IPC분류정보
국가/구분 |
United States(US) Patent
등록
|
국제특허분류(IPC7판) |
|
출원번호 |
US-0212065
(2002-08-06)
|
우선권정보 |
FR-0012829 (2001-10-05) |
발명자
/ 주소 |
- Maury, Jean-Pierre
- Milhau, Alain
- Pauly, Bernard
|
출원인 / 주소 |
|
대리인 / 주소 |
Stevens, Davis, Miller & Mosher, LLP
|
인용정보 |
피인용 횟수 :
19 인용 특허 :
5 |
초록
▼
An aircraft includes a fuselage and a fixed flying surface having two wings, and a cradle-shaped ventral fairing at the crossover of the latter with the flying surface and provided with two longitudinal flanges climbing laterally along the fuselage and being provided with an opening for the passage
An aircraft includes a fuselage and a fixed flying surface having two wings, and a cradle-shaped ventral fairing at the crossover of the latter with the flying surface and provided with two longitudinal flanges climbing laterally along the fuselage and being provided with an opening for the passage with play of the corresponding wing to form a first peripheral slot around the ventral fairing and a second peripheral slot around each wing. An elongate seal is fixed to the periphery of the ventral fairing and to the periphery of each opening, so at to shut off the first and second slots, respectively. The seal includes a longitudinal elastic end lip applied, via the inner face of its free end, respectively against the fuselage or the flying surface and a longitudinal leaktightness member, carried by the inner face of the seal set back with respect to the end lip and also able to be applied against the fuselage or flying surface, respectively. The additional longitudinal leaktightness member is radially elastic bead.
대표청구항
▼
An aircraft includes a fuselage and a fixed flying surface having two wings, and a cradle-shaped ventral fairing at the crossover of the latter with the flying surface and provided with two longitudinal flanges climbing laterally along the fuselage and being provided with an opening for the passage
An aircraft includes a fuselage and a fixed flying surface having two wings, and a cradle-shaped ventral fairing at the crossover of the latter with the flying surface and provided with two longitudinal flanges climbing laterally along the fuselage and being provided with an opening for the passage with play of the corresponding wing to form a first peripheral slot around the ventral fairing and a second peripheral slot around each wing. An elongate seal is fixed to the periphery of the ventral fairing and to the periphery of each opening, so at to shut off the first and second slots, respectively. The seal includes a longitudinal elastic end lip applied, via the inner face of its free end, respectively against the fuselage or the flying surface and a longitudinal leaktightness member, carried by the inner face of the seal set back with respect to the end lip and also able to be applied against the fuselage or flying surface, respectively. The additional longitudinal leaktightness member is radially elastic bead. application No. PCT/US 01/11447, Date of Mailing Jul. 19, 2001, 6 pages. Search Report for Patent Cooperation Treaty application No. PCT/US 01/11467, Date of Mailing Jul. 19, 2001, 7 pages. Search Report for Patent Cooperation Treaty application No. PCT/US 01/12091, Date of Mailing Jul. 9, 2001, 4 pages. Search Report for Patent Cooperation Treaty application No. PCT/US 01/14113, Date of Mailing Jul. 19, 2001, 6 pages. Search Report for Patent Cooperation Treaty application No. PCT/US 01/40677, Date of Mailing Jul. 19, 2001, 6 pages. Letter, dated Apr. 4, 1998, and accompanying drawings. Invitation to Pay Additional Fees for Patent Cooperation Treaty application No. PCT/US 01/27698, Date of Mailing Jan. 10, 2002, 7 pages. Search Report for Patent Cooperation Treaty application No. PCT/US 01/28520, Date of Mailing Mar. 4, 2002, 7 pages. Search Report for Patent Cooperation Treaty application No. PCT/US01/27698, Date of Mailing Apr. 5, 2002, 4 pages.
※ AI-Helper는 부적절한 답변을 할 수 있습니다.