GB688011A - Control arrangement for jet-propulsion - Google Patents
Control arrangement for jet-propulsionInfo
- Publication number
- GB688011A GB688011A GB15282/51A GB1528251A GB688011A GB 688011 A GB688011 A GB 688011A GB 15282/51 A GB15282/51 A GB 15282/51A GB 1528251 A GB1528251 A GB 1528251A GB 688011 A GB688011 A GB 688011A
- Authority
- GB
- United Kingdom
- Prior art keywords
- jet pipe
- axis
- jet
- rudder
- axially
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C15/00—Attitude, flight direction, or altitude control by jet reaction
- B64C15/02—Attitude, flight direction, or altitude control by jet reaction the jets being propulsion jets
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Excavating Of Shafts Or Tunnels (AREA)
- Gas Burners (AREA)
Abstract
688,011. Self-propelled missiles. WENGER, A. June 27, 1951 [June 28, 19501, No. 15282/51. Class 9(ii) [Also in Group XXXIII] A control arrangement for jet propulsion is characterized by a rudder located partially behind the outlet opening of the jet pipe and surrounding the latter over a part of its circumference, means being provided for adjusting the rudder around the longitudinal axis of the jet pipe and for adjusting it axially so that the portion of the rudder located behind said opening varies in length. The extremity of the jet pipe 2, Fig. 2, is fitted with a sleeve 3 formed with a part cylindrical extension 4 and is capable of rotary and longitudinal movement with respect to the axis of the jet pipe. Two annular grooves are formed on the outer surface of the member 3 one of which accommodates a peg 6 attached to an axially movable rod 7 and the other of which carries a gear ring 8 meshing with a pinion 9 driven by a shaft 11 formed with an axially slidable connection 10. In an alternative arrangement of the member 3, 4, Fig. 3 (not shown), it is mounted in such a manner that fore and aft movement of the sleeve 3 causes pivotal movement of the part 4 which is pivoted about a transverse axis arranged normal to the axis of the jet pipe.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CH688011X | 1950-06-28 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB688011A true GB688011A (en) | 1953-02-25 |
Family
ID=4529023
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB15282/51A Expired GB688011A (en) | 1950-06-28 | 1951-06-27 | Control arrangement for jet-propulsion |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB688011A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3162011A (en) * | 1961-09-14 | 1964-12-22 | Rolls Royce | Deflecting jet discharge nozzles for jet propulsion engines |
US3451624A (en) * | 1966-07-23 | 1969-06-24 | Entwicklungsring Sued Gmbh | Apparatus for directing fluid flow |
GB2188886A (en) * | 1986-04-14 | 1987-10-14 | Rolls Royce Plc | Thrust deflector for jet nozzles |
-
1951
- 1951-06-27 GB GB15282/51A patent/GB688011A/en not_active Expired
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3162011A (en) * | 1961-09-14 | 1964-12-22 | Rolls Royce | Deflecting jet discharge nozzles for jet propulsion engines |
US3451624A (en) * | 1966-07-23 | 1969-06-24 | Entwicklungsring Sued Gmbh | Apparatus for directing fluid flow |
GB2188886A (en) * | 1986-04-14 | 1987-10-14 | Rolls Royce Plc | Thrust deflector for jet nozzles |
GB2188886B (en) * | 1986-04-14 | 1990-01-31 | Rolls Royce Plc | Thrust deflectors for turbomachine propulsion nozzles |
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