GB9409420D0 - Thrust nozzle for jet engines with securing elements - Google Patents
Thrust nozzle for jet engines with securing elementsInfo
- Publication number
- GB9409420D0 GB9409420D0 GB9409420A GB9409420A GB9409420D0 GB 9409420 D0 GB9409420 D0 GB 9409420D0 GB 9409420 A GB9409420 A GB 9409420A GB 9409420 A GB9409420 A GB 9409420A GB 9409420 D0 GB9409420 D0 GB 9409420D0
- Authority
- GB
- United Kingdom
- Prior art keywords
- securing elements
- jet engines
- thrust nozzle
- thrust
- nozzle
- 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.)
- Granted
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
- F02K1/78—Other construction of jet pipes
- F02K1/80—Couplings or connections
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
- F02K1/78—Other construction of jet pipes
- F02K1/82—Jet pipe walls, e.g. liners
- F02K1/822—Heat insulating structures or liners, cooling arrangements, e.g. post combustion liners; Infrared radiation suppressors
-
- 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
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Nozzles (AREA)
- Connection Of Plates (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE4317807A DE4317807C1 (en) | 1993-05-28 | 1993-05-28 | Thruster for jet drives with fasteners |
Publications (3)
Publication Number | Publication Date |
---|---|
GB9409420D0 true GB9409420D0 (en) | 1994-06-29 |
GB2278403A GB2278403A (en) | 1994-11-30 |
GB2278403B GB2278403B (en) | 1996-09-25 |
Family
ID=6489144
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB9409420A Expired - Fee Related GB2278403B (en) | 1993-05-28 | 1994-05-11 | Thrust nozzle for jet engines |
Country Status (3)
Country | Link |
---|---|
DE (1) | DE4317807C1 (en) |
FR (1) | FR2705736A1 (en) |
GB (1) | GB2278403B (en) |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE19633589A1 (en) * | 1996-08-21 | 1998-02-26 | Mtu Muenchen Gmbh | Outlet nozzle for reaction motor combustion chamber |
RU2516760C1 (en) * | 2013-04-11 | 2014-05-20 | Оао Умпо | Turbojet adjustable nozzle |
DE102018212757B3 (en) * | 2018-07-31 | 2019-11-14 | Siemens Healthcare Gmbh | Gradient coil and method for producing a gradient coil |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3701704A (en) * | 1970-05-18 | 1972-10-31 | Mc Donnell Douglas Corp | Method of fabricating a rocket nozzle liner |
US3826708A (en) * | 1970-05-18 | 1974-07-30 | Mc Donnell Douglas Corp | Rocket nozzle liner construction |
DE3618038A1 (en) * | 1986-05-28 | 1987-12-03 | Messerschmitt Boelkow Blohm | SUPPORT STRUCTURE FOR LIQUID-COOLED EXPANSION NOZZLES |
US4920742A (en) * | 1988-05-31 | 1990-05-01 | General Electric Company | Heat shield for gas turbine engine frame |
DE4115403A1 (en) * | 1991-05-10 | 1992-11-12 | Mtu Muenchen Gmbh | NOZZLE WALL |
-
1993
- 1993-05-28 DE DE4317807A patent/DE4317807C1/en not_active Expired - Fee Related
-
1994
- 1994-05-11 GB GB9409420A patent/GB2278403B/en not_active Expired - Fee Related
- 1994-05-27 FR FR9406460A patent/FR2705736A1/en not_active Withdrawn
Also Published As
Publication number | Publication date |
---|---|
GB2278403A (en) | 1994-11-30 |
FR2705736A1 (en) | 1994-12-02 |
GB2278403B (en) | 1996-09-25 |
DE4317807C1 (en) | 1994-08-04 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PCNP | Patent ceased through non-payment of renewal fee |
Effective date: 19980511 |