← Back to Patent Explorer
US4487034A Expired / Lapsed US ⏱️ 0.0 years remaining

Energy-efficient all-electric ECS for aircraft

Assignee: Lockheed Martin Corp
•
Filing: 1983-08-03
•
Granted: 1984-12-11
•
Expires: 2003-08-03
📄 Original PDF 🌐 Google Patents 🔄 Sync Now

Abstract

Abstract The invention is an energy-efficient all-electric environmental control system (70). The system includes a cabin compressor (16) and a Freon compressor (14), both of which are commonly driven by a two-speed electric motor (12). The motor (12) operates at low speed at low altitudes and on the ground to drive the Freon compressor (14). Freon fluid then cools the electric motor (12) and the cabin (18) and avionics (56) by means of the evaporator/dehumidifier systems (72) and (74), respectively. At high altitudes the electric motor (12) runs at high speed to drive the cabin compressor (16) to provide pressurization for the cabin (18). In this operation mode, the Freon compressor can be disconnected via an electromagnetic clutch (48). The ECS (70) also includes a liquid Freon pump (52) which can be utilized when the Freon compressor is disconnected or bypassed to circulate liquid Freon to cool the electric motor (12) and to circulate through the evaporators (38) and (76). The pump (52) is driven by an ac or dc motor (54).

Inventors

  • 👤 Michael J. Cronin
  • 👤 Gordon Seid

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-30 18:55
CPC Classifications
B; B64; B64D; B64D13/00; B64D13/06; F; F25; F25B; F25B27/00; F25B5/00; F25B5/02; B64D2013/0603; B64D2013/0614; B64D2013/0644; B64D2013/0688; Y; Y02; Y02T; Y02T50/00; Y02T50/40; Y02T50/50

Claims Analysis

Total Claims: 12
Claim 1
Independent Claim 102 words
In an aircraft environmental control system having an air cycle cooling system powered by an electrical motor and, an evaporative cooling sub-system coupled thereto, said cooling sub-system having a cooling circuit including fluid coolant, at least one coolant compressor coupled to said electric motor, and at least one coolant expansion means the improvement comprising: means to selectively disconnect said coolant compressor from said electric motor; said air cycle cooling system having means to bypass said at least one coolant expansion means and said at least one coolant compressor; and a liquid coolant pump for circulating said fluid coolant through said cooling circuit.
Claim 2
Dependent Claim 102 words
In an aircraft environmental control system having an air cycle cooling system powered by an electrical motor and, an evaporative cooling sub-system coupled thereto, said cooling sub-system having a cooling circuit including fluid coolant, at least one coolant compressor coupled to said electric motor, and at least one coolant expansion means the improvement comprising: means to selectively disconnect said coolant compressor from said electric motor; said air cycle cooling system having means to bypass said at least one coolant expansion means and said at least one coolant compressor; and a liquid coolant pump for circulating said fluid coolant through said cooling circuit.
Claim 3
Dependent Claim 21 words
An environmental control system as in claim 1 including an ac or dc motor adapted for driving said liquid coolant pump.
Claim 4
Dependent Claim 29 words
An environmental control system as in claim 1 wherein said ac or dc motor is adapted to be powered by ground support, aircraft primary and aircraft auxiliary power sources.
Claim 5
Dependent Claim 16 words
An environmental control system as in claim 3 wherein said clutch element comprises an electromagnetic clutch.
Claim 6
Dependent Claim 23 words
An environmental control system as in any one of claims 1 or 3 wherein said bypass means comprises at least one bypass valve.
Claim 7
Dependent Claim 21 words
An environmental control system as in claim 5 including an ac or dc motor adapted for driving said liquid coolant pump.
Claim 8
Dependent Claim 19 words
An environmental control system as in claim 5 wherein said first bypass means comprises at least one bypass valve.
Claim 9
Dependent Claim 94 words
In an aircraft environmental control system having an air cycle cooling system powered by an electric motor, an evaporative cooling sub-system coupled thereto, said cooling sub-system having a cooling circuit including fluid coolant, at least one coolant compressor coupled to said electric motor, and at least one coolant expansion means, the improvement comprising: said air cycle system having first means to bypass said at least one coolant compressor and second means to bypass said at least one coolant expansion means; and a liquid coolant pump for circulating said fluid coolant through said cooling circuit.
Claim 10
Dependent Claim 94 words
In an aircraft environmental control system having an air cycle cooling system powered by an electric motor, an evaporative cooling sub-system coupled thereto, said cooling sub-system having a cooling circuit including fluid coolant, at least one coolant compressor coupled to said electric motor, and at least one coolant expansion means, the improvement comprising: said air cycle system having first means to bypass said at least one coolant compressor and second means to bypass said at least one coolant expansion means; and a liquid coolant pump for circulating said fluid coolant through said cooling circuit.
Claim 11
Dependent Claim 29 words
An environmental control system as in claim 8 wherein said ac or dc motor is adapted to be powered by ground support, aircraft primary and aircraft auxiliary power sources.
Claim 12
Dependent Claim 24 words
An environmental control system as in any one of claims 5 or 9 wherein said second bypass means comprises at least one bypass valve.

References Cited (Backward Citations)

US2363273A Cited
US2452704A Cited
US2451280A Cited
US2585570A Cited
US2614815A Cited
US2678542A Cited
US2697917A Cited
US2892318A Cited
US3010289A Cited
US3464226A Cited
US3636723A Cited
US3646773A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1987-12-11 1988-06-11 1988-12-11 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1991-12-11 1992-06-11 1992-12-11 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1995-12-11 1996-06-11 1996-12-11 $7700.00 Window Closed / Lapsed

Assigned Categories & Tags

No categories assigned to this patent yet.

Assign Category Tag