Turboprop-powered aircraft with thermal system

• US 9,422,060 B2
• Filed: 01/06/2012
• Issued: 08/23/2016
• Est. Priority Date: 01/11/2011
• Status: Expired due to Fees

• Current Assignee: BAE Systems Plc
• Original Assignee: BAE Systems Plc
• Inventors: Smith, Stephen John Richard, Watt, Kieran James
• Primary Examiner(s): Rivera, Carlos A
• Application Number:
  US13/979,065
• Publication Number:
  US 20130292085A1
• Time in Patent Office: 1,691 Days
• US Class Current: 1/1
• CPC Class Codes: B64D 13/00 Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space , or structural parts of the aircraft treatment rooms with artificial climate for medical purposes A61G10/02; respiratory apparatus in general A62B; for vehicles in general B60H
• CPC Class Codes: B64D 13/06 the air being conditioned pressurising B64D13/02
• CPC Class Codes: B64D 13/08 the air being heated or cooled
• CPC Class Codes: B64D 15/02 by ducted hot gas or liquid
• CPC Class Codes: B64D 2013/0614 with subsystems for cooling avionics
• CPC Class Codes: B64D 2013/0633 including chemical reaction-based thermal management systems
• CPC Class Codes: B64F 1/362 Installations for supplying conditioned air to parked aircraft
• CPC Class Codes: Y02T 50/50 On board measures aiming to increase energy efficiency

Abstract

A method and apparatus are disclosed for a turboprop-powered medium altitude long endurance (MALE) aircraft, having: a heat exchanger with a heat-storage material, for example a heat-storage wax; and an air recirculation path. The heat exchanger can be arranged to cool air recirculating around the air recirculation path which is arranged to provide cooling to the MALE aircraft, for example to an equipment bay. The heat-storage material may be cooled by ground-based cooling apparatus when the aircraft is on the ground and/or by ram air when the aircraft is in flight. The heat-storage material may have a melting point selected so as to be rendered solid during ground-based cooling and/or ram air cooling, and/or selected so as to undergo melting while cooling the air recirculating around the air recirculation path.

Claims

1. A turboprop-powered medium altitude long endurance aircraft, comprising:

a heat exchanger having an air flow channel interlaced with a heat-storage material;

an air inlet arranged to input external air from ground-based cooling air and/or a ram air scoop directly into the air flow channel so as to cool the heat-storage material; and

an air recirculation path including the air flow channel;

wherein

the heat exchanger is configured to cool recirculating air flowing through the air flow channel; and

the air recirculation path is arranged to allow the recirculating air to provide cooling from the air flow channel to the turboprop-powered medium altitude long endurance aircraft.

2. A turboprop-powered medium altitude long endurance aircraft according to claim 1, wherein the air inlet is configured to provide an input for ground-based cooling apparatus such that the heat-storage material will be cooled by the ground-based cooling apparatus when the aircraft is on the ground.

3. A turboprop-powered medium altitude long endurance aircraft according to claim 1, wherein the air inlet is configured to provide ram air scoop functionality such that the heat-storage material will be cooled by ram air during aircraft flight.

4. A turboprop-powered medium altitude long endurance aircraft according to claim 2, wherein the heat-storage material has a melting point selected so as to be rendered solid when cooling is to be performed by the ground-based cooling apparatus when the aircraft is on the ground and/or by ram air during aircraft flight.

5. A turboprop-powered medium altitude long endurance aircraft according to claim 3, wherein the heat-storage material has a melting point selected so as to be rendered solid when cooling is to be performed by a ground-based cooling apparatus when the aircraft is on the ground and/or by the ram air during aircraft flight.

6. A turboprop-powered medium altitude long endurance aircraft according to claim 1, wherein the heat-storage material has a melting point selected so as to undergo melting to assist heat capturing characteristics of the heat storage material when cooling air is recirculating around the air recirculation path.

7. A turboprop-powered medium altitude long endurance aircraft according to claim 1, wherein the air recirculation path is arranged to provide cooling to an aircraft equipment bay.

8. A turboprop-powered medium altitude long endurance aircraft according to claim 1, wherein the heat exchanger comprises:

a heat sink;

wherein

the heat sink is thermally coupled to the air flow channel and configured such that in operation heat will be extracted from air flowing along the air flow channel and the extracted heat will be stored in the heat sink; and

the heat sink includes the heat-storage material, the heat-storage material having a melting point selected relative to a temperature of air intended to be cooled such that the heat-storage material will be initially solid and then will melt or start to melt while extracting and storing heat from air flowing along the air flow channel.

9. A turboprop-powered medium altitude long endurance aircraft according to claim 1, wherein the heat-storage material is a heat-storage wax.

10. A turboprop-powered medium altitude long endurance aircraft according to claim 9, wherein the heat-storage wax is paraffin wax.

11. A method of thermally managing a turboprop-powered medium altitude long endurance aircraft, the method comprising:

providing a heat exchanger having an air flow channel interlaced with a heat-storage material;

using external air input from ground-based cooling air and/or a ram air scoop directly into the heat exchanger from an air inlet via the air flow channel to cool the heat-storage material; and

cooling, after using the external air input from ground-based air and/or the ram air scoop to cool the heat-storage material of the heat exchanger, the turboprop-powered medium altitude long endurance aircraft with recirculated air passed via the air flow channel.

12. A method according to claim 11, comprising:

cooling, with ground-based cooling air input into the heat exchanger from the air inlet, the heat-storage material of the heat exchanger prior to using the recirculated air passed via the heat exchanger to cool the turboprop-powered medium altitude long endurance aircraft.

13. A method according to claim 11, comprising:

cooling, with ram air input into the heat exchanger from the air inlet, the heat-storage material of the heat exchanger after using the recirculated air passed via the heat exchanger to cool the turboprop-powered medium altitude long endurance aircraft.

14. A method according to claim 13, comprising:

cooling, after using ram air to cool the heat-storage material of the heat exchanger, the turboprop-powered medium altitude long endurance aircraft with recirculated air passed via the heat exchanger.

15. A method according to claim 11, comprising:

performing heating of the turboprop-powered medium altitude long endurance aircraft with heat scavenged from an engine of the aircraft.

16. A method according to claim 11, comprising:

cooling, after using ground-based air to cool the heat-storage material of the heat exchanger, the turboprop-powered medium altitude long endurance aircraft with recirculated air passed via the heat exchanger.

17. A method according to claim 11, comprising:

cooling, with ground-based cooling air input into the heat exchanger from the air inlet, the heat-storage material of the heat exchanger prior to using the recirculated air passed via the heat exchanger to cool the turboprop-powered medium altitude long endurance aircraft;

cooling, after using ground-based air to cool the heat-storage material of the heat exchanger, the turboprop-powered medium altitude long endurance aircraft with recirculated air passed via the heat exchanger;

cooling, with ram air input into the heat exchanger from the air inlet, the heat-storage material of the heat exchanger after using the recirculated air passed via the heat exchanger to cool the turboprop-powered medium altitude long endurance aircraft;

cooling, after using the ram air to cool the heat-storage material of the heat exchanger, the turboprop-powered medium altitude long endurance aircraft with recirculated air passed via the heat exchanger.

18. A method according to claim 11, comprising:

in a first stage, while stationary on the ground, cooling, with ground-based cooling air input into the heat exchanger from the air inlet, the heat-storage material of the heat exchanger prior to using the recirculated air passed via the heat exchanger to cool the turboprop-powered medium altitude long endurance aircraft;

in a second stage following disconnection from the ground-based cooling, cooling, after using ground-based air to cool the heat-storage material of the heat exchanger, the turboprop-powered medium altitude long endurance aircraft with recirculated air passed via the heat exchanger;

in a third stage while flying in ambient air, cooling, with ram air input into the heat exchanger from the air inlet, the heat-storage material of the heat exchanger after using the recirculated air passed via the heat exchanger to cool the turboprop-powered medium altitude long endurance aircraft;

after landing, cooling, after using the ram air to cool the heat-storage material of the heat exchanger, the turboprop-powered medium altitude long endurance aircraft with recirculated air passed via the heat exchanger.

19. A method according to claim 11, wherein said turboprop-powered medium altitude long endurance aircraft does not include active air conditioning.

20. A system for thermally managing a turboprop-powered medium altitude long endurance aircraft, the system comprising:

a heat exchanger;

a heat-storage material;

an air inlet;

an air flow channel;

an air recirculation path;

external air from ground-based cooling air and a ram air scoop;

wherein the air flow channel is interlaced with the heat-storage material;

wherein the air inlet is arranged to input the external air into the heat exchanger so as to cool the heat-storage material within the heat exchanger;

wherein the heat exchanger is configured to cool recirculating air around the air recirculation path;

wherein the air recirculation path is arranged to allow the recirculating air to provide aircraft cooling air; and

a thermal control system configured to

provide cooling of the heat-storage material in the heat exchanger using the external air from the air inlet into the air flow channel; and

after the cooling of the heat-storage material, provide cooling, with the recirculated air cooled via the air flow channel, the turboprop-powered medium altitude long endurance aircraft.