GB475525A - Improvements in or connected with cowling flaps for aircraft engines - Google Patents
Improvements in or connected with cowling flaps for aircraft enginesInfo
- Publication number
- GB475525A GB475525A GB14512/36A GB1451236A GB475525A GB 475525 A GB475525 A GB 475525A GB 14512/36 A GB14512/36 A GB 14512/36A GB 1451236 A GB1451236 A GB 1451236A GB 475525 A GB475525 A GB 475525A
- Authority
- GB
- United Kingdom
- Prior art keywords
- cowling
- pipe
- flaps
- ram
- fluid
- 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
- 239000012530 fluid Substances 0.000 abstract 4
- 238000001816 cooling Methods 0.000 abstract 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
- B64D33/08—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of power plant cooling systems
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Temperature-Responsive Valves (AREA)
Abstract
475,525. Cooling cylinders. DODSON, E. May 22, 1936, No. 14512. [Class 7 (ii)] [Also in Group XXXIII] A cowling for aircraft engines includes one or more flaps angularly adjustable thereon and which are constructed so that, when open, their leading edges fit closely on the cowling and, when closed, they form a smooth continuation of the cowling. As shown, the flaps b are pivotally mounted on tubes b<4> mounted in bearings c carried by brackets c<1> c<2> attached to a ring c<3> fixed within the main portion of the cowling a. Each bracket c<1> carries a hydraulic ram d containing a plunger d<1> formed with shoulders d<2> which engage with arms b<5>, b<6> on the adjacent ends of tubes b<4>. The ram d<1> is operated in either direction by the supply of fluid to either of parts d3, d<4>. To prevent loss of fluid due to leakage, passages d<8>, d<9> are connected by a passage d<10> which communicates with a pipe dll which connects all such pipes d<10> and is connected to the exhaust side of the fluid pressure system. Fluid is led to or exhausted from the ram through pipes d<12>, d<13> communicating through a valve e<4> with a supply pipe f and an exhaust pipe f<1>. The valve e<4> is conical and has passages and grooves provided therein such that when either pipe d<12>, d<13> is connected to supply the other pipe is connected to exhaust. The ram moves between adjustable abutments d<6>, d<7>. The flaps are provided with lateral extensions which are formed to act as stops. The valve e<4> may be controlled by hand or by a remote acting, thermostat which includes bellows g<2> connected to a boiler h fitted to the engine, and constructed as described in Specification 449,078. The thermostat actuates the valves through a trip mechanism of the kind described in Specification 341,759, [Group XXVIII]. Changes in atmospheric pressure are compensated for by an aneroid element h<5> connected with the bellows through a lever h<6>. A hand control may be provided to override the manual control.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB14512/36A GB475525A (en) | 1936-05-22 | 1936-05-22 | Improvements in or connected with cowling flaps for aircraft engines |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB14512/36A GB475525A (en) | 1936-05-22 | 1936-05-22 | Improvements in or connected with cowling flaps for aircraft engines |
Publications (1)
Publication Number | Publication Date |
---|---|
GB475525A true GB475525A (en) | 1937-11-22 |
Family
ID=10042537
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB14512/36A Expired GB475525A (en) | 1936-05-22 | 1936-05-22 | Improvements in or connected with cowling flaps for aircraft engines |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB475525A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5681861A (en) * | 1991-02-08 | 1997-10-28 | Cambridge Neuroscience, Inc. | Aminoguanidines and methods of use of same |
-
1936
- 1936-05-22 GB GB14512/36A patent/GB475525A/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5681861A (en) * | 1991-02-08 | 1997-10-28 | Cambridge Neuroscience, Inc. | Aminoguanidines and methods of use of same |
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