GB1302180A - - Google Patents
Info
- Publication number
- GB1302180A GB1302180A GB1302180DA GB1302180A GB 1302180 A GB1302180 A GB 1302180A GB 1302180D A GB1302180D A GB 1302180DA GB 1302180 A GB1302180 A GB 1302180A
- Authority
- GB
- United Kingdom
- Prior art keywords
- plates
- link
- movement
- march
- flow area
- 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
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D17/00—Regulating or controlling by varying flow
- F01D17/10—Final actuators
- F01D17/12—Final actuators arranged in stator parts
- F01D17/14—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits
- F01D17/141—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of shiftable members or valves obturating part of the flow path
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Control Of Turbines (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Supercharger (AREA)
Abstract
1302180 Turbines ROTAX Ltd 18 March 1970 [31 March 1969] 16672/69 Heading FIT The effective flow area of the nozzle blades 10 of a turbine can be varied by radially movable shutter plates 13, 14 disposed upstream thereof. The plates 13, 14 include leg portions 15 mounted at 16 upon spaced pivots carried on a fixed member 17, the latter also pivotally supporting at 19 a cross link 18 having slotted ends 20 within which engage pins 21 mounted on the legs 15. An actuating member 22 engages via a curved link 23 with the pin 21 associated with plate 13 so that movement of member 22 causes angular movement of link 18 and thus radially inward or outward movement of plates 13, 14 to vary the flow area. (For Figures see next page)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1667269 | 1969-03-31 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1302180A true GB1302180A (en) | 1973-01-04 |
Family
ID=10081546
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1302180D Expired GB1302180A (en) | 1969-03-31 | 1969-03-31 |
Country Status (3)
Country | Link |
---|---|
DE (2) | DE7011554U (en) |
FR (1) | FR2040145A5 (en) |
GB (1) | GB1302180A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4497171A (en) * | 1981-12-22 | 1985-02-05 | The Garrett Corporation | Combustion turbine engine |
-
1969
- 1969-03-31 GB GB1302180D patent/GB1302180A/en not_active Expired
-
1970
- 1970-03-28 DE DE19707011554 patent/DE7011554U/en not_active Expired
- 1970-03-28 DE DE19702015057 patent/DE2015057A1/en active Pending
- 1970-03-31 FR FR7011395A patent/FR2040145A5/fr not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4497171A (en) * | 1981-12-22 | 1985-02-05 | The Garrett Corporation | Combustion turbine engine |
Also Published As
Publication number | Publication date |
---|---|
FR2040145A5 (en) | 1971-01-15 |
DE7011554U (en) | 1973-02-01 |
DE2015057A1 (en) | 1970-10-08 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PS | Patent sealed | ||
PLNP | Patent lapsed through nonpayment of renewal fees |