GB1083573A - Air conditioning apparatus for aircraft - Google Patents
Air conditioning apparatus for aircraftInfo
- Publication number
- GB1083573A GB1083573A GB979363A GB979363A GB1083573A GB 1083573 A GB1083573 A GB 1083573A GB 979363 A GB979363 A GB 979363A GB 979363 A GB979363 A GB 979363A GB 1083573 A GB1083573 A GB 1083573A
- Authority
- GB
- United Kingdom
- Prior art keywords
- valve
- pressure
- spring
- solenoid
- opened
- 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
- 238000004378 air conditioning Methods 0.000 title abstract 2
- 230000001143 conditioned effect Effects 0.000 abstract 3
- 230000006835 compression Effects 0.000 abstract 1
- 238000007906 compression Methods 0.000 abstract 1
- 238000011144 upstream manufacturing 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
- B64D13/06—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space the air being conditioned
-
- 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
- B64D13/06—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space the air being conditioned
- B64D2013/0603—Environmental Control Systems
- B64D2013/0688—Environmental Control Systems with means for recirculating cabin air
Landscapes
- Health & Medical Sciences (AREA)
- General Health & Medical Sciences (AREA)
- Pulmonology (AREA)
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Fluid-Driven Valves (AREA)
- Reciprocating Pumps (AREA)
Abstract
1,083,573. Fluid-pressure servomotor systems. BRISTOL SIDDELEY ENGINES Ltd. March 11, 1964 [March 12, 1963; June 20, 1963], Nos. 9793/63 and 24625/63. Heading G3P. [Also in Divisions B1 and F4] An air flow shut off and control valve assembly in the air conditioning system of an aircraft (see Division F4) comprises a shut off valve and a control valve in series in a casing 24 through which pressurized fresh air passes from the left as seen in Fig. 4. A shut off valve member 65 is connected to a piston 66 biased towards the open position by a spring 67 and towards the closed position by the connection of a chamber 68 through openings 69 and 70 with the pressurized air stream. The chamber 71 on the other side of the piston communicates through an opening 72 with the chamber 68. The valve is then open unless a relief passage 73 leading from the chamber 71 is opened by either of valves 73A or 73B (Fig. 5). The valve 73A is opened by energization of a solenoid 73C. The valve 73B is connected to a member 95 forming one end of a bellows diaphragm 96 acted on by a spring 100 and by the pressure in two chambers 98 and 99. The chambers are connected by passages 101 and 102 with the fresh air supply upstream of the shut off valve so that normally the valve 73B is maintained closed by the spring 100. Pressure may be relieved in the passage 101 to open the valve 73B by either of two valves 104 and 105. The valve 104 is opened by an excess temperature device in the conditioned air supply line to the aircraft cabin and the valve 105 is opened by a bellows 41 if the pressure in the conditioned air line exceeds a given value. The member 95 has a stem 106 sliding in a guide 107 provided with apertures locating latching balls 108 which cooperate with a notch 109 in the stem to hold valve 73B open when it has been opened. When the balls enter the notch they release a sleeve 109A which moves under the action of a spring 110 to lock the balls in the notch. To reset the valve 73B a solenoid 111 is energized to move the sleeve back to its original position and to simultaneously operate a valve 113 to relieve pressure in the chamber 99. The control valve of the assembly is controlled from a Venturi 32 in the conditioned air line and comprises a sleeve valve 73a having a piston working in a cylinder 76. Connections 36A and 36B with the Venturi are connected to either side of a diaphragm 89 connected to a relief valve 88 to control the pressure in a bellows 82A thus varying the compression of a spring 83 and the pressure at which a relief valve 81 opens. The datum pressure may be changed by energizing a solenoid 92 to compress a spring 91 acting on the diaphragm 89. Alternatively the arrangement may be such that de-energization of the solenoid produces the higher datum pressure. The solenoid 92 may be arranged to operate if the fresh air flow rate falls below a given value.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB979363A GB1083573A (en) | 1963-03-12 | 1963-03-12 | Air conditioning apparatus for aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB979363A GB1083573A (en) | 1963-03-12 | 1963-03-12 | Air conditioning apparatus for aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1083573A true GB1083573A (en) | 1967-09-13 |
Family
ID=9878875
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB979363A Expired GB1083573A (en) | 1963-03-12 | 1963-03-12 | Air conditioning apparatus for aircraft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB1083573A (en) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2004037642A2 (en) * | 2002-10-07 | 2004-05-06 | Honeywell International Inc. | Method of heating for an aircraft electric environmental control system |
DE102005037285A1 (en) * | 2005-08-08 | 2007-02-15 | Liebherr-Aerospace Lindenberg Gmbh | Method for operating an aircraft air conditioning system |
WO2007115811A1 (en) * | 2006-04-07 | 2007-10-18 | Airbus Deutschland Gmbh | Air-conditioning system for aircraft |
JP2009511338A (en) * | 2005-10-17 | 2009-03-19 | エアバス・ドイチュラント・ゲーエムベーハー | Extraction supply system and method for supplying extraction to an aircraft |
EP3095703A1 (en) * | 2015-05-11 | 2016-11-23 | United Technologies Corporation | Environmental cooling systems for aircraft |
-
1963
- 1963-03-12 GB GB979363A patent/GB1083573A/en not_active Expired
Cited By (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2004037642A2 (en) * | 2002-10-07 | 2004-05-06 | Honeywell International Inc. | Method of heating for an aircraft electric environmental control system |
WO2004037642A3 (en) * | 2002-10-07 | 2004-05-27 | Honeywell Int Inc | Method of heating for an aircraft electric environmental control system |
DE102005037285A1 (en) * | 2005-08-08 | 2007-02-15 | Liebherr-Aerospace Lindenberg Gmbh | Method for operating an aircraft air conditioning system |
US7797962B2 (en) | 2005-08-08 | 2010-09-21 | Liebherr-Aerospace Lindenberg Gmbh | Method of operating an aircraft system |
JP2009511338A (en) * | 2005-10-17 | 2009-03-19 | エアバス・ドイチュラント・ゲーエムベーハー | Extraction supply system and method for supplying extraction to an aircraft |
WO2007115811A1 (en) * | 2006-04-07 | 2007-10-18 | Airbus Deutschland Gmbh | Air-conditioning system for aircraft |
JP2009532261A (en) * | 2006-04-07 | 2009-09-10 | エアバス ドイチェランド ゲゼルシャフト ミット ベシュレンクテル ハフツング | Air conditioning system for aircraft |
US8087255B2 (en) | 2006-04-07 | 2012-01-03 | Airbus Deutschland Gmbh | Air-conditioning system for aircraft |
CN101415606B (en) * | 2006-04-07 | 2013-06-19 | 空中客车德国运营有限责任公司 | Air-conditioning system for aircraft |
EP3095703A1 (en) * | 2015-05-11 | 2016-11-23 | United Technologies Corporation | Environmental cooling systems for aircraft |
US10494106B2 (en) | 2015-05-11 | 2019-12-03 | United Technologies Corporation | Environmental cooling systems for aircraft |
US10669031B2 (en) | 2015-05-11 | 2020-06-02 | Raytheon Technologies Corporation | Environmental cooling systems for aircraft |
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