Datei:US2656017-drawings-page-4 core.png – Wikipedia

Originaldatei (1.860 × 2.708 Pixel, Dateigröße: 137 KB, MIME-Typ: image/png)

Diese Datei und die Informationen unter dem roten Trennstrich werden aus dem zentralen Medienarchiv Wikimedia Commons eingebunden.

Zur Beschreibungsseite auf Commons

Beschreibung

Beschreibung

Beschreibung
English: Automatic braking apparatus for aircraft
English: Automatic Braking Apparatus for Aircraft
  • Figure 1 -is a side elevation, partly in section, of an automatic brake apparatus constructed in accordance with the invention looking from the left of Figure 2,
  • Figure 2 is a section through A--A of Figure 1, looking in the direction of the arrows.
  • Figure 3 is a part section through B-B of figure 1, looking in the direction of the arrows.
  • Figure 4 is a view from the left of Figure 2, with the valve-body removed.
  • Figure 5 is a part section through C-C of Figure 2 looking in the direction of the arrows.
  • Figure 6 is a part view from the right of Figure 2 with the flywheel casing and bracket arm removed.
  • 1 flange
  • 2 arm
  • 3 arm
  • 4 hollow cylindrical housing
  • 4a radially-extending wall (radial wall)
  • 4b axially-extending peripheral wall
  • 4c a separable radially-extend wall (radial wall)
  • 5 boss
  • 6 metal bearing
  • 7 cylindrical recess
  • 8 ball bearings
  • 9 bearing
  • 10 annular flange
  • 11 metal bearing
  • 12 ball bearings
  • 13 bearing
  • 14 sealing ring
  • 15 solid rubber twin-contact tire
  • 16 and 17 coaxial drums
    • 16 outer drum
    • 17 inner drum
  • 18 two diametrically opposed Substantially arcuate portions / acurate stops of the drum member
  • 19 screws
  • 20 dowels
  • 22 rcumferentially-extending slot
  • 23 circumferentially extending recess
  • 24 series of ball-bearings
  • 25 annular flywheel
  • 26 radially-extending rib
  • 27 a plurality of equispaced, axially-extending blind holes
  • 28 clock-type coiled Spring
  • 29 blind holes
  • 30 thin beam / flywheel beam
  • 31 two equi-sized holes (for balls 35)
  • 32 cam member/drum member
  • 33 two diametrically Opposed keys
  • 34 anti-friction ball
  • 35 two balls (in holes 31)
  • 36 disc
  • 37 part-annular torque-arms (clutch mechanism)
  • 37a extending portion
  • 38 part-annular torque-arms
  • 38a extending portion
  • 39 extending hole
  • 40 stud
  • 41 helical spring
  • 42 coaxial hole
  • 43 Grease retainers
  • 44 substantially rectangular recess
  • 45 thrust rod / spring-loaded thrust rod
  • 46 part-spherical projection
  • 47 helical spring
  • 48 annular flange
  • 49 spindle
  • 50 cranked lever arm / inlet valve
  • 51 lever arm
  • 52 second recess / pressure chamber
  • 53 sealing washer
  • 54 rectangular valve body
  • 54a sealing ring
  • 55 blind hole
  • 56 fluid pressure conduit
  • 57 two brake operating nozzles
  • 58 valve beam
  • 60 slide valve / inlet valve
  • 62 radially extending holes
  • 63 radially extending holes
  • 64 annular groove
  • 64a pressure conduit
  • 65 inlet nozzle
  • 66 filter
  • 67 exhaust valve plug
  • 68 annular recess
  • 69 holes
  • 70 hole
  • 71 a smaller coaxial hole
  • 72 exhaust valve
  • 73 exhaust nozzle
  • 74 leaf-spring
  • 72 exhaust valve
Deutsch: * 15 massiver Reifen
  • 16 & 17 Trommel
  • 25 Schwungrad
  • 28 Drehfeder
  • 60 Ventil
Datum
Quelle https://patents.google.com/patent/US2656017A/en
Urheber Trevaskis Henry William (Dunlop Rubber Co Ltd)

Lizenz

Public domain The text and illustrations of US patents published before March 1, 1989 are in the public domain unless the patent text contains a specific notice that portions are copyrighted. See 37 CFR 1.71(d), 37 CFR 1.84(s)

The original patent contains no such notice, so its contents are in the public domain. Note: This only applies to images published before March 1, 1989. Patents published after that date are most likely copyrighted, unless in the public domain for another reason, such as {{PD-ineligible}}.

Dateiversionen

Klicke auf einen Zeitpunkt, um diese Version zu laden.

Version vomVorschaubildMaßeBenutzerKommentar
aktuell06:42, 29. Jul. 2023Vorschaubild der Version vom 06:42, 29. Jul. 20231.860 × 2.708 (137 KB)MichaelFrey=={{int:filedesc}}== {{Information |description={{en|1=Automatic braking apparatus for aircraft {{:User:MichaelFrey/US2656017}}}} |date=1950-11-14 |source=https://patents.google.com/patent/US2656017A/en |author=Trevaskis Henry William (Dunlop Rubber Co Ltd) |permission= |other versions= }} =={{int:license-header}}== {{PD-US-patent-no notice}} Category:Dunlop Maxaret

Die folgende Seite verwendet diese Datei:

Metadaten

Diese Datei enthält weitere Informationen (beispielsweise Exif-Metadaten), die in der Regel von der Digitalkamera oder dem verwendeten Scanner stammen. Durch nachträgliche Bearbeitung der Originaldatei können einige Details verändert worden sein.

Abgerufen von „https://de.wikipedia.org/wiki/Datei:US2656017-drawings-page-4_core.png“