Taper bolt connection and use of a taper bolt connection
View Patent ↗Disclosed is a taper bolt connection including a taper bolt received in a taper bush, a fastening nut and a washer, the taper bush having a continuous longitudinal slot, and the taper bush being capable of being spread open uniformly in the radial direction by means of a fastening nut screwable onto the taper bolt. Since the taper bolt and/or the taper bush have/has, at least in regions, an at least Teflon-containing coating, tribochemical processes between the taper bush wedge surface and the taper bolt wedge surface are largely avoided, so that the taper bolt connection can be released again without great effort even after a long period of connection. Furthermore disclosed is the use of the taper bolt connection for connecting a rudder unit to a carrying structure of a fuselage cell of an aircraft.
1. A taper bolt connection for use in an aircraft comprising a taper bolt comprising a wedge surface, a taper bush having a wedge surface, a fastening nut, and a washer,
wherein the taper bush comprises a continuous longitudinal slot,
wherein the taper bush is capable of being spread open uniformly in the radial direction by means of the fastening nut screwed onto said taper bolt,
wherein a longitudinal extent of the taper bush wedge surface corresponds to a longitudinal extent of said taper bolt wedge surface, and
wherein said taper bolt is capable of avoiding a tribochemical reaction between the contact surfaces of said taper bolt and said taper bush by means of includes a polytetraflouroethylene-containing coating comprising at least three strips arranged uniformly spaced apart from one another, around the circumference of said taper bolt, and
each strip extending over the entire longitudinal extent of said taper bolt wedge surface.
2. The taper bolt connection according to claim 1 , wherein the taper bolt wedge surface and the taper bush wedge surface each comprise an inclination ratio ranging from 0.01 to 0.1.
3. The taper bolt connection according to claim 1 , wherein the Teflon containing coating comprises a thickness ranging from 0.01 mm to 0.5 mm.
4. The taper bolt connection according to claim 3 , wherein the Teflon containing coating comprises a thickness of about 0.15 mm.
5. The taper bolt connection according to claim 1 , wherein the taper bush and the taper bolt are formed from titanium.
6. The taper bolt connection according to claim 1 , wherein the taper bush and the taper bolt are formed from high-grade steel.
7. The taper bolt connection according to claim 1 , wherein the washer is arranged between the fastening nut and the taper bolt.
8. The taper bolt connection according to claim 1 , wherein the fastening nut is a castle nut secured onto the taper bolt by means of a securing cotter pin.
9. Use of a taper bolt connection according to claim 8 for fastening a rudder unit to a fork connected to a carrying structure of a fuselage cell of an aircraft, comprising the steps of:
receiving the taper bush in a sleeve of the rudder unit, and two bore holes of the fork,
introducing the taper bolt into the taper bush,
bracing the taper bolt with the castle nut,
locating the washer between the castle nut and the taper bush,
bracing the taper bolt with the taper bush,
tightening of the castle nut to draw the taper bolt into the taper bush,
spreading the taper bush uniformly outwards in the radial direction; and
bracing firmly the rudder unit with the fork.