Disposable heat transfer device and system integrating such a device
US-2017367527-A1 · Dec 28, 2017 · US
Multi-phase circuit flow-through heater for aerospace beverage maker
US2016000262A1 · US · A1
| Field | Value |
|---|---|
| Publication number | US-2016000262-A1 |
| Application number | US-201514754641-A |
| Country | US |
| Kind code | A1 |
| Filing date | Jun 29, 2015 |
| Priority date | Jul 3, 2014 |
| Publication date | Jan 7, 2016 |
| Grant date | — |
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- Title
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- Abstract
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Abstract
Official abstract text for this publication.
A water heater for an aircraft beverage brewing apparatus includes a three way electrical conduit for conducting electrical power in three separate phases. The heater has a housing with a fluid inlet port at a first removable end piece and a fluid outlet port at a second removable end piece. The hollow cylindrical core incorporates a heating element wound around the core, and the housing includes three resettable temperature sensors at the outlet, each of the three resettable temperature sensors connected to a separate phase of power from the three way electrical conduit.
First claim
Opening claim text (preview).
I claim: 1 . A water heater for an aircraft beverage brewing apparatus, comprising: a three way electrical conduit for conducting electrical power in three separate phases; a housing coupled to the three way electrical conduit, the housing including a body, a first removable end piece, and a second removable end piece; a fluid inlet port at the first removable end piece and a fluid outlet port at the second removable end piece; a hollow cylindrical core disposed in the housing between the first and second removable end pieces, the hollow cylindrical core including a heating element wound around the core from a first end to a second end; and first, second, and third resettable temperature sensors disposed on the second removable end piece, each of the first, second, and third resettable temperature sensors connected to a separate phase of power from the three way electrical conduit. 2 . The water heater of claim 1 , wherein the hollow cylindrical core is plastic. 3 . The water heater of claim 1 , wherein the first and second removable end pieces include a threaded stem that engages a tapped hole at the respective end of the core. 4 . The water heater of claim 1 , wherein each phase in the three-phase power has a maximum 805 Watts. 5 . The water heater of claim 4 , where the operating temperature of the heater is 195° F. 6 . The water heater of claim 1 , wherein each phase in the three-phase power has a maximum 533 Watts. 7 . The water heater of claim 6 , where the operating temperature of the heater is 300° F.
Assignees
Inventors
Classifications
using electric energy supply · CPC title
- A47J31/542Primary
Continuous-flow heaters · CPC title
- A47J31/545Primary
Control or safety devices · CPC title
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Frequently asked questions
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- What does patent US2016000262A1 cover?
- A water heater for an aircraft beverage brewing apparatus includes a three way electrical conduit for conducting electrical power in three separate phases. The heater has a housing with a fluid inlet port at a first removable end piece and a fluid outlet port at a second removable end piece. The hollow cylindrical core incorporates a heating element wound around the core, and the housing includ…
- Who is the assignee on this patent?
- Be Aerospace Inc
- What technology area does this patent fall under?
- Primary CPC classification A47J31/542. Mapped technology areas include Human Necessities.
- When was this patent published?
- Publication date Thu Jan 07 2016 00:00:00 GMT+0000 (Coordinated Universal Time) (A1). Legal status and post-grant events are not shown on this page.
- What related patents are in patentsdb?
- We list 8 related publications on this page (citations in our corpus or others sharing the same primary CPC).