AIRCRAFT GALLEY INSERT WITH PATHOGENS DIAGNOSTIC TEST CAPABILITIES
20220152614 · 2022-05-19
Assignee
Inventors
Cpc classification
G16B40/00
PHYSICS
B01L2200/18
PERFORMING OPERATIONS; TRANSPORTING
G16B10/00
PHYSICS
B01L7/52
PERFORMING OPERATIONS; TRANSPORTING
G01N1/2226
PHYSICS
B64D2013/0603
PERFORMING OPERATIONS; TRANSPORTING
B64D11/00
PERFORMING OPERATIONS; TRANSPORTING
B01L2200/10
PERFORMING OPERATIONS; TRANSPORTING
B01L3/505
PERFORMING OPERATIONS; TRANSPORTING
B01L3/021
PERFORMING OPERATIONS; TRANSPORTING
B64D13/08
PERFORMING OPERATIONS; TRANSPORTING
C12Q1/04
CHEMISTRY; METALLURGY
B01L2300/18
PERFORMING OPERATIONS; TRANSPORTING
H04L67/12
ELECTRICITY
B01L2300/023
PERFORMING OPERATIONS; TRANSPORTING
International classification
B01L7/00
PERFORMING OPERATIONS; TRANSPORTING
Abstract
A modular aircraft galley insert for performing thermal cycling for PCR testing includes a housing having a sample module for receiving a sample to be tested, a thermal module thermally connected to the sample module for cycling temperatures of the sample to be tested, a power module for providing power to the thermal module, a detector module configured to analyze the sample and connected to receive power from the power module, and a connectivity module for communicating results of a test from the detector module to a remote location with respect to the housing.
Claims
1. A modular aircraft galley insert for performing thermal cycling for PCR testing comprising: a housing having: a sample module for receiving a sample to be tested; a thermal module thermally connected to the sample module for cycling temperatures of the sample to be tested; a power module for providing power to the thermal module; a detector module configured to analyze the sample and connected to receive power from the power module; and a connectivity module for communicating results of a test from the detector module to a remote location with respect to the housing.
2. The insert of claim 1, further comprising a first storage space storing for consumables and process waste materials within the housing.
3. The inset of claim 1, further comprising a second storage space for storing the tested sample.
4. The insert of claim 1, further comprising a loading module for sample automatic loading and configured to transfer a portion of a test sample through a pipette tip for testing purposes.
5. The insert of claim 4, wherein the loading module further comprises a pump.
6. The insert of claim 4, wherein the loading module further comprises a pipette.
7. The inset of claim 1, wherein the power rating of the insert is approximately 1000 W.
8. The insert of claim 1, wherein further comprising a plurality of testing vessels configured to receive an individual sample within the housing.
9. The insert of claim 1, wherein the insert is configured to operate independently of the cabin pressure ranges or other environmental conditions in the aircraft.
10. The insert of claim 1, wherein the insert is inserted within a galley monument for a cabin area of an aircraft, where the monument includes: a first monument stack; a second monument stack adjacent to the first monument stack; and a tray within the second monument stack to secure the insert.
11. The insert of claim 1, wherein the connectivity module is connected to a cockpit of an aircraft.
12. The insert of claim 1, wherein the connectivity module is connected to an on on-ground-receiver.
13. The inset of claim 1, wherein the power module is connected to an aircraft power source.
14. The insert of claim 1, wherein the insert is integrated within a monument stack.
15. The insert of claim 1, wherein the insert is removably attached to a monument stack.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0011] So that those skilled in the art to which the subject disclosure appertains will readily understand how to make and use the devices and methods of the subject disclosure without undue experimentation, embodiments thereof will be described in detail herein below with reference to certain figures, wherein:
[0012]
[0013]
DETAILED DESCRIPTION
[0014] Reference will now be made to the drawings wherein like reference numerals identify similar structural features or aspects of the subject disclosure. For purposes of explanation and illustration, and not limitation, a partial view of an exemplary embodiment of a system in accordance with the disclosure is shown in
[0015]
[0016] The power rating of the insert 100 is about 1000 W. A volume of the insert is sized to fit within a galley ARINC size between 4 and 6. The insert can operate independently of the cabin pressure ranges or other environmental conditions in the aircraft.
[0017] Referring to
[0018] The reagents that are present within the insert 102, being ready to use, are mixed, and stable at room temperatures. Reagents will be pathogen-specific, that is, a determined set of reagents for each specific pathogen to be detected. Protocols for running programs are programed in the unit for PCR cycling: a few examples are the setup Temperatures of the specific thermal cycle, timing or number of cycles; in the case of the thermal module.
[0019] The methods and systems of the present disclosure, as described above and shown in the drawings, provide for an improved bulk data and analysis of passenger pathogens on an aircraft. The system provides a more efficient primary health controls at airports, helps identify at early stages emerging pathogens and origin of outbreaks, and empower their scientific research (either academic and/or commercial / institutional).While the apparatus and methods of the subject disclosure have been shown and described with reference to preferred embodiments, those skilled in the art will readily appreciate that changes and/or modifications may be made thereto without departing from the scope of the subject disclosure.