GB681144A - Mechanism and method for conditioning air for an enclosure - Google Patents
Mechanism and method for conditioning air for an enclosureInfo
- Publication number
- GB681144A GB681144A GB7784/48A GB778448A GB681144A GB 681144 A GB681144 A GB 681144A GB 7784/48 A GB7784/48 A GB 7784/48A GB 778448 A GB778448 A GB 778448A GB 681144 A GB681144 A GB 681144A
- Authority
- GB
- United Kingdom
- Prior art keywords
- air
- heat exchanger
- damper
- turbine
- coolant
- 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
- 230000003750 conditioning effect Effects 0.000 title 1
- 238000001816 cooling Methods 0.000 abstract 6
- 239000002826 coolant Substances 0.000 abstract 4
- 238000005192 partition Methods 0.000 abstract 1
- 238000009423 ventilation 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
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/50—On board measures aiming to increase energy efficiency
Landscapes
- Health & Medical Sciences (AREA)
- General Health & Medical Sciences (AREA)
- Pulmonology (AREA)
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Central Air Conditioning (AREA)
Abstract
681,144. Ventilation. GARRETT CORPORATION. March 15, 1948 [April 5, 1947], No. 7784/48. Class 137 [Also in Group XIII] In air-cooling apparatus in which air from a compressor 11 is cooled, before .delivery to an enclosure such as an aircraft cabin 10, in cooling means including a heat exchanger 12, part of the air leaving the cooling means is returned to the heat exchanger to act as a coolant, the amount of air so returned being controlled by a characteristic, e.g. the pressure, of the air which has passed through the cooling means. The cooling means includes a turbine 29 which is driven by, and so further cools, the cooled air leaving the heat exchanger 12. In the form shown, a damper 36 in the passage 34, through which part of the cooled air leaving the turbine 29 returns to the heat exchanger, is controlled by a diaphragm 41 moving in response to changes in the difference between the pressure of the air in the aircraft cabin 10 to which the cooled air is supplied and the external atmospheric pressure. Coolant air from the external atmosphere is admitted to the heat exchanger through an inlet 19 controlled by a damper 47 which is opened and closed by changes in the temperature of the air in the chamber 10. The damper 47 is linked to a damper 45 which controls a passage 44 through which cooled air from the heat-exchanger can byepass the turbine 29. When the temperature in the chamber 10 is high, and the pressure difference from the external atmosphere is low, the valves 19, 36 are open and the valve 45 is closed, to produce maximum cooling. The turbine 29 drives a fan 31 in the outlet 22 for coolant air. A partition 35 may divide the coolant space in the heat exchanger into two parts. Specifications 654,622 and 604,301 are referred to.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US681144XA | 1947-04-05 | 1947-04-05 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB681144A true GB681144A (en) | 1952-10-22 |
Family
ID=22080494
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB7784/48A Expired GB681144A (en) | 1947-04-05 | 1948-03-15 | Mechanism and method for conditioning air for an enclosure |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB681144A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE1176677B (en) * | 1960-05-10 | 1964-08-27 | Dowty Rotol Ltd | Air conditioning for internal combustion engine powered vehicles |
| EP3193128A1 (en) * | 2016-01-15 | 2017-07-19 | Hamilton Sundstrand Corporation | Cold corner flow baffle |
| US10124452B2 (en) | 2013-08-09 | 2018-11-13 | Hamilton Sundstrand Corporation | Cold corner flow baffle |
-
1948
- 1948-03-15 GB GB7784/48A patent/GB681144A/en not_active Expired
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE1176677B (en) * | 1960-05-10 | 1964-08-27 | Dowty Rotol Ltd | Air conditioning for internal combustion engine powered vehicles |
| US10124452B2 (en) | 2013-08-09 | 2018-11-13 | Hamilton Sundstrand Corporation | Cold corner flow baffle |
| EP3193128A1 (en) * | 2016-01-15 | 2017-07-19 | Hamilton Sundstrand Corporation | Cold corner flow baffle |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| GB681144A (en) | Mechanism and method for conditioning air for an enclosure | |
| GB904252A (en) | Improvements relating to gas cooling systems | |
| GB773248A (en) | Improvements in and relating to systems for cooling of air for example for aircraft pressurised spaces | |
| GB795109A (en) | Improvements in or relating to a closed cycle refrigeration system | |
| GB721676A (en) | Air conditioning means for an enclosure | |
| GB654678A (en) | Enclosure air conditioning mechanism | |
| GB753120A (en) | Improvements in or relating to an aircraft air-conditioning system | |
| GB829727A (en) | High pressure ratio cooling system | |
| GB695781A (en) | Mechanism for conditioning air for enclosures | |
| GB688246A (en) | Cooling system for high speed aircraft | |
| GB621351A (en) | Gas turbine-driven auxiliary power and air conditioning system | |
| GB688191A (en) | Cooling system for high speed aircraft | |
| GB663817A (en) | Aircraft air conditioning system | |
| GB609823A (en) | Air temperature conditioning system | |
| GB621827A (en) | An air cooling unit more particularly intended for use in aircraft | |
| GB744557A (en) | Air conditioner | |
| GB646257A (en) | Improvements in or relating to air or like conditioning systems | |
| GB673698A (en) | Cooling system for compartments using expansion engine means | |
| GB820316A (en) | Apparatus for controlling the temperature of air within a compartment | |
| GB817975A (en) | An air conditioning system | |
| GB729626A (en) | Apparatus for conditioning gaseous fluids | |
| GB772022A (en) | Improvements in or relating to fluid conditioning or refrigeration systems | |
| GB574467A (en) | Improvements in and relating to cooling plants | |
| GB632678A (en) | Cabin cooling system for aircraft | |
| GB737393A (en) | Enclosure air supply system |