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Table 2 Physical meanings and expressions of ωn

From: Effect of Dynamic Pressure Feedback Orifice on Stability of Cartridge-Type Hydraulic Pilot-Operated Relief Valve

Sign

Physical meaning

Expressions

ω1

Natural frequency of main mass-spring vibration system.

\(\omega_{1} = \sqrt {\frac{{k_{{1}} + K_{{\text{D}}} p_{{{\text{sx}}}} }}{{m_{{1}} }}}\)

ω2

Natural frequency of pilot mass-spring vibration system.

\(\omega_{2} = \sqrt {\frac{{k_{{2}} + K_{{\text{G}}} p_{{{\text{cx}}}} }}{{m_{{2}} }}}\)

ω3

Break-frequency of chamber A.

\(\omega_{3} = \frac{{E\left( {K_{{\text{A}}} + K_{{\text{C}}} } \right)}}{{V_{{\text{A}}} }}\)

ω4

Break-frequency of chamber C(original model).

\(\omega_{4} = \frac{{E\left( {K_{{\text{C}}} + K_{{\text{E}}} } \right)}}{{V_{{\text{C}}} }}\)

ω5

Break-frequency of the main port differential element.

\(\omega_{5} = \frac{{K_{{\text{B}}} }}{{A_{{1}} }}\)

ω6

Break-frequency of the pilot port differential element.

\(\omega_{6} = \frac{{K_{{\text{F}}} }}{{A_{{2}} }}\)

ω7

Break-frequency of chamber B(original model).

\(\omega_{7} = \frac{{EG_{{\text{r}}} }}{{V_{{\text{B}}} }}\)

ω8

Break-frequency produced by the orifice R2.

\(\omega_{8} = \frac{{G_{{\text{r}}} }}{{A_{1}^{2} }}\)

ω9

Break-frequency of integration element corresponding to chamber B.

\(\omega_{9} = \frac{E}{{V_{{\text{B}}} }}\)

ω10

Break-frequency of chamber B(contrast model).

\(\omega_{10} = \frac{{E\left( {K_{{\text{C}}} + K_{{\text{E}}} } \right)}}{{V_{{\text{B}}} }}\)