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Variometer comprising a measuring box
   
Document Number
US Patent 3964307
Issued Date
June 22, 1976
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Inventors
Huhne; Dirk (Frenkendorf,CH)
Map
Abstract
The variometer includes a measuring chamber communicating with the atmosphere through a first passageway and an elastically deformable measuring box, positioned within the measuring chamber, communicating with the atmosphere through a second passageway. One of the passageways, preferably the second passageway, is provided with a system of orifice inserts serving to delay pressure equalization between the measuring chamber and the measuring box. The system of orifice inserts includes at least two orifice inserts with successive orifice inserts being separated from each other by an intermediate space. The orifice inserts are threaded into the internally threaded bore of a hollow screw, and preferably three orifice inserts are provided so as to define two intermediate spaces. At least one of the orifice inserts is displaceable axially of the hollow screw, and preferably two orifice inserts are so displaceable. Each orifice insert is a hollow externally threaded member in which the orifice is formed in a bore through a jewel or the like at one end of the orifice insert.
Drawing
Variometer comprising a measuring box - US Patent 3964307 Drawing
Drawing from US Patent 3964307
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Number of Claims:
7
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Owner
Published
June 22, 1976
Application Number
05/581,479
Filed
May 28, 1975
US Classification
73/179  
Int'l Classification
G01P   3/62   (20060101)  
Attorney/Law Firm
Priority Data
Dec 30, 1974 [CH] 17362/74
USPTO Field of Search
73/179   340/27NA  
Related Patents
4376980 - Variometer - Owned by S.F.E.N.A. (Velizy Villacoublay,FR)

This invention concerns an improved variometer which is used in aircraft which operates on a circuit that calculates the instantaneous speed hx.degree. of the aircraft and the potential vertical speed of the aircraft h.sub.T .degree.. A luminous display is also provided to display the values so calculated to alert the pilot of the aircraft. The instantaneous vertical speed hx.degree. is obtained by means of a circuit solving the equation: ##EQU1## in which j.sub.z.sbsb. is the component of the acceleration on the vertical axis of the aircraft, g is the acceleration of gravity, .phi. is the angle of roll of the airplane, s is the Laplace operator, .tau..sub.1 and .tau..sub.2 are constants of time and h.degree..sub.A is a signal of vertical speed.

Claims
Description
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