IP Library Granted Patent US 10,259,597
Granted Patent B1
US 10,259,597 · App. 15/597,545 · Granted Apr 16, 2019

Aircraft fuel system test unit

Inventors: Paul Spinazze (Toledo, OH); Sherry Drake (Toledo, OH)
Assignee: Tronair, Inc.
B64F5/45B64F5/60G01M3/025
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Quick Facts
Patent No.
US 10,259,597
App. No.
15/597,545
Granted
Apr 16, 2019
Kind
B1
Abstract

This aircraft maintenance equipment is a fuel system leak test unit, designed to insure installation integrity of fuel system lines and hoses and to ensure that the system is free from any debris generated during the assembly and maintenance process for an aircraft. The unit is designed to check for leaks using vacuum or pressure while monitoring for fuel leaks or bubbles through a clear tube section.

Claims (14)

1. A portable aircraft fuel system test apparatus comprising:

a cart ( 10 ) having a mounting surface ( 12 ); and

a fuel system leak testing unit ( 14 ) mounted on the mounting surface wherein the fuel system leak testing unit ( 14 ) comprises a fuel particle filter ( 16 ), lines and hoses ( 18 ) and wherein the testing unit ( 14 ) further comprises;

an engine fuel line interface;

a discharge lie, and a suction line comprising a clear line section;

wherein the clear line section is located between the engine fuel line interface and the discharge line;

wherein the clear line section is configured for monitoring for the presence of bubbles.

2. A test apparatus according to claim 1 further comprising a source of vacuum or air pressure is connected to air connection ( 22 ) connected to the system of fuel lines and hoses ( 18 ).

3. A test apparatus according to claim 1 further comprising a control panel ( 34 ) connected to the fuel system test apparatus.

4. A test apparatus according to claim 1 wherein the fuel particle filter ( 16 ) is a 0.5 to 1 micron particle filter.

5. An apparatus according to claim 1 further comprising:

a means for stopping fuel transfer to the test unit.

6. A test apparatus according to claim 1 wherein the testing unit ( 14 ) further comprises pumps ( 26 ), at least one test gauge ( 28 ) and at least one regulator ( 30 ) located between the engine fuel line interface and the discharge line.

7. A test apparatus according to claim 6 further comprising air operated motors ( 32 ) for driving the pumps ( 26 ).

Assignments (7)
SECURITY INTEREST Recorded Dec 23, 2025
From: TRONAIR, INC.
To: AUDAX PRIVATE DEBT LLC
Reel/Frame 073306/0744 →
RELEASE OF SECURITY INTEREST Recorded Nov 6, 2025
From: CIT NORTHBRIDGE CREDIT LLC, AS AGENT
To: TRONAIR, INC.
Reel/Frame 072810/0331 →
SECURITY INTEREST Recorded Apr 21, 2023
From: TRONAIR, INC.
To: CIT NORTHBRIDGE CREDIT LLC, AS AGENT
Reel/Frame 063399/0070 →
RELEASE OF SECURITY INTEREST Recorded Mar 31, 2023
From: WILMINGTON SAVINGS FUND SOCIETY, FSB
To: TRONAIR, INC.
Reel/Frame 063195/0452 →
ASSIGNMENT OF SECURITY INTEREST IN PATENTS Recorded Nov 11, 2022
From: SOCIÉTÉ GÉNÉRALE, AS ADMINISTRATIVE AGENT AND COLLATERAL AGENT
To: WILMINGTON SAVINGS FUND SOCIETY, FSB, AS SUCCESSOR ADMINISTRATIVE AGENT AND COLLATERAL AGENT
Reel/Frame 061921/0055 →
CORRECTIVE ASSIGNMENT TO CORRECT THE ASSIGNEE STATE OF INCORPORATION FROM OHIO TO GEORGIA PREVIOUSLY RECORDED AT REEL: 042411 FRAME: 0253. ASSIGNOR(S) HEREBY CONFIRMS THE ASSIGNMENT. Recorded Jun 10, 2021
From: SPINAZZE, PAUL; DRAKE, SHERRY
To: TRONAIR INC.
Reel/Frame 056586/0507 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded May 17, 2017
From: SPINAZZE, PAUL; DRAKE, SHERRY
To: TRONAIR INC.
Reel/Frame 042411/0253 →
Continuity (2)
Continuation In Part 13954186 · Jul 30, 2013
Provisional Application 61680846 · Aug 8, 2012