GB464489A - Warming of aircraft cock pits - Google Patents
Warming of aircraft cock pitsInfo
- Publication number
- GB464489A GB464489A GB2939535A GB2939535A GB464489A GB 464489 A GB464489 A GB 464489A GB 2939535 A GB2939535 A GB 2939535A GB 2939535 A GB2939535 A GB 2939535A GB 464489 A GB464489 A GB 464489A
- Authority
- GB
- United Kingdom
- Prior art keywords
- aircraft
- air
- passes
- warmed
- engine
- 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
- 238000010792 warming Methods 0.000 title 1
- 238000001816 cooling Methods 0.000 abstract 1
- 238000010438 heat treatment Methods 0.000 abstract 1
- 230000004048 modification Effects 0.000 abstract 1
- 238000012986 modification 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
- B64D13/00—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft
- B64D13/06—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft the air being conditioned
- B64D13/08—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft the air being conditioned the air being heated or cooled
Landscapes
- Health & Medical Sciences (AREA)
- General Health & Medical Sciences (AREA)
- Pulmonology (AREA)
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Supercharger (AREA)
Abstract
464,489. Ventilating and heating aircraft. ELLOR, J. E. Oct. 24, 1935, Nos. 29395/35 and 12589/36. [Class 137] [Also in Group XIII] The cockpit of aircraft is heated and ventilated by admitting thereto, under control, part of the airstream which has been warmed by performing a cooling function for the aircraft engine. Air entering a tunnel D<2> passes through an intercooler D which is fitted between a supercharger D<1> and the cylinders of the engine A<1>. Part of the warmed air escapes through an outlet D<3>, and part passes through a pipe E, under control of a valve E to the cockpit. In Fig. 4, the air heated by the radiator C in a tunnel C<1> clings to the under surface of the fuselage, and passes through openings F<1> controlled by flap valves F<2>. Openings C in the top covering allow escape of the warmed air after use. In a modification, warmed air is taken from the cowl round a rotary engine.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB2939535A GB464489A (en) | 1935-10-24 | 1935-10-24 | Warming of aircraft cock pits |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB2939535A GB464489A (en) | 1935-10-24 | 1935-10-24 | Warming of aircraft cock pits |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB464489A true GB464489A (en) | 1937-04-19 |
Family
ID=10290890
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB2939535A Expired GB464489A (en) | 1935-10-24 | 1935-10-24 | Warming of aircraft cock pits |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB464489A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US9797297B2 (en) | 2015-02-20 | 2017-10-24 | Pratt & Whitney Canada Corp. | Compound engine assembly with common inlet |
| US9879591B2 (en) | 2015-02-20 | 2018-01-30 | Pratt & Whitney Canada Corp. | Engine intake assembly with selector valve |
| US9896998B2 (en) | 2015-02-20 | 2018-02-20 | Pratt & Whitney Canada Corp. | Compound engine assembly with modulated flow |
| US9932892B2 (en) | 2015-02-20 | 2018-04-03 | Pratt & Whitney Canada Corp. | Compound engine assembly with coaxial compressor and offset turbine section |
-
1935
- 1935-10-24 GB GB2939535A patent/GB464489A/en not_active Expired
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US9797297B2 (en) | 2015-02-20 | 2017-10-24 | Pratt & Whitney Canada Corp. | Compound engine assembly with common inlet |
| US9879591B2 (en) | 2015-02-20 | 2018-01-30 | Pratt & Whitney Canada Corp. | Engine intake assembly with selector valve |
| US9896998B2 (en) | 2015-02-20 | 2018-02-20 | Pratt & Whitney Canada Corp. | Compound engine assembly with modulated flow |
| US9932892B2 (en) | 2015-02-20 | 2018-04-03 | Pratt & Whitney Canada Corp. | Compound engine assembly with coaxial compressor and offset turbine section |
| US10533489B2 (en) | 2015-02-20 | 2020-01-14 | Pratt & Whitney Canada Corp. | Compound engine assembly with common inlet |
| US10533487B2 (en) | 2015-02-20 | 2020-01-14 | Pratt & Whitney Canada Corp. | Engine intake assembly with selector valve |
| US10883414B2 (en) | 2015-02-20 | 2021-01-05 | Pratt & Whitney Canada Corp. | Engine intake assembly with selector valve |
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