GB1094913A - Improvements in or relating to turbojet engines for vertical take-off and landing aircraft - Google Patents
Improvements in or relating to turbojet engines for vertical take-off and landing aircraftInfo
- Publication number
- GB1094913A GB1094913A GB1585265A GB1585265A GB1094913A GB 1094913 A GB1094913 A GB 1094913A GB 1585265 A GB1585265 A GB 1585265A GB 1585265 A GB1585265 A GB 1585265A GB 1094913 A GB1094913 A GB 1094913A
- Authority
- GB
- United Kingdom
- Prior art keywords
- nozzles
- engine
- relating
- vertical take
- axis
- 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
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
- F02K1/002—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto with means to modify the direction of thrust vector
- F02K1/004—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto with means to modify the direction of thrust vector by using one or more swivable nozzles rotating about their own axis
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Control Of Turbines (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Transmission Devices (AREA)
- Toys (AREA)
Abstract
1,094,913. Jet propelled aircraft. M.A.N. TURBO G.m.b.H. April 13, 1965 [April 16, 1964], No. 15852/65. Heading B7G. A by-pass gas turbine engine has two propelling nozzles 7 rotatable about a common transverse axis, each comprising an elbow bend and an arcuate portion downstream of the bend so that the thrust vectors pass forwardly of the said axis when the engine, disposed with its axis horizontal, is producing direct lift. The nozzles are rotated, either independently or together, by jacks acting on the peripheries of the rotatable nozzles at their mounting, or on a shaft 9 on which they are mounted. The nozzles may be mounted on the engine, or on a nacelle or fuselage containing the engine. The shaft 9 has guide vanes 15 fixed to it.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DEM60671A DE1219804B (en) | 1964-04-16 | 1964-04-16 | Turbine jet engine for aircraft taking off and landing vertically |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1094913A true GB1094913A (en) | 1967-12-13 |
Family
ID=7309903
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1585265A Expired GB1094913A (en) | 1964-04-16 | 1965-04-13 | Improvements in or relating to turbojet engines for vertical take-off and landing aircraft |
Country Status (2)
Country | Link |
---|---|
DE (1) | DE1219804B (en) |
GB (1) | GB1094913A (en) |
-
1964
- 1964-04-16 DE DEM60671A patent/DE1219804B/en active Pending
-
1965
- 1965-04-13 GB GB1585265A patent/GB1094913A/en not_active Expired
Also Published As
Publication number | Publication date |
---|---|
DE1219804B (en) | 1966-06-23 |
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