Seal plates are typically mounted over stringer-receiving openings in aircraft ribs. A sealing tool for sealing a stringer-receiving opening in an aircraft rib is disclosed. The sealing tool includes a seal member arranged to seal a gap formed by the opening between the stringer and the rib. An intermediate member is configured to be adjustably mounted on the rib. The adjustable member receives and aligns the seal member over the gap.

A sealing assembly and a turbomachine including the sealing assembly are provided. The sealing assembly includes a sealing body configured to be inserted into an insertion hole of a second component adjacent to a first component, and a sealing protrusion, formed on one circumferential side of the sealing body, protruding toward one circumferential direction from the sealing body and configured to be inserted into a sealing groove formed on the other circumferential side of a sealing body of the first adjacent sealing assembly, the sealing body of the first adjacent sealing assembly being adjacent to the sealing body in a circumferential direction.

Various embodiments provide for a filter assembly. The filter assembly includes a filter housing, a filter element, and a cover. The filter housing has a first housing end and a second housing end that define an internal cavity. The filter housing has a housing seal member formed on the second housing end. The filter element is disposed in the internal cavity. The filter element includes a filter media, an endplate, and a filter seal member. The filter media has a first media end and a second media end. The endplate is disposed at the first media end. The filter seal member is formed on the endplate. The filter seal member includes an inner seal portion and an outer seal portion. The filter seal member is configured to engage the housing seal member. The cover secures the engagement of the housing seal member and the filter seal member.

A seal is disclosed having a pair of side walls, a base extending between the side walls, a first concave surface extending inwardly from one of the side walls, a second concave surface extending inwardly from the other side wall, and a convex surface extending between the first concave and second concave surface to form a rounded peak having an apex. The seal has a seal width defined between the seal side walls, and a seal height defined between the apex of the rounded peak and the base. The width is at least twice the height of the seal. The seal is located in a channel recess of a first component opposite a second component to seal between the first component and the second component, the channel recess having a floor and a height defined between the floor and a surface of the first component in which the channel recess is formed.

A seal is disclosed having a pair of side walls, a base extending between the side walls, a first concave surface extending inwardly from one of the side walls, a second concave surface extending inwardly from the other side wall, and a convex surface extending between the first concave and second concave surface to form a rounded peak having an apex. The seal has a seal width defined between the seal side walls, and a seal height defined between the apex of the rounded peak and the base. The width is at least twice the height of the seal. The seal is located in a channel recess of a first component opposite a second component to seal between the first component and the second component, the channel recess having a floor and a height defined between the floor and a surface of the first component in which the channel recess is formed.

A sealing member has a seal body configured to be inserted into a groove of a cover member. The seal body has, in a vehicle-exterior-side end portion, a first sealing lip portion formed in such a manner as to protrude toward a door hole. The first sealing lip portion is configured to be brought into press-contact with a peripheral portion of the groove of the cover member on a side nearer to the door hole. The sealing member includes an edge seal portion provided in the vehicle-exterior-side end portion of the seal body. The edge seal portion is configured to press the first sealing lip portion against the cover member while being brought into press-contact with a peripheral portion of the door hole of a door inner panel.

A sealing member has a seal body configured to be inserted into a groove of a cover member. The seal body has, in a vehicle-exterior-side end portion, a first sealing lip portion formed in such a manner as to protrude toward a door hole. The first sealing lip portion is configured to be brought into press-contact with a peripheral portion of the groove of the cover member on a side nearer to the door hole. The sealing member includes an edge seal portion provided in the vehicle-exterior-side end portion of the seal body. The edge seal portion is configured to press the first sealing lip portion against the cover member while being brought into press-contact with a peripheral portion of the door hole of a door inner panel.

Apparatus and method contemplating a high pressure fluid end assembly having a body defining a body bore and defining a groove in the body intersecting the body bore. A closure is joined to the body and forms a sealing surface. A seal is mounted to the body in the groove and configured to extend from the groove beyond the body bore to seal against the sealing surface formed by the closure.

In accordance with at least one aspect of this disclosure, a fuel seal for an aircraft fuel system includes a seal ring of a metallic material configured to retain a shape of the seal ring under compression, and a coating of elastomeric material, over molded onto the seal ring and configured to conform to a shape of a sealing surface. In embodiments, the seal ring and coating can be configured to provide drop-tight sealing at a temperature of at least 400 degrees F. In certain embodiments, the seal ring and coating can be configured to seal one or more fuel system components of an aircraft fuel system.

A gasket installation guide and method of use wherein the gasket installation guide is used to aid in the insertion of rubber gaskets into flair connector comprising a body that is inserted into the flair connector to align the center hole that passes through the body with the female flare fitting of the flair connector, so that the rubber gasket can be easily installed.