GB1365305A - Aircraft - Google Patents
AircraftInfo
- Publication number
- GB1365305A GB1365305A GB3979470A GB3979470A GB1365305A GB 1365305 A GB1365305 A GB 1365305A GB 3979470 A GB3979470 A GB 3979470A GB 3979470 A GB3979470 A GB 3979470A GB 1365305 A GB1365305 A GB 1365305A
- Authority
- GB
- United Kingdom
- Prior art keywords
- flap
- efflux
- engine
- doors
- aug
- 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.)
- Expired
Links
- 102100033121 Transcription factor 21 Human genes 0.000 abstract 1
- 101710119687 Transcription factor 21 Proteins 0.000 abstract 1
- 239000011358 absorbing material Substances 0.000 abstract 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C23/00—Influencing air flow over aircraft surfaces, not otherwise provided for
- B64C23/005—Influencing air flow over aircraft surfaces, not otherwise provided for by other means not covered by groups B64C23/02 - B64C23/08, e.g. by electric charges, magnetic panels, piezoelectric elements, static charges or ultrasounds
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Other Liquid Machine Or Engine Such As Wave Power Use (AREA)
- Toys (AREA)
Priority Applications (4)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE19712139962 DE2139962A1 (de) | 1971-08-16 | 1971-08-10 | Anordnung zur Klappenanblasung bei Flugzeugtragflächen |
| GB3979470A GB1365305A (en) | 1971-08-16 | 1971-08-16 | Aircraft |
| US00172844A US3746283A (en) | 1971-08-16 | 1971-08-18 | Aircraft |
| FR7130070A FR2149290B3 (enExample) | 1971-08-16 | 1971-08-18 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB3979470A GB1365305A (en) | 1971-08-16 | 1971-08-16 | Aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB1365305A true GB1365305A (en) | 1974-08-29 |
Family
ID=10411549
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB3979470A Expired GB1365305A (en) | 1971-08-16 | 1971-08-16 | Aircraft |
Country Status (4)
| Country | Link |
|---|---|
| US (1) | US3746283A (enExample) |
| DE (1) | DE2139962A1 (enExample) |
| FR (1) | FR2149290B3 (enExample) |
| GB (1) | GB1365305A (enExample) |
Families Citing this family (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US8814081B2 (en) | 2010-12-27 | 2014-08-26 | Rolls-Royce North American Technologies, Inc. | Aircraft and external pod for aircraft |
| US9534537B2 (en) | 2011-03-29 | 2017-01-03 | Rolls-Royce North American Technologies Inc. | Phase change material cooling system for a vehicle |
| CN111017194B (zh) * | 2019-12-24 | 2023-08-04 | 中国航空工业集团公司西安飞机设计研究所 | 一种动力增升机翼 |
-
1971
- 1971-08-10 DE DE19712139962 patent/DE2139962A1/de active Pending
- 1971-08-16 GB GB3979470A patent/GB1365305A/en not_active Expired
- 1971-08-18 US US00172844A patent/US3746283A/en not_active Expired - Lifetime
- 1971-08-18 FR FR7130070A patent/FR2149290B3/fr not_active Expired
Also Published As
| Publication number | Publication date |
|---|---|
| FR2149290A1 (enExample) | 1973-03-30 |
| FR2149290B3 (enExample) | 1974-05-10 |
| US3746283A (en) | 1973-07-17 |
| DE2139962A1 (de) | 1972-02-24 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| GB1480340A (en) | Aircraft | |
| US3355125A (en) | Flap systems for aircraft | |
| US2699906A (en) | Air inlet for airplane gaseous combustion turbine engines | |
| GB1529886A (en) | Aerofoil tip-vortex control | |
| GB1283042A (en) | Improvements relating to aircraft | |
| GB1512719A (en) | Vertical takeoff and landing aircraft | |
| GB1014238A (en) | Improvements in ducted fan powerplants | |
| FR2076030B1 (enExample) | ||
| GB1079296A (en) | A system and method for generating lift of aircraft | |
| GB1258202A (enExample) | ||
| GB945078A (en) | Improvements in or relating to wing-fan doors of vertical take-off aircraft | |
| GB1397068A (en) | Aircraft | |
| GB1465412A (en) | Aircraft | |
| GB979910A (en) | Aircraft for taking off and landing vertically or with a short run | |
| GB1228806A (enExample) | ||
| GB1381646A (en) | Aircraft with short take-off and landing characteristics | |
| GB1333102A (en) | Propuldion power plant for aircraft | |
| GB1365305A (en) | Aircraft | |
| GB1463810A (en) | Aircraft | |
| GB1014250A (en) | Improvements in ducted fan powerplants | |
| GB1151431A (en) | Improvements in or relating to Aircraft Wings | |
| GB1071764A (en) | Improvements in or relating to aircraft or other vehicles having a sustaining or lift effect airfoil | |
| GB1302228A (enExample) | ||
| GB1135946A (en) | Improvements in aircraft | |
| GB745281A (en) | Improvements relating to aircraft |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PS | Patent sealed [section 19, patents act 1949] | ||
| PLNP | Patent lapsed through nonpayment of renewal fees |