IP Library Granted Patent US 7,227,131
Granted Patent B2
US 7,227,131 · App. 10/929,768 · Granted Jun 5, 2007

Time of flight mass spectrometer

Assignees: Shimadzu Corporation; Osaka University
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Quick Facts
Patent No.
US 7,227,131
App. No.
10/929,768
Granted
Jun 5, 2007
Kind
B2
Abstract

A time of flight type mass spectrometer (TOF-MS) of the present invention includes: a flight space containing a loop orbit on which ions fly once or more than once; a flight controller for making ions of a same mass to charge ratio fly the loop orbit at several values of number of turns; a flight time measurer for measuring a length of flight time of the ions; and a processor for determining the mass to charge ratio of the ions based on a relationship between the value of number of turns and the length of flight time of the ions. The speed of ions flying a loop orbit depends on their mass to charge ratios. For ions of the same mass to charge ratio, the difference between the lengths of flight time of the ions flying the loop orbit N turns and of the ions flying the loop orbit N+1 turns depends on the speed of the ions, so that the difference depends on the mass to charge ratio of the ions. The difference in the length of flight time is unrelated to the variation in the starting time (jitter), variation in the detection timing (jitter), etc, so that the value of the mass to charge ratio can be precisely determined free from errors caused by such disturbing factors.

Claims (5)

1. A time of flight mass spectrometer (TOF-MS) comprising: a flight space containing a loop orbit on which ions fly once or more than once; a flight controller for making ions of a same mass to charge ratio fly the loop orbit at at least two values of number of turns; a flight time measurer for measuring a length of flight time of the ions; and a processor for determining the mass to charge ratio of the ions based on a relationship between the value of number of turns and the length of flight time of the ions.

2. The TOF-MS according to claim 1 , wherein the loop orbit is circular.

3. The TOF-MS according to claim 1 , wherein the loop orbit is figured “8”.

4. The TOF-MS according to claim 1 , wherein the flight controller makes ions of a same mass to charge ratio fly the loop orbit at more than two values of number of turns.

5. The TOF-MS according to claim 1 , wherein the flight controller makes ions of a same mass to charge ratio fly the loop orbit at two values of number of turns, and the processor determines the mass to charge ratio of the ions based on a relationship between a difference of the two values of number of turns and a difference of the lengths of flight time of the ions at the two values of number of turns.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded May 12, 2005
From: YAMAGUCHI, SHINICHI; ISHIHARA, MORIO; TOYODA, MICHISATO; OKUMURA, DAISUKE
To: SHIMADZU CORPORATION; OSAKA UNIVERSITY
Reel/Frame 016558/0682 →
Priority Claims (1)
JP 2003-309553 · Sep 2, 2003 · national
Continuity (1)
Related Publication 20050194528A1 · Sep 8, 2005