP0122790B1 (en) | Aircraft wing and winglet arrangement | |
| US7100867B2 (en) | Lifting foil | |
| CN112088124A (zh) | 翼身后缘整流罩及其制造方法 | |
| KR20140048256A (ko) | 윙의 윙팁 장치 및 이러한 윙팁 장치를 갖는 윙 | |
| EP3366572A1 (en) | Protective finish for wing tip devices | |
| EP3626609B1 (en) | A wing tip device | |
| Hefner et al. | An overview of concepts for aircraft drag reductions | |
| WO1995017334A1 (en) | Aircraft wing/nacelle combination | |
| CN210681131U (zh) | 一种机翼结构 | |
| US11447239B2 (en) | Aircraft wing and wing tip device | |
| Smith | Three-dimensional viscous and inviscid separation of a vortex sheet from a smooth non-slender body | |
| US4377267A (en) | Vortex tranquilizer | |
| CN110386243B (zh) | 一种高升阻比的低速无人机翼型 | |
| CN105000159A (zh) | U型风帆结构 | |
| Lee Jr et al. | Installation effects of long-duct pylon-mounted nacelles on a twin-jet transport model with swept supercritical wing | |
| Liu et al. | Flow patterns and aerodynamic characteristics of a wing-strake configuration | |
| CN107444611A (zh) | 一种高升力通用飞机翼型 | |
| CN107745796B (zh) | 一种背负式大型天线罩双支腿 | |
| GB2171361A (en) | Separation plate for hydrofoil keel for sailing vessels | |
| Shevell | Aerodynamic bugs-can cfd spray them away? | |
| CN102167154A (zh) | 飞机翼尖装置 | |
| Lawford | Low-speed wind-tunnel tests on an unswept wing-fuselage model of aspect ratio 9.8, with tangential blowing over trailing-edge flaps and ailerons, including the effect of slipstream | |
| Zhang et al. | On forward-swept wing's aerodynamic characteristics |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| WAP | Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1) |