System and method for automatically controlling cabin air temperature in an aircraft

• US 6,012,515 A
• Filed: 11/27/1996
• Issued: 01/11/2000
• Est. Priority Date: 11/27/1996
• Status: Expired due to Term

• Current Assignee: Sikorsky Aircraft Corporation (Martin Marietta Corporation)
• Original Assignee: Sikorsky Aircraft Corporation (Martin Marietta Corporation)
• Inventors: Georgeou, Hercules, Loschiavo, Michael D., Stubbendorff, P. Lars R.
• Primary Examiner(s): Ford, John K.
• Application Number:
  US08/757,540
• Time in Patent Office: 1,140 Days
• Field of Search: 165/257, 165/254, 165/42, 165/43, 165/291, 165/256, 236/1 C, 236/13
• US Class Current: 165/257
• CPC Class Codes: B64D 13/08 the air being heated or cooled

Abstract

A system and method for automatically controlling cabin air temperature T_CBN in an aircraft having a cabin and a mixed air delivery system. The mixed air delivery system provides a flow of mixed air having an actual mixed air temperature into the cabin. The mixed air delivery system comprises a hot bleed air sub-system for providing a flow of hot bleed air, a cool air sub-system for providing a flow of cool air, and an ambient air sub-system for providing a flow of ambient air. The method comprises the steps of defining a selected cabin air temperature T_CBN SEL, and then controlling the flow of hot bleed air, the flow of cool air, and the flow of ambient air such that the mixed air temperature is driven toward a target mixed air temperature defined as k(T_CBN SEL -T_CBN)+T_CBN SEL, wherein k is a gain factor.

Claims

1. A method for automatically controlling cabin air temperature in an aircraft having an ambient air inlet, an exhaust outlet, an auxiliary heater, a turbine engine providing a flow of hot bleed air, a bleed air shutoff valve, a regulator valve assembly for regulating said flow of hot bleed air, and an air conditioning sub-system for providing a flow of cool air, said air conditioning sub-system having a compressor, evaporator, and an evaporator fan having low, medium and high speeds, said method comprising the steps of:

(a) defining a selected cabin air temperature T_CBN SEL

(b) sensing an ambient air temperature;

(c) comparing said ambient air temperature with a first ambient air switch point temperature;

(d) ensuring that an air conditioning mode is initiated if said ambient air temperature is greater than said first ambient air switch point temperature, the air conditioning mode including the steps of

ensuring that said ambient air inlet is closed,

ensuring that said exhaust outlet is closed,

ensuring that said compressor is activated,

sensing a cabin air temperature T_CBN,

comparing said cabin air temperature with said selected cabin air temperature,

ensuring that a first cooling sub-mode is initiated if said cabin air temperature is less than said selected cabin air temperature, and

ensuring that a second cooling sub-mode is initiated if said cabin air temperature is equal to or greater than said selected cabin air temperature;

(e) ensuring that a heating mode is initiated if said ambient air temperature is equal to or less than said first ambient air switch point temperature; and

(f) returning to said ambient air temperature sensing step.

2. A method for automatically controlling cabin air temperature in an aircraft having an ambient air inlet, an exhaust outlet, an auxiliary heater, a turbine engine providing a flow of hot bleed air, a bleed air shutoff valve, a regulator valve assembly for regulating said flow of hot bleed air, and an air conditioning sub-system for providing a flow of cool air, said air conditioning sub-system having a compressor, evaporator, and an evaporator fan having low, medium and high speeds, said method comprising the steps of:

defining a selected cabin air temperature T_CBN SEL

sensing an ambient air temperature;

comparing said ambient air temperature with a first ambient air switch point temperature;

ensuring that an air conditioning mode is initiated if said ambient air temperature is greater than said first ambient air switch point temperature, the air conditioning mode including the steps of

ensuring that said ambient air inlet is closed,

ensuring that said exhaust outlet is closed,

ensuring that said compressor is activated,

sensing a cabin air temperature T_CBN,

comparing said cabin air temperature with said selected cabin air temperature,

ensuring that a first cooling sub-mode is initiated if said cabin air temperature is less than said selected cabin air temperature, and

ensuring that a second cooling sub-mode is initiated if said cabin air temperature is equal to or greater than said selected cabin air temperature;

ensuring that a heating mode is initiated if said ambient air temperature is equal to or less than said first ambient air switch point temperature; and

returning to said ambient air temperature sensing step

wherein said first cooling sub-mode comprises the steps of;

ensuring that said evaporator fan is set to said low speed, thereby providing for said flow of cool air from said air conditioning subsystem;

ensuring that said bleed air shutoff valve is open to provide said flow of hot bleed air;

mixing said flow of hot bleed air with said flow of cool air to produce a flow of mixed air having an actual mixed air temperature; and

regulating said flow of hot bleed air with said regulator valve assembly such that said actual mixed air temperature is driven toward a target mixed air temperature.

3. The method of claim 2, wherein said target mixed air temperature is defined as k(T_CBN SEL -T_CBN)+T_CBN SEL, wherein k is a gain factor.

4. The method of claim 3, wherein said gain factor equals three.

5. A method for automatically controlling cabin air temperature in an aircraft having an ambient air inlet, an exhaust outlet, an auxiliary heater, a turbine engine providing a flow of hot bleed air, a bleed air shutoff valve, a regulator valve assembly for regulating said flow of hot bleed air, and an air conditioning sub-system for providing a flow of cool air, said air conditioning sub-system having a compressor, evaporator, and an evaporator fan having low, medium and high speeds, said method comprising the steps of:

defining a selected cabin air temperature T_CBN SEL

sensing an ambient air temperature;

comparing said ambient air temperature with a first ambient air switch point temperature;

ensuring that an air conditioning mode is initiated if said ambient air temperature is greater than said first ambient air switch point temperature, the air conditioning mode including the steps of

ensuring that said ambient air inlet is closed,

ensuring that said exhaust outlet is closed,

ensuring that said compressor is activated,

sensing a cabin air temperature T_CBN,

comparing said cabin air temperature with said selected cabin air temperature,

ensuring that a first cooling sub-mode is initiated if said cabin air temperature is less than said selected cabin air temperature, and

ensuring that a second cooling sub-mode is initiated if said cabin air temperature is equal to or greater than said selected cabin air temperature;

ensuring that a heating mode is initiated if said ambient air temperature is equal to or less than said first ambient air switch point temperature; and

returning to said ambient air temperature sensing step

wherein said second cooling sub-mode comprises the steps of;

ensuring that said bleed air shutoff valve is closed;

comparing said cabin air temperature with an air conditioning switch point temperature;

ensuring that said evaporator fan is set to said high speed if said cabin air temperature is greater than said air conditioning switch point temperature; and

ensuring that said evaporator fan is set to said medium speed if said cabin air temperature is equal to or less than said air conditioning switch point temperature.

6. A method for automatically controlling cabin air temperature in an aircraft having an ambient air inlet, an exhaust outlet, an auxiliary heater, a turbine engine providing a flow of hot bleed air, a bleed air shutoff valve, a regulator valve assembly for regulating said flow of hot bleed air, and an air conditioning sub-system for providing a flow of cool air, said air conditioning sub-system having a compressor, evaporator, and an evaporator fan having low, medium and high speeds, said method comprising the steps of:

defining a selected cabin air temperature T_CBN SEL

sensing an ambient air temperature;

comparing said ambient air temperature with a first ambient air switch point temperature;

ensuring that an air conditioning mode is initiated if said ambient air temperature is greater than said first ambient air switch point temperature;

ensuring that a heating mode is initiated if said ambient air temperature is equal to or less than said first ambient air switch point temperature; and

returning to said ambient air temperature sensing step;

wherein said heating mode comprises the steps of

(a) ensuring that said compressor is inactivated;

(b) ensuring that said bleed air shutoff valve is open to provide said flow of hot bleed air;

(c) sensing a cabin air temperature T_CBN ;

(d) comparing said cabin air temperature with a first heating switch point temperature;

(e) ensuring that said evaporator fan is set to said low speed if said cabin air temperature is less than said first heating switch point temperature;

(f) ensuring that said evaporator fan is set to said high speed if said cabin air temperature is equal to or greater than said first heating switch point temperature;

(g) comparing said ambient air temperature with a second ambient air switch point temperature;

(h) ensuring that said ambient air inlet is closed and ensuring that said exhaust outlet is closed if said ambient air temperature is less than said second ambient air switch point temperature, wherein said evaporator fan provides a flow of recirculated air;

(i) ensuring that said ambient air inlet is open and ensuring that said exhaust outlet is open if said ambient air temperature is equal to or greater than said second ambient air switch point temperature, wherein said evaporator fan provides a flow of ambient air;

(j) mixing said flow of hot bleed air with said flow of recirculated air to produce a flow of mixed air having an actual mixed air temperature if said ambient air temperature is less than said second ambient air switch point temperature and alternatively, mixing said flow of hot bleed air with said flow of ambient air to produce a flow of mixed air having an actual mixed air temperature if said ambient air temperature is equal to or greater than said second ambient air switch point temperature;

(k) regulating said flow of hot bleed air with said regulator valve assembly such that said actual mixed air temperature is driven toward a target mixed air temperature;

(l) comparing said cabin air temperature with a second heating switch point temperature;

(m) ensuring that said auxiliary heater is activated if said cabin air temperature is less than said second heating switch point temperature; and

(n) ensuring that said auxiliary heater is not activated if said cabin air temperature is equal to or greater than said second heating switch point temperature.

7. The method of claim 6, wherein said target mixed air temperature is defined as k(T_CBN SEL -T_CBN)+T_CBN SEL, wherein k is a gain factor.

8. The method of claim 7, wherein said gain factor equals three.